2014 COURSE UNIVERSITY OF KANSAS CATALOG

LAS VEGAS SEATTLE MARYLAND SAN DIEGO ORLANDO March April June September November

aeroshortcourses.ku.edu/air Toll-free in the U.S.: 877-404-5823 or 785-864-5823 2014 COURSE UNIVERSITY OF KANSAS CATALOG

Invest in Yourself • Invest in Your Company • Invest in the Aerospace Industry

GLOBAL LEADERS IN AEROSPACE TRAINING

The University of Kansas Continuing Education Aerospace Short Course Program has been serving the worldwide aerospace community for the last 36 years by providing outstanding non-credit short courses in aircraft design, flight control systems, aircraft compliance and safety, avionic hardware and software and aerospace systems and process management.

The Aerospace Short Course Program was founded in 1977 to address the professional development needs of aircraft designers in the North American aerospace industry. It has evolved into one of the most respected non- credit professional development programs in the worldwide aerospace industry. In recent years, one third of our course attendees have been from outside of the United States.

WELCOME TO OUR 2014 COURSE LISTINGS

In the following pages of this catalog you will find detailed descriptions of our exceptional courses, instructors and delivery methods.

With a brilliant instructor pool derived from industry, academia and government experts, the 2014 program offers more than 40 publicly offered short courses at five locations in the United States. Our 2014 public course schedule is located on pages 3–4. We can also bring our courses to your workplace. See page 11 for details. Plus, striving to meet individual training needs, we offer video and web-based conferencing opportunities and on-line courses. See page 12.

As you peruse our 2014 course catalog, if you have any questions or comments, please contact our staff. We are here to serve you.

Professional education is vital to increasing your effectiveness in the workforce. We invite you to invest in your success by registering for a short course today!

Our internationally recognized program uniquely serves your training needs by:

• Offering practical, one-of-a-kind classes taught by outstanding academic and industry professionals; • Continually upgrading the portfolio of courses by diligently following the industry trends and needs; • Providing outstanding customer services; • Responding to global client companies and individual customers by traveling to their locations and respecting their culture and learning styles.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 2 2014 KU AEROSPACE SHORT COURSES LIST Advanced Flight Tests 13 Aerodynamic Design Improvements: High-Lift and Cruise ...... 14 Aerodynamic Design of Transport Aircraft NEW ...... 15 Aerospace Applications of Systems Engineering 16 Aircraft Engine Vibration Analysis, Turbine and Reciprocating Engines: FAA Item 28489 ...... 17 Aircraft Icing: Meteorology, Protective Systems, Instrumentation and Certification 18 Aircraft Lightning: Requirements, Component Testing, Aircraft Testing and Certification 19 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification 20 Aircraft Structures Design and Analysis ...... 21 Airplane Aerodynamic Design and Subsonic Wind Tunnel Testing ...... 22 Airplane Flight Dynamics: Open and Closed Loop ...... 23 Airplane Performance: Theory, Applications and Certification (online course) 24 Airplane Preliminary Design ...... 25 Applied Nonlinear Control and Analysis 26 Aviation Weather Hazards ...... 27 Commercial Aircraft Safety Assessment and 1309 Design Analysis 28 Commercial Space—What It Means and the Issues It Raises NEW 29 Complex Electronic Hardware Development and DO-254 30 Conceptual Design of Unmanned Aircraft Systems 31 Digital Flight Control Systems: Analysis and Design ...... 32 Durability and Damage Tolerance Concepts for Aging Aircraft Structures (online course) 33 Electrical Wiring Interconnect System (EWIS) and FAA Requirements NEW ...... 34 Essentials of Effective Technical Writing for Engineering Professionals NEW ...... 35 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems 36 FAA Conformity, Production and Airworthiness Certification Approval Requirements ...... 37 FAA Functions and Requirements Leading to Airworthiness Approval ...... 38 FAA Parts Manufacturer Approval (PMA) Process for Aviation Suppliers 39 FAR 145 for Aerospace Repair and Maintenance Organizations ...... 40 Flight Control Actuator Analysis and Design ...... 41 Flight Control and Hydraulic Systems ...... 42 Flight Test Principles and Practices ...... 43 Flight Testing Unmanned Aircraft—Unique Challenges ...... 44 Fundamental Avionics ...... 45 Fundamentals of Project Management for Aerospace Professionals ...... 46 Integrated Modular Avionics (IMA) and DO-297 47 Modelling and Analysis of Dynamical Systems: A Practical Approach 48 Operational Aircraft Performance and Flight Test Practices 49 Principles of Aeroelasticity ...... 50 Principles of Aerospace Engineering ...... 51 Process-Based Management in Aerospace: Defining, Improving and Sustaining Processes ...... 52 Propulsion Systems for UAVs and General Aviation Aircraft ...... 53 Reliability and 1309 Design Analysis for Aircraft Systems (online course) 54 Rotorcraft Vibration: Analysis and Practical Reduction Methods 55 RTCA DO-160 Qualification: Purpose, Testing and Design Considerations 56 Software Safety, Certification and DO-178C ...... 57 Stress Analysis for Aerospace Structures NEW ...... 58 Structural Composites ...... 59 Subcontract Management in Aerospace Organizations 60 Sustainment and Continued Airworthiness for Aircraft Structures ...... 61 Unmanned Aircraft System Software Airworthiness ...... 62

Welcome ...... 1 General information ...... 7 Individual course listings . . . . . 13 Short courses list ...... 2 Certificates of specialization . . . . 9 Instructor biographies ...... 63 Public courses schedule ...... 3 On-site class information . . . . . 11 Registration form . . . . .back cover Lodging and travel information . . 5 Course delivery options . . . . . 12 aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 3 2014 KU AEROSPACE SHORT COURSES PUBLIC SCHEDULE Las Vegas, Nevada Alexis Park All Suite Resort Course # Page March 3–7 Airplane Aerodynamic Design and Subsonic Wind Tunnel Testing AA141260 22 Willem A.J. Anemaat March 3–7 Operational Aircraft Performance and Flight Test Practices AA141270 49 Mario Asselin March 3–7 Principles of Aerospace Engineering AA141280 51 Wally Johnson March 4–6 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems AA141290 36 Robert D. Adamson March 4–7 Aircraft Icing: Meteorology, Protective Systems, Instrumentation and Certification AA141300 18 Wayne R. Sand, Steven L. Morris March 4–7 Fundamentals of Project Management for Aerospace Professionals AA141310 46 Herbert Tuttle March 4–7 RTCA DO-160 Qualification: Purpose, Testing and Design Considerations AA141320 56 Ernie Condon

Seattle, Washington DoubleTree Suites by Hilton Hotel Seattle Airport—Southcenter April 28–May 2 NEW Aerodynamic Design of Transport Aircraft AA141330 15 Roelof Vos April 28–May 2 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification AA141340 20 Wally Johnson April 28–May 2 Aircraft Structures Design and Analysis AA141350 21 Michael Mohaghegh, Mark S. Ewing April 28–May 2 Airplane Preliminary Design AA141360 25 Willem A.J. Anemaat April 28–May 2 Commercial Aircraft Safety Assessment and 1309 Design Analysis AA141370 28 Marge Jones April 28–May 2 Fundamental Avionics AA141380 45 Albert Helfrick April 29–May 1 FAA Functions and Requirements Leading to Airworthiness Approval AA141390 38 Gilbert L. Thompson April 29–May 2 Aviation Weather Hazards AA141400 27 Wayne R. Sand California, Maryland Southern Maryland Higher Education Center June 9–13 Advanced Flight Tests AA141410 13 Donald T. Ward, Thomas William Strganac June 9–13 Rotorcraft Vibration: Analysis and Practical Reduction Methods AA141420 55 Richard L. Bielawa San Diego, California Marriott Mission Valley Week One September 8–10 Complex Electronic Hardware Development and DO-254 AA151000 30 Jeff Knickerbocker September 8–11 Sustainment and Continued Airworthiness for Aircraft Structures AA151010 61 Marv Nuss September 8–12 Commercial Aircraft Safety Assessment and 1309 Design Analysis AA151020 28 Marge Jones September 8–12 Conceptual Design of Unmanned Aircraft Systems AA151030 31 Bill Donovan aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 4 2014 KU AEROSPACE SHORT COURSES PUBLIC SCHEDULE San Diego, cont’d. Course # Page September 8–12 Flight Test Principles and Practices AA151040 43 Donald T. Ward, George Cusimano September 9–11 FAA Conformity, Production and Airworthiness Certification Approval Requirements AA151050 37 Jim Reeves September 9–11 Unmanned Aircraft System Software Airworthiness AA151060 62 Willie J. Fitzpatrick, Jr. September 10–12 FAA Functions and Requirements Leading to Airworthiness Approval AA151070 38 Gilbert L. Thompson and Robert D. Adamson September 11–12 Integrated Modular Avionics (IMA) and DO-297 AA151080 47 Jeff Knickerbocker September 8–12 Combine AA151000 (DO-254) and AA151080 (DO-297) (SAVE $) AA151090 30, 47 Jeff Knickerbocker Week Two September 15–17 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems AA151100 36 Gilbert L. Thompson and Robert D. Adamson September 15–17 Flight Testing Unmanned Aircraft—Unique Challenges AA151110 44 George Cusimano September 15–18 Software Safety, Certification and DO-178C AA151120 57 Jeff Knickerbocker September 15–19 Aircraft Engine Vibration Analysis, Turbine and Reciprocating Engines: FAA Item 28489 AA151130 17 Guil Cornejo September 15–19 NEW Electrical Wiring Interconnect System (EWIS) and FAA Requirements AA151140 34 C. Bruce Stephens September 15–19 Principles of Aeroelasticity AA151150 50 Thomas William Strganac September 15–19 Structural Composites AA151160 59 Mark S. Ewing September 16–19 NEW Stress Analysis for Aerospace Structures AA151170 58 Dennis C. Philpot September 18–19 NEW Essentials of Effective Technical Writing for Engineering Professionals AA151180 35 Paul H. Park

Orlando, Florida DoubleTree by Hilton at the Entrance to Universal Orlando November 17–21 Aircraft Lightning: Requirements, Component Testing, Aircraft Testing and Certification AA151190 19 C. Bruce Stephens November 17–21 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification AA151200 20 Wally Johnson November 17–21 Aircraft Structures Design and Analysis AA151210 21 Michael Mohaghegh, Mark S. Ewing November 17–21 Airplane Flight Dynamics: Open and Closed Loop AA151220 23 Willem A.J. Anemaat November 17–21 Digital Flight Control Systems: Analysis and Design AA151230 32 David R. Downing November 17–21 Flight Control and Hydraulic Systems AA151240 42 Wayne Stout November 17–21 Fundamental Avionics AA151250 45 Albert Helfrick November 18–20 NEW Commercial Space—What It Means and the Issues It Raises (new) AA151260 29 Marco Villa, Max Vozoff aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 5 LODGING AND TRAVEL INFORMATION

• Lodging and transportation costs are not included in the course fees. • Attendees are responsible for acquiring their own lodging and travel arrangements. • The following lodging and transportation suggestions are offered as a convenience and do not represent an endorsement.

Las Vegas, Nevada Seattle, Washington March 3–7, 2014 April 28–May 2, 2014

Alexis Park All Suite Resort DoubleTree Suites by Hilton Hotel Seattle Airport – 375 East Harmon Southcenter Las Vegas, Nevada 89109 16500 Southcenter Parkway Seattle, Washington 98188 A limited number of rooms has been reserved at the Alexis Park All Suite Resort for course attendees. This is a non- A limited number of rooms has been reserved at the gaming facility. The rate is $89 for a standard single room Doubletree Suites by Hilton Hotel Seattle Airport – and $99 for a double room plus applicable state and local Southcenter for course attendees. The rate is $129 for a occupancy taxes. These rooms will be held as a block, unless standard single/double room plus local occupancy taxes. These depleted, until February 13, 2014, at which time they will rooms will be held as a block, unless depleted, until April 24, be released to the public. After February 13, room rate and 2014, at which time they will be released to the public. After availability cannot be guaranteed. April 24, room rate and availability cannot be guaranteed.

To ensure that you get all the benefits available to our group To ensure that you get all the benefits available to our group, including complimentary Internet in the guest rooms (for one including complimentary self-parking and Internet in the guest device per registered person) and free parking, please make rooms, please make sure you or your travel agent book your hotel sure you or your travel agent book your hotel room in the room in the University of Kansas room block. State that you will University of Kansas room block. Our group code is “AERO be attending a University of Kansas aerospace short course and 014”. To make a reservation, call 1-800-582-2228 (toll-free in the give the Group Code UOK. To make your reservation, call (toll- continental United States) or 1-702-796-3322. Hotel reservations free worldwide) 800-222-8733. Reservations can also be made may also be made via email at [email protected] or on-line. All reservations must be guaranteed with a major credit on-line. Please note that room rates cannot be changed after card or first night room deposit. For additional assistance the check-in for guests who fail to identify their group affiliation. A direct number to the hotel is: 206-575-8220. deposit of the first night’s revenue plus tax is required. You may cancel with no fee up to 48 hours prior to arrival. The deposit The Seattle-Tacoma International Airport (SEA) is 3.5 miles will be forfeited for all no-show reservations. (5.6 km) from the hotel. The hotel provides complimentary shuttle service. No reservation is required. The hotel shuttle The McCarran International Airport (LAS) is 2 miles (3.2 courtesy phone is located on the baggage claim level. There are km) from the Alexis Park All Suite Resort. The hotel provides two Doubletree properties near the airport. Make sure to take complimentary airport shuttle, based on availability, from the shuttle for the Doubletree Suites by Hilton Hotel Seattle 7:00 am to 10:00 pm daily. To use the Alexis Park Resort Airport – Southcenter. Taxi cab fare is approximately $18. Airport Shuttle, call (702) 796-3300 once you have deplaned and are headed to the baggage claim area. Taxi cab fare The Doubletree Suites by Hilton Hotel Seattle Airport – is approximately $8. Commercial airport shuttle fare is Southcenter also offers complimentary shuttle to the light rail approximately $12–15 roundtrip. Ground transportation pick train station. Getting to downtown Seattle is easy using this up is located on the level below the baggage claim level. new transit system.

Southern Maryland There is no hotel room block associated with this event. For June 9–13, 2014 a list of hotels in the area, please visit the St. Mary’s County Travel & Tourism website: www.visitstmarysmd.com Southern Maryland Higher Education Center International airports serving this area: 44219 Airport Road • Baltimore-Washington Thurgood Marshall International California, Maryland 20619 Airport (BWI) • Ronald Reagan Washington National Airport (DCA) Courses will be held on the Southern Maryland Higher • Dulles International Airport (IAD) Education Center campus. Parking is free. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 6

Are you planning to attend one of our programs in the United States but are not a U.S. citizen? Please visit travel.state.gov/visa for visa and travel information.

San Diego, California Orlando, Florida September 8–12, 2014 • September 15–19, 2014 November 17–21, 2014

San Diego Marriott Mission Valley DoubleTree by Hilton at the Entrance to Universal 8757 Rio San Diego Drive Orlando San Diego, California 92108 5780 Major Boulevard Orlando, Florida 32819 A limited number of rooms has been reserved at the San Diego Marriott Mission Valley for course attendees. The A limited number of rooms has been reserved at the rate will be the prevailing U.S. federal government per diem DoubleTree by Hilton at the Entrance to Universal Orlando for September 2014 (the current rate is $133) for a single/ for course attendees. The rate will be the U.S. federal double room plus applicable state and local occupancy taxes. government per diem for November 2014 (the current rate These rooms will be held as a block, unless depleted, until is $97) for a single/double room plus applicable state and August 14, 2014, at which time they will be released to the local occupancy taxes. These rooms will be held as a block, public. After August 14, room rate and availability cannot be unless depleted, until October 30, 2014, at which time guaranteed. they will be released to the public. After October 30, room rate and availability cannot be guaranteed. Orlando is a To ensure that you get all the benefits available to our group, busy convention town and the hotel may sell out so book including complimentary Internet in the guest rooms and your room early. Please note that room reservations at this discounted parking, please make sure you or your travel property must be cancelled 72 hours prior to arrival to avoid agent book your hotel room in the University of Kansas room cancellation penalties and early departures are subject to an block. State that you will be attending a University of Kansas early departure penalty. aerospace short course and give the group code KANKANA. To make your reservation, call (toll-free worldwide) 877-622- To ensure that you get all the benefits available to our group, 3056 or 619-692-3800. All reservations must be guaranteed including discounted parking and Internet in the guest with a major credit card or first night room deposit. rooms, please make sure you or your travel agent book your hotel room in the University of Kansas room block. No Participants are responsible for their own parking fees. The group code number was available at the time of publishing. San Diego Marriott Mission Valley will offer a discounted rate Please check our website for updated information. To make a of $5.00 a day for overnight self-parking and day guests. reservation, call (toll-free worldwide) 800-327-2110 or 407-351- 1000. State that you will be attending a University of Kansas The San Diego International Airport (SAN) is 8.1 miles (13 aerospace short course. All reservations must be guaranteed km) from the hotel. SuperShuttle provides transportation for and accompanied by a first night’s room deposit by credit $12.00 each way to and from the Marriott Mission Valley hotel. card, guest check or money order. (Fees are subject to change.) Arrangements can be made online at www.supershuttle.com or by calling (toll-free in the United The Orlando International Airport (ORL) is 18 miles (29 km) States) 800-258-3826. The local number is 858-974-8885. Be from the DoubleTree by Hilton at the Entrance to Universal sure to use our group code UPBP7 to receive a discounted rate. Orlando. Mears Transportation provides 24 hour shuttle Taxi cab fare is approximately $30–35 each way. service for $19 one-way or $30 round trip. (Fees are subject to change.) Reservations can be made on-line or walk-up service is available at the Mears Transportation kiosk on level one of the airport. For additional information, call them at For the most current information on our 407-423-5566. Orlando Airport Van is now providing airport courses and events, including convenient shuttle service in Orlando. Their rate is $9.99 per passenger. weblinks to assist you with making your Reservations can be made on line or by calling 866-204-4000. travel plans, please visit our website at Taxi cab fare is approximately $45 each way. aeroshortcourses.ku.edu/air/locations/

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 7

GENERAL INFORMATION aeroshortcourses.ku.edu/air

Phone 785-864-5823 or toll-free within the U.S. 877-404-5823 Fax 785-864-4871 Email [email protected] Website aeroshortcourses.ku.edu/air UNIVERSITY OF KANSAS Mail KU Continuing Education Aerospace Short Course Program 1515 Saint Andrews Drive Lawrence, Kansas 66047-1619 • U.S.

Enroll Anytime Complete the registration form on the Refund We encourage you to send a qualified substitute back cover to enroll by mail or fax. To enroll online, visit if you cannot attend a course. If you wish to transfer into aeroshortcourses.ku.edu/air. another course you have one year from the original course Enrollment is limited and will be accepted in order of date to transfer and complete a short course or a refund will receipt. We recommend that you register as soon as possible automatically be issued. A full refund of registration fees will so that you can secure your place and we can prepare the be available if requested in writing and received two weeks proper amount of course material. Pre-registration is required before a course. After that date a refund will be made, less for your protection; otherwise, the course could be cancelled a $100.00 administrative fee. If no prior arrangements have due to insufficient enrollment. been made, no refunds will be made after 30 calendar days A confirmation letter will be emailed to each enrollee upon following the event. registration. If you prefer to receive the confirmation letter by mail or fax, please indicate your preference on the registration Cancellation Policy The University of Kansas Continuing form. If you do not receive a confirmation letter, please Education reserves the right to cancel any short course contact us. and return all fees in the event of insufficient registration, instructor illness or other unforeseen emergency situations. Fees/Billing All fees are payable in U.S. dollars and are The liability of the University of Kansas is limited to due at the time the class is held. Fees are listed on each course the registration fee. The University of Kansas will not page. be responsible for any losses incurred by the registrants We accept MasterCard, VISA, Discover and American including, but not limited to, airline cancellation charges or Express. Please note for security reasons we cannot accept hotel deposits. credit card information via email. You may mail a check in U.S. dollars to the address listed Privacy Policy KU Continuing Education does not share, above. Please make checks payable to “The University of sell, or rent its mailing lists. You have our assurance that any Kansas”. If you have received an invoice number, please information you provide will be held in confidence by KU include it on your check. If no invoice number is available, Continuing Education. please reference “KU Aerospace Continuing Education” on We occasionally use mailing lists that we have leased. If you your check. receive unwanted communication from KUCE, it is because You may make a wire transfer payment in U.S. dollars to your name appears on a list we have acquired from another US Bank of Lawrence, 900 Massachusetts, Lawrence, Kansas source. In this case, please accept our apologies. 66044, U.S. In the wire transfer you must reference “KU Aerospace Continuing Education” and include your invoice Nondiscrimination Policy The University of Kansas number. You are responsible for paying any bank transfer fees. prohibits discrimination on the basis of race, color, ethnicity, For account and ACH or routing numbers, please call 785- religion, sex, national origin, age, ancestry, disability, status as 864-5823 or email [email protected]. You must be registered a veteran, sexual orientation, marital status, parental status, in a course before requesting bank transfer information. gender identity, gender expression and genetic information in the University’s programs and activities. The following person Late Payment Fee All course fees are due at the time has been designated to handle inquiries regarding the non- the class is held. KU allows a 30-day grace period. Any fees discrimination policies: Director of the Office of Institutional that remain unpaid after 30 days following the class will be Opportunity and Access, [email protected], 1246 W. Campus Road, assessed a late fee of $100.00. Room 153A, Lawrence, KS, 66045, (785)864-6414, 711 TTY.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 8

Group Discounts Group discounts are available for companies registering more than two people for the same course at the same time. All participants eligible for the discount must be billed together on the same invoice. The discount rates are as follows: 2–4 people 5% discount 5–9 people 10% discount 10–14 people 15% discount 15+ people 20% discount If you have more than 10 people, ask about our on-site program. For more information, see page 11. All discounts must be requested at the time of registration and ALL registration forms must be submitted together to receive the discount. We are unable to register groups on-line. Please copy the registration form on the back of this catalog or download registration forms from our website. Send completed registration forms together by mail, fax, or scan and submit them via email. Please do not send credit card information by email. If you have any questions or if you need assistance, please call 785-864-5823 or toll-free within the U.S. 877-404-5823. The group discount cannot be combined with any other course discount.

Course Information KU Aerospace Short Courses is Now Mobile! Location The public course venues are listed on pages 5 This year we launched our new award-winning mobile site and 6. When you register for a course, the location will which is optimized for smartphones and smaller tablets. Our be included in the confirmation letter. aim is to provide the best possible user experience for reading Program Accessibility We accommodate persons with and accessing our content, whatever your device. We have disabilities. Please call 785-864-5823 or email ceipeinfo@ built our mobile site from the ground up, focusing on user ku.edu, and a KU Continuing Education representative interface, reliability, convenience and download speed. will contact you to discuss your needs. To ensure Try it today. accommodation, please register at least two weeks before the start of the event. See the nondiscrimination policy on page 7. Scan to bookmark Course Schedule The University of Kansas Continuing or visit us at Education and/or its instructors reserve the right to adjust aeromobile.continuinged.ku.edu course outlines, schedules and/or materials. Course times and total hours are approximate and may be adjusted by the instructor(s) as the situation warrants. Instructors The University of Kansas Continuing Education reserves the right to substitute an equally qualified instructor in the event of faculty illness or other circumstances beyond its control. If an equally qualified instructor is not available, the course will be cancelled. Audio or Video Recording Audio or video recording is not permitted in the classroom. Join us in a conversation on aerospace training Certificate of Attendance A certificate of achievement opportunities on LinkedIn at http://www.linkedin.com/ will be awarded to each participant who is present for 100 groups/KU-Aerospace-Short-Courses-3836449 percent of the course. KU Aerospace Short Courses group on LinkedIn provides Continuing Education Units (CEUs) are assigned for each opportunities for networking, idea exchanges and course and are listed on each course page. CEUs may not be training suggestions among the alumni and friends of this used for college credit. short-course program. All alumni are encouraged to join. Attending an aerospace short course expands your knowledge and increases your effectiveness and productivity in the workplace.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 9 CERTIFICATES OF SPECIALIZATION Enhance Your Knowledge—Advance Your Career

Certificates of specialization are for people who Or, you can contact us and we will send you an desire concentrated study in a specific area of application form. Upon approval of your application, interest. Achieving a certificate of specialization you will receive a special certificate of achievement. demonstrates to employers, coworkers and the aerospace industry that you are qualified, competent There is no fee required to receive a certificate of and current in your field. It distinguishes you as a specialization. The University of Kansas Aerospace professional who is committed to your career and Short Course Program is pleased to promote your strives to be the best. commitment to the industry.

Completion Requirements If you have questions or need assistance, please You can earn a certificate in one of eight specialized contact us: areas by completing four courses in a specialization Phone 785-864-5823 or toll-free within the U.S. track. 877-404-5823 Email [email protected] To apply for a certificate of specialization, complete and return the application form that can be found on our website at aeroshortcourses.ku.edu/air.

Aerospace Compliance Track Aircraft Design Track

• Aircraft Icing: Meteorology, Protective Systems, • Aerodynamic Design Improvements: High-Lift and Instrumentation and Certification–p. 18 Cruise–p. 14 • Commercial Aircraft Safety Assessment and 1309 • NEW Aerodynamic Design of Transport Aircraft–p. 15 Design Analysis–p. 28 OR Reliability and 1309 Design • Airplane Flight Dynamics: Open and Closed Loop–p. 23 Analysis for Aircraft Systems (Online Course)–p. 54 • Airplane Preliminary Design–p. 25 • NEW Electrical Wiring Interconnect System (EWIS) • Airplane Aerodynamic Design and Subsonic Wind and FAA Requirements –p. 34 Tunnel Testing–p. 22 • FAA Certification Procedures and Airworthiness • Conceptual Design of Unmanned Aircraft Systems–p. 31 Requirements as Applied to Military Procurement of • Principles of Aeroelasticity–p. 50 Commercial Derivative Aircraft/Systems–p. 36 • Principles of Aerospace Engineering–p. 51 • FAA Conformity, Production and Airworthiness • Propulsion Systems for UAVs and General Aviation Certification Approval Requirements–p. 37 Aircraft–p. 53 • FAA Functions and Requirements Leading to • NEW Stress Analysis for Aerospace Structures–p. 58 Airworthiness Approval–p. 38 • FAA Parts Manufacturer Approval (PMA) Process for Aviation Suppliers–p. 39 • FAR 145 for Aerospace Repair and Maintenance Organizations–p. 40 • Sustainment and Continued Airworthiness for Aircraft Structures–p. 61

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 10

Aircraft Maintenance and Safety Track Flight Control Systems Design Track

• Aircraft Engine Vibration Analysis, Turbine and • Applied Nonlinear Control and Analysis–p. 26 Reciprocating Engines: FAA Item 28489–p. 17 • Digital Flight Control Systems: Analysis and Design– • Aircraft Icing: Meteorology, Protective Systems, p. 32 Instrumentation and Certification–p. 18 • Flight Control Actuator Analysis and Design–p. 41 • Aviation Weather Hazards–p. 27 • Flight Control and Hydraulic Systems–p. 42 • Commercial Aircraft Safety Assessment and 1309 • Modelling and Analysis of Dynamical Systems: A Design Analysis–p. 28 OR Reliability and 1309 Design Practical Approach–p. 48 Analysis for Aircraft Systems (Online Course)–p. 54 • Durability and Damage Tolerance Concepts for Aging Aircraft Structures (Online Course)–p. 33 Flight Tests and Aircraft Performance Track • NEW Electrical Wiring Interconnect System (EWIS) and FAA Requirements–p. 34 • Aircraft Engine Vibration Analysis, Turbine and • FAR 145 for Aerospace Repair and Maintenance Reciprocating Engines: FAA Item 28489–p. 17 Organizations–p. 40 • Advanced Flight Tests–p. 13 • Sustainment and Continued Airworthiness for Aircraft • Airplane Flight Dynamics: Open and Closed Loop–p. 23 Structures–p. 61 • Airplane Performance: Theory, Applications and Certification–p. 24 • Flight Test Principles and Practices–p. 43 Aircraft Structures Track • Flight Testing Unmanned Aircraft—Unique Challenges–p. 44 • Aircraft Structural Loads: Requirements, Analysis, • Operational Aircraft Performance and Flight Test Testing and Certification–p. 20 Practices–p. 49 • Aircraft Structures Design and Analysis–p. 21 • Principles of Aeroelasticity–p. 50 • Structural Composites–p. 59 • Rotorcraft Vibration: Analysis and Practical Reduction • Sustainment and Continued Airworthiness for Aircraft Methods–p. 55 Structures–p. 61

Management and Systems Track Avionics and Avionic Components Track • Aerospace Applications of Systems Engineering–p. 16 • Aircraft Lightning: Requirements, Component Testing, • NEW Commercial Space—What It Means and the Issues Aircraft Testing and Certification–p. 19 It Raises–p. 29 • Complex Electronic Hardware Development and • NEW Essentials of Effective Technical Writing for DO-254–p. 30 Engineering Professionals–p. 35 • Fundamental Avionics–p. 45 • Process-Based Management in Aerospace: Defining, • NEW Electrical Wiring Interconnect System (EWIS) Improving and Sustaining Processes–p. 52 and FAA Requirements–p. 34 • Fundamentals of Project Management for Aerospace • Integrated Modular Avionics (IMA) and DO-297–p. 47 Professionals–p. 46 • RTCA DO-160 Qualification: Purpose, Testing and • Subcontract Management in Aerospace Organizations– Design Considerations–p. 56 p. 60 • Software Safety, Certification and DO-178C–p. 57 • Unmanned Aircraft System Software Airworthiness– p. 62

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 11 ON-SITE AEROSPACE SHORT COURSES Realize substantial savings by bringing our outstanding courses to your workplace.

Our 2014 short courses are available Frequently Asked Questions Industry Leaders Who Have for on-site presentations. Let us bring Where can you provide in-house Supported the KU Aerospace our world-class instructors and the training? training you need to your workplace. Short Course Program Anywhere in the world, except U.S. Airbus Benefits of KU Aerospace embargoed countries or travel warning BAE Systems On-Site Training countries listed by the U.S. Department Beechcraft Corporation of State. Bell Helicopter Textron When you choose the KU Aerospace The Boeing Company Short Course Program for your on-site What does the company provide? training, you: Bombardier You provide the attendees, a classroom CAAC—Civil Aviation Administration • Train when it fits your schedule and audio-visual equipment such as a of China • Train more people projector and a screen. We will send Cessna Aircraft Company • Incur lower costs per participant you a description of the course needs COMAC—Commercial Aircraft • Save employee travel expenses in advance to prepare for the class. If Corporation of China, LTD. • Reduce the time employees are away you cannot provide a classroom, we DAPA—Defense Acquisition Program from work can set up a course at a nearby hotel Administration • Train as a team to enhance project management or conference center for an additional DCA-BR—Organização Brasileira para charge. o Desenvolvimento da Certificação Aeronáutica Contact the On-site What does KU provide? Embraer-Empresa Brasileira de Program Manager KU provides the instructor’s Aeronáutica S.A. Obtain a no-cost, no-obligation honorarium, his or her travel, all European Aviation Safety Agency proposal for an on-site course. course materials, shipping and customs Federal Aviation Administration charges, certificates with CEUs for Garmin Phone 785-864-8282 participants who attend all days, GE Aviation Fax 785-864-5074 course evaluation and coordination. General Atomics Email [email protected] Goodrich Corporation How is an on-site course price Gulfstream Aerospace Corporation determined? Honeywell, Inc. The courses listed below are only Lockheed Martin Corporation available for on-site delivery, and To make it cost effective for all Lycoming Engines are not available as public courses in parties, we base our course fees on NASA 2014. These courses and ALL of our 20 participants and offer substantial public courses can be brought to your discounts for each additional National Aerospace Laboratory of company for on-site delivery. participant. We also have worked with The Netherlands New Zealand Defence Force • Aerodynamic Design Improvements: organizations to form consortia with other area companies to share costs. Northrop Grumman Corporation High-Lift and Cruise Pilatus Aircraft Ltd. • Aerospace Applications of Systems The course fee of an on-site class depends on the instructor’s QinetiQ Ltd. Engineering Rockwell Collins • Applied Nonlinear Control and honorarium, the instructor’s travel SAAB Aircraft AB Analysis reimbursements, the cost of the course • FAA Parts Manufacturer Approval materials specific for that class and the Samsung (PMA) Process for Aviation Suppliers shipping costs of the course materials. Sierra Nevada Corporation • FAR 145 for Aerospace Repair and Sikorsky Aircraft Corporation Maintenance Organizations How far in advance do you need to Spirit AeroSystems • Flight Control Actuator Analysis and schedule a course? SR Technics STM—Savunma Teknolojileri Design In order to schedule the instructor and Mühendislik • Modelling and Analysis of Dynamical order the course materials, we request Systems: A Practical Approach Transport Canada at least 8 to 12 weeks of lead time prior • Process-Based Management in United States Department of Defense to the actual course date. Aerospace: Defining, Improving and (Air Force, Army, Navy and Coast Sustaining Processes Guard) • Propulsion Systems for UAVs and General Aviation Aircraft • Subcontract Management in Aerospace Organizations aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 12 COURSE DELIVERY OPTIONS

Online Courses Video Conferencing Now you have the opportunity to further your training The Aerospace Short Course Program can provide various without worrying about time away from work or family and video conferencing solutions for companies to take advantage the costs of traveling. of when determining training needs for their employees. Our video classroom at the KU Continuing Education building When you register for an online course from the Aerospace allows you to reach as many as eight international locations Short Course Program you will have six months to complete simultaneously and in real time, as well as save thousands of the course at your own pace. Each course will have a project dollars in travel expenses. Staff will be available and on hand or case study to complete during the duration of the course. at all times. Once the project or case study is completed satisfactorily you will be awarded a certificate for instructional hours and In addition to our video conference classroom, we can provide Continuing Education Units (CEUs). various web-based solutions to assist in your on-site training needs. We can host a course through our Adobe ConnectPro The Aerospace Short Course Program is pleased to offer the format or work with your company’s internal conferencing following online courses. systems to provide a blended delivery option to several • Airplane Performance: Theory, Applications and different locations. Certification–p. 24 • Durability and Damage Tolerance Concepts for Aging Aircraft Structures –p. 33 • Reliability and 1309 Design Analysis for Aircraft Systems– For more information, p. 54 contact [email protected]

We are committed to developing more on-line courses in the future.

Dr. Jan Roskam’s online Airplane Performance: Theory, Applications and Certification course

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 13 California, Maryland ADVANCED FLIGHT TESTS Instructors: Donald T. Ward, Thomas William Strganac

Day One • Experimental tools for preflight Offering Location preparation: water tunnel tests and flow Location California, Maryland • Why such tests are necessary; philosophy and attitudes, overview visualization tools, static wind tunnel Date June 9–13, 2014 of documents describing governing tests, dynamic wind tunnel tests, rotary balance tests Course Number AA141410 regulations, history • Fundamental principles of aeroelasticity: Day Four Times/CEUs description of static and dynamic • Instrumentation for post-stall flight aeroelastic phenomena; definitions, tests: sensors needed and their Monday–Thursday 8 a.m.–4 p.m. terminology and assumptions; limitations specifications; pre-test planning and Friday 8 a.m.–2 p.m. of theory; flutter analysis; development of preparation: data requirements, flight basic aeroelastic equations; interpretation Class time 33 hours test team preparation and training, of supporting analyses flight simulation; maneuver monitoring CEUs 3.3 • Experimental and analytical tools in real time for envelope expansion used in preflight preparation: modal • Emergency recovery devices: types Description methods, ground vibration tests and of devices available, sizing and other analysis, wind tunnel test techniques, design constraints, validation Provides practical knowledge interpretation of dynamically similar needed to plan a series of flutter • Subsystem modifications for post- wind tunnel model data envelope expansion tests safely and stall testing: additional pilot restraint comprehensively. Includes suggestions Day Two devices, control system modifications, and recommendations for flutter • Instrumentation for flutter envelope propulsion system modifications and post-stall certification and • Recommended recovery techniques; demonstration of new or significantly expansion: suitable sensors, near real- modified airplane designs to meet civil time data analysis interpreting post-stall flight test results: or military requirements. • Subcritical response techniques, analyzing real-time data, postflight interpretation of supporting analyses analysis of data Day Five Target Audience • Interpreting test results: analyzing real- time data, postflight analysis of data • Guidelines and discipline for Designed for practicing and entry-level conducting advanced flight tests: test flight test engineers and managers, • Expanding the envelope: excitation team training, incremental buildup to aircraft engineers and aircraft methods, clearance to 85 percent flutter critical conditions, use of simulation, designers. envelopes, example programs independent review teams • Discussions of limit cycle oscillations • Planning for efficiency in data Fee Day Three collection and data management: $2,445 • Foundations of post-stall flight testing: tailoring the scope of the tests to the requirement; identifying critical parts Includes instruction, a course notebook, definitions of stall, departure, post-stall of the envelope; combining maneuvers Introduction to Flight Test Engineering, gyrations and spins; description of spin and integration of backup test points; Volumes I and II, by Don Ward, Thomas modes and spin phases; development of Strganac and Rob Niewoehner, and a large disturbance equations of motion; using all available tools: real-time CD including AGARD Report #776 Aircraft idealized flight path in a spin; balance monitoring, automated inserts; shared Dynamics at High Angles of Attack, of aerodynamic and inertial forcing data processing between test site and refreshments and five lunches. functions; autorotation and its causes; home site The course notes are for participants effect of damping derivatives; effect • Contingency planning: attrition of only and are not for sale. of mass distribution; simplification of resources, backup support facilities, post-stall equations of motion safety guidelines and documentation; • Aerodynamic conditions for dynamic course wrap-up and critique Certificate Track equilibrium: pitching moment This course is part of the Flight Tests equilibrium, rolling and yawing and Aircraft Performance Track. See moment equilibrium; design goals and page 10. trends to provide post-stall capability: agility measures of merit, unsteady lift, thrust vector control, vortex control aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 14 AERODYNAMIC DESIGN IMPROVEMENTS: HIGH-LIFT AND CRUISE Instructors: C.P. (Case) van Dam, Paul Vijgen

Day One Day Four Offering Available as on-site course • Aircraft design and the importance of • High-lift physics of swept and unswept Contact us for a no-cost, no obligation drag on fuel efficiency, operational cost single-element wings proposal for an on-site course: and the environmental impact • Physics of three-dimensional high- On-site Program Manager • Empirical drag prediction including scale lift systems including features of 3D Email [email protected] effects on aircraft drag and examples of high-lift flows and lessons from high Phone 785-864-8282 drag estimates for several aircraft Reynolds number tests • History of laminar flow for drag • Importance of boundary-layer reduction transition, relaminarization and Times/CEUs • Natural laminar flow design, roughness (icing, rain) effects on high- Class time 35 hours lift aerodynamics application, certification and viability CEUs 3.5 • Laminar flow control, hybrid laminar • Overview and survey of high-lift flow control design and application systems; types of high-lift systems considerations including suction system including support and actuation Description considerations systems Covers recent advances in high- lift systems and aerodynamics as • CFD-based drag prediction and • High-lift computational aerodynamics decomposition methods well as cruise drag prediction and Day Five reduction. Includes discussion of Day Two numerical methods and experimental • Critical factors in CFD-based • Passive and active flow separation techniques for performance analysis prediction control of wings and bodies and boundary- layer transition prediction/detection. • Boundary-layer transition prediction • Conceptual studies of high-lift and analysis ranging from empirical to systems including multi-disciplinary approaches Parabolic Stability Equation (PSE) and Target Audience Direct Numerical Simulation (DNS) • High-lift characteristics of techniques unconventional systems and Designed for engineers and managers involved in the aerodynamic design • Supersonic laminar flow including configurations including canard and tandem-wing configurations, Upper and analysis of airplanes, rotorcraft boundary-layer instability, transition and other vehicles. mechanisms and control methods at Surface Blowing (USB), Externally supersonic speeds Blown Flaps (EBF) and Circulation Control Wings (CCW) • Wave drag reduction at transonic and Fee supersonic conditions • High-lift flight experiments involving general aviation and transport type Includes instruction and a course • Passive and active methods for airplanes notebook. turbulent drag reduction • Final observations The course notes are for participants Day Three only and are not for sale. • Induced-drag reduction ranging from classic linear theory to active reduction Certificate Track concepts including wingtip turbines This course is part of the Aircraft and tip blowing Design Track. See page 9. • Experimental techniques for laminar and turbulent flows • Impact of high-lift on performance and economics of general aviation and subsonic transport aircraft • Physics of single-element airfoils at high-lift including types of stall characteristics, Reynolds and Mach number effects aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 15 Seattle AERODYNAMIC DESIGN OF TRANSPORT AIRCRAFT (NEW) Instructor: Roelof Vos

Day One: Introduction and • Design considerations for pressure Offering Location review of aerodynamic distributions on finite swept wings Location Seattle, Washington fundamentals: • Discussion of examples of modern Date April 28–May 2, 2014 swept-wing designs • Introduction, classification, design Course Number AA141330 requirements and objectives of Day Four: Empennage transport aircraft, certification design, control surface Times/CEUs regulations and design rules, general goals in aerodynamic design design and engine Monday–Friday 8 a.m.–4 p.m. integration: • Boundary-layer aerodynamics and Class time 35 hours subsonic cruise drag • Horizontal tail surface design: CEUs 3.5 functions and requirements, • Relation between supervelocity planform shape, aeroelastic effects, and pressure coefficient. Relation elevator lock Description between geometry and pressure distribution • Vertical tail surface design: Examines how the exterior design of high- functions and requirements, subsonic transport aircraft can be manipulated • Interference drag and area ruling planform shape, effect of dorsal fin in order to meet specified performance objectives and satisfy relevant certification Day Two: Airfoil design: • Control surface design: functions constraints. The course covers which geometric and requirements, linearity, characteristics of the airplane allow for a high • Pressure distribution on airfoil operating Mach number while keeping fuel sections at high and low speed. aeroelasticity, stall burn at acceptable levels, demonstrates how Development of the transonic airfoil • Spoiler panels: functions, effect on the exterior of all major airplane components can be shaped so as to adequately handle low- • Design of supercritical and sonic pressure distribution, interaction subsonic and high-subsonic flow, and shows airfoils. Reynolds number effects with flaps how aerodynamic design and operation at low and high speeds affect the airplane in terms of • Low-speed stalling characteristics of • Engine intake design: lip design for balance, stability, aeroelastic behavior, weight, airfoil sections take-off and cruise conditions, drag controllability, cruise performance, and field in OEI condition. Exhaust design: performance. Through many historic and • Reynolds number and Mach number effect of ambient pressure, boat contemporary examples, the participant will effects on maximum lift coefficient learn to relate the functions of high-subsonic tail drag. Thrust reversers: types, transport aircraft to their external design. • High-speed stall (buffet) on airfoil interference with empennage sections Day Five: Operation: Target Audience • Airfoils equipped with high-lift devices: mutual interaction, types of • Stalling characteristics of full Designed for aeronautical engineers, pilots with flow separation scale aircraft: stall requirements, some engineering background, government mechanism complexity vs. research laboratory personnel, engineering Day Three: Wing design: maximum lift coefficient, spanwise managers and educators. • Wing requirements stall onset, deep stall • Development of the swept-wing • Take-off performance: requirements, Fee concept: historical background, minimum unstick speed, lift-to-drag $2,445 principle of wing sweep, transonic ratio in take-off and landing Includes instruction, a course notebook, flow characteristics, effect on • The buffet onset boundary: Aerodynamic Design of Transport Aircraft, by Ed boundary layer, effect on maximum requirements, effect on flight Obert, refreshments and five lunches. lift coefficient, fences envelope. Flight characteristics The course notes are for participants only and • First generation of swept wing between MMO and MD: are not for sale. aircraft: tip-stall, aeroelastic requirements, Mach tuck, Mach deformation trim compensation Certificate Track • Pressure distribution on finite swept wings: spanwise drag distribution, This course is part of the Aircraft Design forward sweep, fuselage interference, Track. See page 9. improving velocity distribution at root and tip, minimizing pitching moment aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 16 AEROSPACE APPLICATIONS OF SYSTEMS ENGINEERING Instructors: Donald T. Ward, Mark K. Wilson, D. Mike Phillips

Day One Day Four Offering Available as on-site course • Systems engineering: overview and • Integrated logistics support Contact us for a no-cost, no obligation terminology • Cost effectiveness analysis proposal for an on-site course: • Generic system life cycles • Electromagnetic compatibility analysis On-site Program Manager • System hierarchy • Environmental impact analysis Email [email protected] Phone 785-864-8282 • Systems of systems • Interoperability analysis • Value of systems engineering • Life-cycle cost analysis Times/CEUs • Life cycle stages and characteristics • Manufacturing and producibility • Tailoring concepts analysis Class time 35 hours Day Two • Mass properties engineering analysis CEUs 3.5 • Requirements: definition, elicitation • Safety and health hazard analysis and analysis • Sustainment engineering analysis Description • Architectural design process • Training needs analysis Based on evolving systems engineering standards, EIA/IS 632 and IEEE P1220 • Evolutionary acquisition, spiral • Usability analysis/human systems and the current version of the INCOSE development and open systems integration Systems Engineering Handbook. Provides • Implementation process a working knowledge of all elements, • Value engineering technical and managerial, involved • Integration process • Applying systems engineering in a in systems engineering as applied to • Verification process “lean” environment (NASA X-38 case aerospace systems of varying complexity. study) Concentrates on the most troublesome • Transition process areas in systems development: • Class exercise requirements derivation, integration, • Validation process allocation of requirements, verification • Operation process Day Five and control. Hardware and software systems case studies, primarily from the • Maintenance process • Software intensive systems engineering (lessons learned) aircraft sector of the aerospace industry • Disposal process are used as examples. Techniques have • Intensive systems engineering (case been used on many commercial (both • Cross-cutting technical methods studies) large airliners and smaller personal aircraft), DoD, and NASA programs. Day Three • Course summary and wrap-up • Project planning process Target Audience • Project assessment and control process Designed for systems engineers at all • Decision management process levels and program managers developing • Risk management process large or small systems. • Configuration management process • Information management process Fee • Measurement process Includes instruction and a course notebook. • Acquisition process The course notes are for participants • Supply process only and are not for sale. • Life cycle model management process • Infrastructure management process Certificate Track • Project portfolio management process This course is part of the • Human resource management process Management and Systems Track. See • Quality management process page 10. • Tailoring process aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 17 San Diego AIRCRAFT ENGINE VIBRATION ANALYSIS, TURBINE AND RECIPROCATING ENGINES: FAA ITEM 28489 Instructor: Guil Cornejo

Day One Day Three Offering Location Location San Diego, California • Review: ABCs of shaft lateral/ • Bearing Babbitt tension, bonding, torsional vibration and phase: time, temperature, load/temperature Date September 15–19, 2014 frequency and modulation domains; hysteresis and fatigue life; Course Number AA151130 natural and forced-coupled arcing and cavitations damage;, vibrations’ elastic and plastic limits crankshaft balance grades and temperature dependence; • Propeller static/dynamic balance, Times/CEUs damping; orbit’s equilibrium; safe prop-balance analyzer, prop mode Monday–Friday 8 a.m.–4 p.m. minimum film thickness, log-dec, shapes, engine frame resonance; rotor whirl, Bode and polar plots Class time 35 hours turbocharger • Classification of vibration and CEUs 3.5 acoustic signals Day Four/Five • Measurements: sensors, • Turbine engine: aircraft engine Description instrumentation and digital design survey, turbojet, turbofan, turboprop and turboshaft The objective of this five-day course is to demystify signal technology’s A/D converter process-vibration concepts to practical remediation process to measure and to analyze • Antifriction bearings, stiffness, tools for resolving and mitigating aircraft engine rotating shaft vibrations damping, orbit root, life, bearing and gearbox vibrations. The course consists of • Optimum vibration load arc and matching four modules: review, measurements, turbine, and reciprocating engine process-vibration instrumentation: oscilloscope, FFT • Rotordynamic direct and analysis and mitigation. In the course, both roller and modulation analyzers cross-coupled instability, and hydrodynamic bearings orbit behavior are • Sensor’s mechanical mounting, damping, gyroscopic; roller and reviewed. Animations depict and simplify both hydrodynamic bearings’ failure; crankshaft and rotor-orbit’s stability metrics and temperature and frequency range how they relate to either spectral signature and limits torsional and lateral vibrations’ to oscilloscope orbits. Stiff, slender, overhung measurements; rotor fatigue rotor and gyroscopic effects are animated to show Day Two • Epicyclical/parallel load gearbox bearing-shaft stiffness reactions; both journal and • Reciprocating engine mechanical bearing-cap orbit behaviors are examined. Roots of vibrations and sidebands vibration sources: power-impulse engine lateral and torsional vibrations and fatigue • Blades and vanes, damping and inertia coupled forces, journal are practically considered. Excel programs for first coatings, resonance/temperature, level field troubleshooting are included. orbits; tappet resonance, star aerodynamic excitations, flutter, diagram and engine harmonics vortices, erosion, torsion, blade/ torsional excitations, damping vane interactions, missing blade; Target Audience and Holzet couplings; crank twist, blade crack detection Aircraft power-plant engineers, engineering bending and balancing; lubricant managers, senior technical personnel and educators cavitations • Shaft balancing: static, concerned with the health, safety, lifecycle and macrobalance and assembly • Reciprocating vibration sources: performance of aircraft power-plant rotating dynamic microbalance components. PV-timing diagrams, ignition, detonation imbalance, torsional/ • Combustor acoustic oscillations, lateral and tappet-clearance damage pulsation levels Fee vibration excitations and • Airborne noise measurements, imbalance $2,445 • Modal analysis Includes instruction, a course notebook, DVD of reference materials, refreshments and five lunches. The course notes are for participants only and are not for sale. What a participant can expect to learn: • practical mitigation of excessive aircraft engine process-vibration; Certificate Track • diagnostic and prognostic evaluation of aircraft engine vibrations; This course is part of the Aircraft Maintenance • demystify aircraft engine and gearing vibration analysis to practical level; and Safety Track and the Flight Tests and Aircraft Performance Track. See page 10. • familiarization with vibration troubleshooting instrumentation; • introduction to new and state-of-the-art blade crack detection. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Las Vegas 18 AIRCRAFT ICING: METEOROLOGY, PROTECTIVE SYSTEMS, INSTRUMENTATION AND CERTIFICATION Instructors: Wayne R. Sand, Steven L. Morris

Day One Offering Location • Icing hazard description Location Las Vegas, Nevada • Atmospheric aerosols Date March 4–7, 2014 • Cloud physics of icing Course Number AA141300 • Ground icing, atmospheric cooling mechanisms • Conceptual cloud modes: convective clouds, stratiform clouds Times/CEUs • Skew-T, Log P adiabatic diagrams Tuesday–Friday 8 a.m.–4 p.m. Day Two Class time 28 hours • Icing environment analysis using Skew-T, Log P CEUs 2.8 • Assessment of icing potential • Critical icing parameters, theory and measurements Description • Meteorology of supercooled large drops (SLD icing) Covers meteorology and physics of aircraft icing; forecasting, finding and • Finding/avoiding icing conditions avoiding icing conditions; designing • New and current icing research and evaluating ice protection systems • Internet resources and certification of aircraft for flight into known icing conditions. Day Three • Ice accretion characteristics Target Audience • Effects of ice on aircraft performance Designed for aerospace engineers, • Anti-ice systems flight test and design engineers, test pilots, line pilots, meteorologists, FAA • De-ice systems engineers, Designated Engineering • Icing instrumentation, icing environment Representatives (DERs) and program • Icing detection managers. Day Four Fee • Effect of SLD on aircraft $2,145 • Engine icing considerations Includes instruction, course and • Ice-testing methods reference notebooks, refreshments • Certification and regulations and four lunches. • Computational methods The course notes are for participants only and are not for sale. • Review and discussion

Certificate Track This course is part of the Aerospace “Very interesting and comprehensive Compliance Track and the Aircraft introduction to icing conditions and preventions. Maintenance and Safety Track. See The instructors are very experienced.” pages 9 and 10. — Zhe Yan, Engineer, Aircraft Integrator Bombardier Aerospace

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 19 Orlando AIRCRAFT LIGHTNING: REQUIREMENTS, COMPONENT TESTING, AIRCRAFT TESTING AND CERTIFICATION Instructors: C. Bruce Stephens, Ernie Condon This course may be taught by one or both instructors, based on their availability. Day One Day Four Offering Location Location Orlando, Florida • Introduction • Fuel systems Date November 17–21, 2014 • The electromagnetic environment of • 14 CFR 25.981, Amendment 102 aircraft Course Number AA151190 • Aircraft wiring and shielding • Metallic and composite aircraft • Electrical Wiring and Installation requirements System (EWIS) Times/CEUs • Electromagnetic Interference (EMI) Monday–Thursday 8 a.m.–4 p.m. • Electromagnetic Compatibility (EMC) Day Five Friday 8 a.m.–11:30 a.m. • Pre-selected teams will simulate • Electrical bonding Class time 31.5 hours the process of determining aircraft • Electrostatic Discharge (ESD) lightning certification and testing CEUs 3.15 • Prescription Static (P-STATIC) requirements for various components installed on the aircraft. • High Intensity Radiated Fields (HIRF) Description • Electromagnetic Effects (EME) • FAA certification process and program management This course provides details for direct requirements and indirect effects of aircraft lightning • Future EME testing techniques; Final testing and certification. Requirements EME discussion and questions for both composite and metallic Day Two aircraft, including proper RTCA/DO- • The lightning environment 160 classifications, are examined. The course will also include a high • The history of lightning requirements level overview of Electromagnetic for aircraft certification Compatibility (EMC), High Intensity Radiated Fields (HIRF), Precipitation • Aircraft lightning attachment Static (P-Static) and Electrical Bonding requirements. The new requirements of • Effects of lightning on aircraft Electrical Wiring and Installation System • Directs effects of lightning (EWIS) and Fuel Tank Safety (14 CFR 25.981 Amd. 102) will also be addressed. • Direct effects testing • RTCA/DO-160 levels for direct effects Target Audience testing This course is designed for all design • Direct effects certification requirements engineering disciplines, project • EASA requirements managers, project engineers and laboratory personnel whose aircraft • Simulation for direct effects “This course is very good, I have system may require protection from the requirements learned a lot about the theory, effects of lightning. application and certification. Perfect Day Three lectures and perfect teacher!” • Indirect effects of lightning Fee — Onsite participant $2,445 • Indirect effects aircraft level testing Includes instruction, a course notebook, • Indirect effects design refreshments and five lunches. • RTCA/DO-160 levels for indirect effects The course notes are for participants bench testing only and are not for sale. • Indirect effects certification requirements Certificate Track • EASA requirements This course is part of the Avionics and • Simulation for indirect effects Avionic Components Track. See requirements page 10. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Seattle and Orlando 20 AIRCRAFT STRUCTURAL LOADS: REQUIREMENTS, ANALYSIS, TESTING AND CERTIFICATION Instructor: Wally Johnson

Day One • Landing loads analysis (one wheel, Offering Locations two wheel, three wheel, landing code) • Introduction and overview of the Location Seattle, Washington course • Ground handling maneuver loads Date April 28–May 2, 2014 • Basic aerodynamics overview analysis (taxi, ground turn, nose- wheel yaw, braking, towing, jacking, Course Number AA141340 • Certification requirements (FAR 23, ground-loads code) FAR 25, EASA, MIL-SPECS) • Fatigue loads analysis (normal Location Orlando, Florida • Mass properties calculations (design operational conditions, missions, load Date November 17–21, 2014 weights, weight-c.g. envelope spectra) development, weight-c.g. code, mass Course Number AA151200 distribution code) Day Four • Structural design airspeeds • Wing loads analysis (design wing Times/CEUs derivations (maneuver, gust conditions, wing-load code) Monday–Thursday 8 a.m.–4 p.m. penetration, cruise, dive, flap • Horizontal tail loads analysis (HT Friday 8 a.m.–11:30 a.m. extended, design-airspeeds code) loads certification requirements, Class time 31.5 hours • V-n diagrams (maneuver and gust design HT conditions) load factors calculations, V-n diagram CEUs 3.15 • Vertical tail loads analysis (VT loads code) certification requirements, design VT Day Two conditions) Description • Introduction to external loads • Fuselage loads analysis (inertia loads, Provides an overview of aircraft structural external loads analysis, including: criteria, (definitions, static vs. dynamic, flutter, airloads, 1g shear curve, fuselage- loads code) design, analysis, fatigue, certification, loads classifications) validation and testing. It covers FAR 23 • Steady maneuvers (wind-up turn, pull- • Control surface and high-lift devices and FAR 25 airplane loads requirements. up, balancing tail loads derivations, loads analysis (cert requirements, However, the concepts may be applicable bal-maneuver code) primary and secondary surfaces, for military structural requirements. Loads flaps, spoilers, hinge moments, airload calculations examples using BASICLOADS • Pitch maneuvers analysis (abrupt pitch distributions) software will be demonstrated up, abrupt pitch down, checked pitch) throughout the course week. A copy of • Roll maneuver analysis Day Five BASICLOADS software will be provided to attendees. • Static and fatigue test loads Day Three • Flight loads validation (ground • Yaw maneuver and engine out analysis loads calibration, in-flight loads Target Audience • Basic structural dynamics overview measurements) Designed for practicing engineers • Course summary and wrap-up and engineering managers whose • Static and dynamic gust analysis (gust responsibilities include aircraft structures. load factor formula, tuned discrete 1-cos gust, PSD gust) Fee $2,445 Includes instruction, a course notebook, a copy of BASICLOADS software, A participant can expect to learn: refreshments and five lunches. • the basics of aerodynamics, weights and structural dynamics; The course notes are for participants only and are not for sale. • how the structural loads are developed; • how the loads group interacts with other groups; • commercial loads certification requirements; Certificate Track This course is part of the Aircraft • the various types of loads conditions; Structures Track. See page 10. • the flight and ground testing requirements. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 21 Seattle and Orlando AIRCRAFT STRUCTURES DESIGN AND ANALYSIS Instructors: Michael Mohaghegh, Mark S. Ewing This course may be taught by one or both instructors, based on their availability.

Day One Day Four Offering Locations Location Seattle, Washington • Structural design overview: evolution • Design to buckling and stiffness: of structural design criteria; FAA buckling of thin-walled structures; Date April 28–May 2, 2014 airworthiness regulations; structural design exercise Course Number AA141350 design concepts, load paths • Component design: wings and • Design requirements and validation empennages, fuselage, landing gear, Location Orlando, Florida of aircraft loads: materials and engine attachments, control surfaces fasteners, flutter and vibrations, static Date November 17–21, 2014 strengths, durability, fail safety and Day Five Course Number AA151210 damage tolerance, crashworthiness, • Design for damage tolerance: historical producibility, maintainability and context of safe life, fail safety and Times/CEUs environment/discrete events damage tolerance; tolerating crack Monday–Friday 8 a.m.–4 p.m. growth in structures; widespread Day Two damage; testing; inspection; design Class time 35 hours • Metals: Product forms, failure modes, exercise CEUs 3.5 design allowables testing, cyclic loads; • Design for durability: fatigue, corrosion processing • Design considerations: design Description • Fiber-reinforced composites: laminated for manufacture, design process composite performance; failure management Introduction to analysis and design of modes and properties; processing; aircraft structures, including design environmental protection • Certification: analysis and validation criteria, structural design concepts, requirements, component and full-scale loads and load paths, metallic and • Material selection: aluminum, titanium, aircraft testing requirements composite materials; static strength, steel, composites and future materials; buckling and crippling, durability and design exercise • Continued airworthiness: aging fleet, damage tolerance; practical design repairs considerations and certification and Day Three repairs. Analysis exercises and a design project are included to involve students • Design to static strength: highly loaded in the learning process. tension structures; combined loads • Mechanical joints; bonded and welded joints; lugs and fittings; design exercise Target Audience • Thin-walled structures: review of Designed for engineers, educators and engineering managers whose bending and torsion for compact responsibilities include aircraft beams; introduction to shear flow structures. analysis of thin-walled beams; analysis exercise; semi-tension field beams; design exercise; introduction to the Fee finite element method $2,445 Includes instruction, a course notebook, refreshments and five lunches. The course notes are for participants only and are not for sale. A participant can expect to learn: • primary requirements for certifiable structural design: static strength, durability and Certificate Track damage tolerance, and how these requirements impact design; This course is part of the Aircraft • to recognize the critical role validation plays in both design and analysis; Structures Track. See page 10. • to describe similarities and differences between composite and metallic structures; • to compare and contrast classical analysis methods with FEA to determine the appropriate application. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Las Vegas 22 AIRPLANE AERODYNAMIC DESIGN AND SUBSONIC WIND TUNNEL TESTING Instructor: Willem A.J. Anemaat

Day One Day Three Offering Location • Introduction to aerodynamics • Longitudinal stability and control Location Las Vegas, Nevada • Introduction to Lift, Drag and • Directional stability and control Date March 3–7, 2014 Moment • Lateral stability and control Course Number AA141260 • Review of drag polar breakdown • Trim, how to use wind tunnel data for subsonic airplanes, rapid to check for trimmability method for drag polar prediction, Times/CEUs check of drag polar realism • Ground effects Monday–Friday 8 a.m.–4 p.m. • Wind tunnel facilities • Airfoils Class time 35 hours • Wings • Scaling forces and moments to full scale CEUs 3.5 • Flaps • Other tests • Introduction to wind tunnel Description testing • Flow visualization: examples This course deals with wind tunnel test specifics • Measurements: what to measure Day Four on how to set up a test, how to run tests, what is and how • Landing gears involved with testing from a test management • Calibration and engineering point of view, how to design • Winglets • Forces and moments the test models and what it is used for in the measurements • Dorsal fins aerodynamic design of airplanes. The course deals with data analysis and how to correct it to • Pressure measurements • Ventral fins full-scale airplanes. • Scale effects, Reynolds number • Nacelles effects • Inlets Target Audience • T-strips Day Two Aeronautical engineers, researchers, • Test plan setup • Brakes and spoilers government research laboratory personnel, • Trip strips • Miscellaneous components engineering managers and educators who • Component build-up are involved with research, development and • Changes to the test plan design of subsonic aircraft or modifications to • Test management • Engine intakes, exhausts aircraft. • Model changes • Propellers/power effects, propwash effects on components. Propeller • Lift sizing for wind tunnel testing Fee • Drag $2,445 Day Five • Pitching moment Includes instruction, a course notebook, Low- • Model design Speed Wind Tunnel Testing, Third Edition, by • Downwash • Pressure distributions Jewel B. Barlow; Airplane Aerodynamics and • Stall Performance, by C. Edward Lan and Jan Roskam; • Pressure distribution on finite • Deep stall wings and Aerodynamic Design of Transport Aircraft, by Ed Obert, reference materials, refreshments and • Subsonic cruise drag and L/D and five lunches. range The course notes are for participants only and • Exercise: setup a small wind are not for sale. tunnel test program • Analyzing wind tunnel test data. Hands-on exercise using wind Certificate Track tunnel data This course is part of the Aircraft Design Track. • Summary See page 9. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 23 Orlando AIRPLANE FLIGHT DYNAMICS: OPEN AND CLOSED LOOP Instructor: Willem A.J. Anemaat

Day One • Applications of the perturbed state equations Offering Location of motion—complete and approximate • The general airplane equations of motion: longitudinal transfer functions; short period, Location Orlando, Florida reduction to steady state and to perturbed state phugoid, third mode, connections with static motions; emphasis: derivation, assumptions Date November 17–21, 2014 longitudinal stability, sensitivity analyses, and applications Course Number AA151220 equivalent stability derivatives; complete • Review of basic aerodynamic concepts: and approximate lateral-directional transfer airfoils—lift, drag and pitching moment, lift- functions—roll mode, spiral mode, Dutch roll Times/CEUs curve slope, aerodynamic center; Mach effects; mode and lateral phugoid, connections with fuselage and nacelles—destabilizing effect in static lateral-directional stability, sensitivity Monday–Friday 8 a.m.–4 p.m. pitch and in yaw; wings, canards and tails—lift, analyses, equivalent stability derivatives Class time 35 hours drag and pitching moments; lift-curve slope; aerodynamic center; downwash; control power Day Four CEUs 3.5 • Longitudinal aerodynamic forces and • Review of flying qualities criteria; MIL-F- moments: stability and control derivatives for 8785C and FARs, Cooper-Harper ratings, Description the steady state and for the perturbed state, relation to system redundancy and the example applications and interpretations airworthiness code Overview of airplane static and • Introduction to Bode plots and the root-locus dynamic stability and control Day Two method theory and applications, classical • Lateral-directional aerodynamic forces and • Introduction to human pilot transfer moments: stability and control derivatives for control theory and applications to functions; analysis of airplane-plus-pilot-in- the steady state and for the perturbed state, airplane control systems. the-loop controllability; synthesis of stability example applications and interpretations augmentation systems—yaw dampers, pitch • Thrust forces and moments: steady state and dampers; effect of flight condition, sensor Target Audience perturbed state orientation and servo dynamics Designed for aeronautical, • The concept of static stability: definition, control system and simulator implications and applications Day Five engineers, pilots with engineering • Applications of the steady state airplane • Synthesis of stability augmentation systems— background, government equations of motion: longitudinal moment yaw dampers, pitch dampers, α-feedback, research laboratory personnel and equilibrium, the airplane trim diagram β-feedback; effect of flight condition, sensor orientation and servo dynamics; basic educators. (conventional, canard and flying wing), airplane neutral point, elevator-speed autopilot modes; longitudinal modes— gradients, the nose-wheel lift-off problem; attitude hold, control-wheel steering, neutral and maneuver point (stick fixed) altitude hold, speed control and Mach trim; Fee lateral-directional modes—bank-angle • Applications of the steady state airplane $2,445 hold, heading hold, localizer and glide- equations of motion: lateral-directional slope control, automatic landing; coupling Includes instruction, Airplane moment equilibrium, minimum control speed problems—roll-pitch and roll-yaw coupling, Flight Dynamics and Automatic with engine-out pitch rate coupling into the lateral-directional Flight Controls, Parts I–II; Airplane modes, nonlinear response behavior; effects Design, Parts VI and VII; Lessons Day Three of aeroelasticity—aileron reversal, wing • Effects of the flight control system: reversible divergence, control power reduction; effect of Learned in Aircraft Design, all by aeroelasticity on airplane stability derivatives Jan Roskam, refreshments and five and irreversible flight controls; control surface hinge moments, stick and pedal forces, force lunches. • Exercise using the Advanced Aircraft Analysis trim; stick-force gradients with speed and software showing stability and control The course notes are for with load factor; neutral and maneuver point derivatives, trim diagram, longitudinal and participants only and are not for stick free; effect of tabs—trim-tab, geared-tab, lateral-directional trim, take-off rotation, servo-tab, spring-tab; effect of down-spring dynamics, flying qualities sale. and bob-weight; flight control system design considerations—reversible and irreversible, actuator sizing and hydraulic system design Certificate Track considerations This course is part of the Flight Tests and Aircraft Performance What a participant can expect to learn: Track and the Aircraft Design • Expect to learn airplane dynamic behavior, how to perform trim, how to check stability, Track. See pages 9 and 10. how aerodynamics and propulsion affect flying qualities and trim. Introduction to stability augmentation systems. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Online Course 24 AIRPLANE PERFORMANCE: THEORY, APPLICATIONS AND CERTIFICATION (Online Course) Instructor: Jan Roskam, Mediated by Mario Asselin

This course delivery features streaming video and animated illustrations. Offering Online Instruction We are excited to present this dynamic learning opportunity featuring Jan Roskam. Available anytime Class time 28 hours Participants will be guided through course sections and will have the CEUs 2.8 flexibility to complete the sections and reading at their own time and pace.

Interaction with the instructor takes place via email. Description Overview of airplane performance and prediction, Course Sections performance applications, certification standards Review of Airfoil Theory and the effects of stability and control on Review of Wing Theory performance. Airplane Drag Breakdown Fundamentals of Stability and Control Target Audience Class I Method for Stability and Control Analysis Designed for aeronautical engineers, pilots with Fundamentals of Flight Performance an engineering background, simulator engineers, government research laboratory personnel and Take-off Performance university faculty. Landing Performance Climb and Drift-Down Performance Fee Airplane Propulsion Systems $1,485 plus Range, Endurance and Payload Range $45 (USD) shipping within the U.S. Sensitivity Studies and Growth Factors $110 (USD) shipping to Canada and international Maneuvering and the Flight Envelope destinations Estimating Wing Area, Take-Off Thrust, Take-Off Power and Includes online instruction, Airplane Aerodynamics Maximum Lift: Clean Takeoff and Landing and Performance, by C. Edward Lan and Jan Preliminary Configuration Design and Integration of the Roskam and Airplane Design, Parts I, II, and VII, by Propulsion System Jan Roskam. Flight Test Principles and Practices The course notebook and supplemental readings will be mailed upon receipt of payment. Airplane Life Cycle Program Costs The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Flight Tests and Aircraft Performance Track. See page 10.

“I have always enjoyed listening to Dr. Roskam. His experience shows with each lecture.” — Online course participant

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 25 Seattle AIRPLANE PRELIMINARY DESIGN Instructor: Willem A.J. Anemaat

Day One • Examples of weight and balance using AAA Offering Location • Review of drag polar breakdown for subsonic • V-n diagram Location Seattle, Washington and supersonic airplanes, rapid method for drag • Class II weight, balance and moment of inertia polar prediction, check of drag polar realism; prediction Date April 28–May 2, 2014 review of fundamentals of flight mechanics: take- Course Number AA141360 off and landing characteristics, range, endurance • Fundamentals of static longitudinal stability; and maneuvering, the payload-range diagram the trim diagram, trim considerations for conventional, canard and three-surface designs, • Preliminary sizing of airplane take-off weight, tail and canard stall Times/CEUs empty weight and fuel weight for a given mission specification: applications; sensitivity of take- Day Four Monday–Friday 8 a.m.–4 p.m. off weight to changes in payload, empty weight, range, endurance, lift-to-drag ratio and specific • Deep stall and how to design for recoverability, Class time 35 hours fuel consumption; role of sensitivity analyses effects of the flight control system; control force in directing program-oriented research and versus speed and load factor gradients; flying CEUs 3.5 development: applications quality considerations; additional stability and control considerations; effect of flaps; minimum • Performance constraint analyses: relation control speed with asymmetric thrust between wing loading and thrust-to-weight ratio Description (or wing loading and weight-to-power ratio) • Take-off rotation and the effect of landing gear Overview of the design decision- for the following cases: stall speed, take-off location making process and relation field length and landing field length, statistical • Review of dynamic stability concepts and method for estimating preliminary drag polars, prediction methods; short period, phugoid, spiral of design to manufacturing, review and effect of airworthiness regulations; maintainability and cost- roll and Dutch roll modes; flying quality criteria: relation between wing loading and thrust-to- before and after failures in flight crucial systems; effectiveness. Applicable to jet weight ratio (or wing loading and weight-to- the role and limitations of stability augmentation; transport, turboprop commuter power ratio) for the following cases: climb and review of control surface sizing criteria: trim, transport, military (trainers, climb rate (AEO and OEI), cruise speed and maneuvering and stability augmentation; maneuvering; the matching of all performance initial system gain determination; sensitivity fighter bomber, UAV) and general constraints and preliminary selection of wing aviation aircraft. analyses and their use in early design decision area and thrust required: applications making; flight control system layout and design considerations; mechanical and hydraulically Day Two powered flight controls; layout design Target Audience • Preliminary configuration selection; what drives considerations for redundant “flight-crucial” unique (advanced) configurations? Discussion systems: architectures associated with various Designed for aeronautical of conventional, canard and three-surface types; safety and survivability considerations engineers, pilots with some configurations; fundamentals of configuration • Airworthiness code engineering background, design, step-by-step analysis of the feasibility of government research laboratory configurations: applications • Fundamental considerations in fuel system layout design; sizing criteria; some do’s and personnel, engineering managers • Fundamentals of fuselage and wing layout design; don’ts; layout and design considerations for and educators. aerodynamic, structural and manufacturing “other” systems: de-icing, water and waste water considerations; effect of airworthiness regulations • High-lift and lateral control design Day Five Fee considerations; handling quality requirements; • Landing gear design revisited, shock absorber icing effects; layout design of horizontal tail, design, structural integration of the landing gear, $2,445 vertical tail and/or canard; static stability and some do’s and don’ts control considerations; the X-plot and the trim Includes instruction, Airplane diagram; stable and unstable pitch breaks; effect • Factors to be considered in estimation of: research Design Parts I–VIII; Lessons Learned of control power nonlinearities; icing effects and development cost and manufacturing and in Aircraft Design, all by Jan operating cost; the concept of airplane life cycle Roskam; Advanced Aircraft Design: Day Three cost: does it matter in commercial programs? Discussion of 81 rules for “design for low cost”; Conceptual Design, Technology • Fundamentals of powerplant integration: inlet the break-even point, estimation of airplane “net and Optimization of Subsonic Civil sizing, nozzle configuration, clearance envelopes, worth” and its effect on program decision making; Airplanes, by Eghert Torenbeek, installation considerations, accessibility other factors in airplane program decision making, considerations, maintenance considerations; refreshments and five lunches. finding a market niche, risk reduction through effect of engine location on weight, stability and technology validation, design to cost; lessons The course notes are for participants control; minimum control speed considerations learned in past programs: do we really learn them? only and are not for sale. • Fundamentals of landing gear layout design; • Automated Design tip-over criteria; FOD considerations; retraction kinematics and retraction volume; take-off rotation • Advanced Concepts including flying wing, hydrogen-fuel airplanes, twin fuselage, joined Certificate Track • Class I weight and balance prediction; the c.g. wing excursion diagram; Class I moment of inertia This course is part of the Aircraft prediction; importance of establishing control • Introduction to design optimization Design Track. See page 9. over weight; preliminary structural arrangement for metallic and composite airframes; manufacturing and materials considerations aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 26 APPLIED NONLINEAR CONTROL AND ANALYSIS Instructor: Bill Goodwine

Day One Day Four Offering Available as on-site course • Identifying nonlinear • Feedback linearization Contact us for a no-cost, no obligation proposal for an phenomena such as multiple • Center manifold theory and on-site course: equilibria, bifurcations, chaos, stability nonunique and multiple On-site Program Manager solutions, limit cycles, finite • Bifurcation theory Email [email protected] escape time, sub- and super- Phone 785-864-8282 harmonic response Day Five • Nomenclature and definitions • Introduction to hybrid Times/CEUs (switching) systems • The theory and process of Class time 35 hours linearization • Stability of hybrid systems under arbitrary switching CEUs 3.5 • The method of harmonic balance • Stability of hybrid systems under controlled switching • Introduction to describing Description functions • Stability of hybrid systems This course covers analysis methods for nonlinear under state-dependent dynamical systems with the primary applications to Day Two switching feedback control. It is particularly designed for control engineers who are facing challenges due to more • Describing functions examples tightly integrated systems and systems governed • Nonlinear stability and by controllers with switching behavior or logic. The Lyapunov functions nonlinear control applications covered are overviews • Control and the direct of describing functions, the direct Lyapunov method, Lyapunov method the Lur’e problem and circle criterion, the small gain theorem, adaptive control, feedback linearization • Methods for determining (dynamic inversion) and hybrid systems. The theoretical Lyapunov functions content, which is the basis for understanding the control applications, consists of identifying nonlinear Day Three phenomena, the process and theory of linearization, • The Lur’e problem, circle Lyapunov stability, boundedness, center manifold criterion and Popov criterion theory and bifurcations. The supplied CD contains MATLAB programs that can be used as the basis for • The small gain theorem and hands-on exercises. applications • Stability of nonlinear nonautonomous systems and Target Audience boundedness This course is appropriate for managers and engineers who work in the analysis and design of modern control systems.

Fee A participant can expect to learn to: Includes instruction, a course notebook and CD. • identify nonlinear phenomena in the dynamics of physical systems; The course notes are for participants only and are not • apply the basic tools of Lyapunov stability theory to determine the for sale. stability of nonlinear systems; • use describing functions to determine the existence of limit cycles; Certificate Track • apply methodologies from adaptive control; This course is part of the Flight Control Systems Design • understand and apply tools for the analysis of center manifolds and Track. See page 10. bifurcating systems; • apply methods for the analysis of hybrid and switching systems. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 27 Seattle AVIATION WEATHER HAZARDS Instructor: Wayne R. Sand

Day One Day Three Offering Location Location Seattle, Washington • Thunderstorms and strong • Basic icing physics: supercooled convective clouds: basic liquid water content, droplet Date April 29–May 2, 2014 conceptual models, single-cell sizes, temperature Course Number AA141400 storms, multi-cell storms and • Intensity and character: light, line storms moderate and severe; continuous Times/CEUs • Stability and instability, storm and intermittent; collection tops and vertical motion efficiency; rime, clear and mixed Tuesday–Friday 8 a.m.–4 p.m. • Turbulence: causes and results, • Icing forecasts: NWS forecasts; Class time 28 hours intensity, tornadoes experimental forecasts; cloud CEUs 2.8 • Lightning: causes and results, type forecasts, cumuliform composite aircraft, lightning (max intermittent) and detection networks stratiform (max continuous); Description orographic influence • Heavy rain: raindrops and drop Examines the key weather hazards that affect all of sizes, precipitation intensity, • Aircraft performance effects: aviation and provides an in-depth understanding effects on performance de-iced and anti-iced aircraft; of the most serious aviation weather hazards unprotected components; faced by all aspects of aviation. Materials and • Radar: airborne weather lift, drag, weight and climb instruction are designed to provide enough depth radar, WSR-88D (NEXRAD), considerations; pilot action to enable pilots to make preflight and in-flight Stormscope considerations weather-related decisions intelligently. Designed to • Hail: mechanisms to develop • Icing sensors, in situ, remote, provide flight test and design engineers the basic hail, visual and radar detection passive information necessary to consider weather factors • Detailed sensors for certification: when designing aircraft and aircraft components. Day Two supercooled liquid water content, Flight dispatchers also will gain insight into aviation • Windshear: physics of droplet sizes, temperature weather hazards, which should substantially enhance microbursts, stability and their ability to make weather-related decisions. instability, precipitation • How to find and/or avoid icing loading, evaporation, dry and conditions wet microbursts Target Audience Day Four • Gust fronts: thunderstorm Designed for pilots, test pilots, meteorologists, flight generated, cold fronts, structure • Mountain weather: differential test engineers, design engineers, dispatchers, RPV heating, mountain and valley designers and operators, government and research • Windshear training aid: winds, channeling winds, detection signals, flight crew laboratory personnel and educators. thunderstorms, waves, rotors, actions density altitude • Clear air turbulence: jet stream, • Low ceiling and visibility: fog, Fee thunderstorm wake, instability, various types; snow, rain; low $2,145 waves, deformation zones ceilings; conditional forecasts, Includes instruction and course notebook, • Detection Systems: Terminal chance and occasional refreshments and four lunches. Doppler Weather Radar, Low- • Weather-related accident Level Windshear Alert Systems, The course notes are for participants only and are not statistics: problem areas, NTSB airborne forward-look systems, for sale. and AOPA statistics, specific airborne in situ systems, accident discussions integrated terminal weather information system • New systems: ASOS, GOES, Certificate Track ADDS, AFSS, data link, rapid This course is part of the Aircraft Maintenance and • Accidents: discussion of key update cycle, new display and Safety Track. See page 10. accidents depiction concepts, air traffic controller weather, others • Review and questions aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Seattle and San Diego 28 COMMERCIAL AIRCRAFT SAFETY ASSESSMENT AND 1309 DESIGN ANALYSIS Instructor: Marge Jones

Day One Day Three Offering Locations • System safety basics • Tailoring the Location Seattle, Washington including accident safety process for statistics/data, system modifications (STCs) Date April 28–May 2, 2014 safety vs. reliability • Failure rate prediction Course Number AA141370 concepts, and techniques and class understanding the exercise Location San Diego, California 1309 regulation • Failure Mode and Date September 8–12, 2014 • Overview of the SAE Effects Analysis Course Number AA151020 ARP 4761 Safety (FMEA)/Failure Mode Assessment process Effects Summary for commercial (FMES) Times/CEUs aviation • Fault Tree Analysis Monday–Thursday 8 a.m.–4 p.m. • Determining the (FTA) concepts, Friday 8 a.m.–11:30 a.m. required level of safety modeling techniques Class time 31.5 hours analysis required and examples, calculating CEUs 3.15 Day Two probabilities, • Aircraft and System importance measures Functional Hazard and software tools Description Assessments including Covers system safety requirements of 14 CFR 23.1309, 25.1309, 27.1309 and • Class FMEA and FTA class exercise 29.1309 from fundamental philosophies and criteria to the analysis techniques exercise to accomplish safety requirement identification, validation and verification. • Overview of the Includes detailed review of SAE ARP 4761 and system safety related aspects SAE ARP 4754A Day Four and of ARP 4754A including allocation of safety requirements and assigning Development Process development assurance levels. Class exercises include Functional Hazard Day Five Assessment, Preliminary System Safety Assessments, Failure Rate Prediction, focused to capture, Failure Mode and Effects Analysis, and Fault Tree Analysis. Principles apply to validation, and • Common cause analysis: particular all types of commercial aircraft certification and may also be adapted for any verification of safety system safety activity. requirements using risk, zonal and safety assessment common mode techniques • System safety Target Audience • System architecture assessment Designed for Parts 23, 25, 27 and 29 system certification engineers, system designers, FAA Designated Engineering Representatives (DERs), aircraft concepts, modeling • Safety analysis certification personnel, system safety specialist new to commercial certification failure conditions and information safety process and military personnel procuring civil equipment. from proposed required to support architecture, and development of assigning development Certification Plans. Fee assurance levels Guidelines for $2,445 including SAE ARP preparing 1309 safety- 4754A Guidelines for related compliance Includes instruction, a course notebook, a CD of references materials, SAE ARP 4754A–Guidelines for Development of Civil Aircraft and Systems, SAE ARP 4761– Development of Civil statements Guidelines and Methods for Conducting the Safety Assessment Process on Civil Aircraft and Systems Airborne Systems and Equipment, SAE ARP 5580–Recommended Failure Modes and Effects Analysis (FMEA) Practices for Non-Automobile Applications, refreshments • Preliminary System and five lunches. Safety Assessments and allocating The course notes are for participants only and are not for sale. safety requirements including common Certificate Track mode mitigations and physical safety This course is part of the Aerospace Compliance Track and the Aircraft requirements (zonal) Maintenance and Safety Track. See pages 9 and 10. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 29 Orlando COMMERCIAL SPACE—WHAT IT MEANS AND THE ISSUES IT RAISES (NEW) Instructors: Marco Villa, Max Vozoff

Day One Day Three Offering Location Location Orlando, Florida • Brief History of Space—Roles of • Terrestrial Markets—Bringing Space Government and Industry Down to Earth Date November 18–20, 2014 • Historical Examples of Commercial • Space Qualifying—Repurposing Course Number AA151260 Space Enterprises—Successful and Terrestrial Products otherwise • Suborbital Vehicles—Blurring the Times/CEUs • Current Examples of Commercial Space Boundary Enterprises—Products, Services and Tuesday–Thursday 8 a.m.–4 p.m. • Potential New Markets—In Space and Target Markets Class time 21 hours Beyond • Analogies and parallels with history • Investors—Space: The Final Frontier CEUs 2.1 and development of aviation • Barriers to Entry and Limitations on • International space landscape (agencies, Growth Description budgets, players, stakeholders) • View from the Bridge—Near-Term Leveraging the unique experience • Culture Clash—“…when an irresistible Prospects and Opportunities of the lecturers, this course will force meets an immovable object…” walk participants through the major characteristics, issues, challenges Day Two and promises of a new outlook for • Intellectual Property—Issues and an industry that is generally highly Management mature and reticent to change. Multiple examples will be presented • The Regulatory Environment—licenses, as examples of the successes, failures permits and certifications and differences between the new and • Accepting Government Money—As a the traditional approaches, and to Contractor, Partner or Customer illustrate the principles which define • Policy and Politics this emergent phenomenon. • Safety, Security, Liability and Insurance • Export Control—Limitations and Target Audience Opportunities Designed for engineers, managers, business developers, entrepreneurs, investors, and other professionals at all levels with an interest in reaping benefit from the commercial space phenomena. What a participant can expect to learn: • how the traditional space industry has differed from other industries; Fee • the key differences in attitude, outlook and approach between the traditional space $1,845 industry and “NewSpace”; Includes instruction, a course notebook, • the reasons for the success of some commercial space companies (and not others); refreshments and three lunches. • the key challenges and hurdles facing the emerging commercial space industry; The course notes are for participants • the potential of applying the precepts, processes and products from other industries only and are not for sale. to space; • the benefits and challenges of spinning space-derived technologies into other Certificate Track industries; This course is part of the • the opportunities the emerging commercial space industry offers to small companies, Management and Systems Track. See entrepreneurs and investors; page 10. • the hurdles in adapting an existing space company to compete in this new commercial space landscape. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 30 COMPLEX ELECTRONIC HARDWARE DEVELOPMENT AND DO-254 Instructor: Jeff Knickerbocker

Day One Day Three Offering Location • Introductions and • Firmware vs. software vs. Location San Diego, California background hardware Date September 8–10, 2014 • History and overview of DO- • Microprocessor assurance Course Number AA151000 254 • Simple vs. complex • FAA’s advisory material • Structural coverage Times/CEUs • Complex electronic • What to expect from technology certification authorities Monday–Wednesday 8 a.m.–4 p.m. • Framework of DO-254 • Challenges in complex Class time 21 hours • Planning process hardware development and CEUs 2.1 • Development process certification • Summary Description Day Two This course provides the fundamentals of developing • Validation and verification and assessing electronic components to the standard • Configuration management RTCA/DO-254 Design Assurance Guidance for Airborne Electronic Hardware. It is designed for developers, • Process assurance (a.k.a. avionics engineers, systems integrators, aircraft designers quality assurance) and others involved in development or implementation • Certification liaison process of complex electronic hardware (Application Specific Integrated Circuits, Field-Programmable Gate Arrays, • Tools etc.). The course also provides insight into the FAA’s review process and guidance and provides practical keys for successful development and certification. Practical exercises and in-class activities will be used to enhance Enroll in this course and the learning process. Integrated Modular Avionics (IMA) and DO-297 (see page 47). Target Audience Save money. The cost for the two courses Designed for developers, avionics engineers, systems combined is $2,445. To enroll in both courses, integrators, aircraft designers and others involved in use course number AA151090. development or implementation of complex electronic hardware and programmable devices (Application Specific Integrated Circuits, Field-Programmable Gate Arrays, etc.).

Fee $1,845 Includes instruction, course notebook, RTCA/DO- 254 Design Assurance Guidance for Airborne Electronic A participant can expect to: Hardware, refreshments and three lunches. • develop and document efficient RTCA/DO-254 compliant The course notes are for participants only and are not for processes; sale. • create, capture and implement compliant requirements design data; Certificate Track • generate and adhere to effective validation and verification strategies; This course is part of the Avionics and Avionic Components Track. See page 10. • evaluate compliance to RTCA/DO-254; • understand FAA’s policy and guidance. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 31 San Diego CONCEPTUAL DESIGN OF UNMANNED AIRCRAFT SYSTEMS Instructors: Armand Chaput, Bill Donovan, Richard Colgren This course may be taught by any of the above instructors, based on his availability.

Day One Day Three Offering Location Location San Diego, California • Course introduction • Air vehicle parametric design Date September 8–12, 2014 • Introduction to UAS • Conceptual level aerodynamics Course Number AA151030 • UAS conceptual design issues • Standard atmosphere models • Fundamentals of system design • Parametric propulsion • UAS operating environments Times/CEUs Day Four • Sortie rate estimates Monday–Thursday 8 a.m.–4 p.m. • Mass properties Friday 8 a.m.–11:30 a.m. Day Two • Parametric geometry Class time 31.5 hours • Requirements analysis • Air vehicle performance CEUs 3.15 • Control station considerations and • Mission assessment sizing • Methodology and correlation Description • Communication considerations/ Conceptual approach to overall design of sizing Day Five Unmanned Aircraft (UA) Systems (UAS) includes • Payload (EO/IR and radar) • Air vehicle optimization concepts of operations, communications, considerations and sizing • Overall system optimization payloads, control stations, air vehicles • Reliability, maintainability and • Class design presentation and support. Includes requirements and support architecture development, initial sizing and conceptual level parametric and spreadsheet • Life cycle cost assessment of major system elements. • Decision making

Target Audience Designed primarily for practicing conceptual level design engineers, systems engineers, technologists, researchers, educators and engineering managers. Students should have some knowledge of basic aerodynamics and conceptual design, although it is not mandatory. Basic knowledge of spreadsheet analysis methods is assumed.

Fee $2,445 Includes instruction, course notebook and five A participant can expect to learn to: lunches. • design and analyze overall unmanned aircraft systems; The course notes are for participants only and • estimate sensor size and performance and impact on overall system are not for sale. performance; • understand basic elements of UAS communications and know how to Certificate Track estimate overall communication system size and power requirements; This course is part of the Aircraft Design Track. • develop overall concepts of cooperation and assess impacts of sortie rate See page 9. and supportability; • understand key air vehicle configuration drivers, how to estimate aero/ propulsion/weight/stability, overall air vehicle performance, size and tradeoffs. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Orlando 32 DIGITAL FLIGHT CONTROL SYSTEMS: ANALYSIS AND DESIGN Instructor: David R. Downing

Day One Day Three Offering Location • Introduction and Problem Definition, • Modern Design of Continuous MIMO Location Orlando, Florida Flight Dynamics: development of Controllers: analysis of MIMO systems, non-linear equations of motion, development of continuous Linear Date November 17–21, 2014 development of linear equations of Quadratic Regulator, weighting matrix Course Number AA151230 motion, standard trim conditions, selection, non-zero set point problem, development of stability and control proportional integral structure, derivatives, Classical Design of control rate weighting structure, PIF Times/CEUs Continuous Controllers Using SISO structure, comparison of PIF and PID Monday–Friday 8 a.m.–4 p.m. Tools: problem definition, Laplace control structures, design of typical Transforms, complex plane analysis lateral and longitudinal control modes Class time 35 hours of linear SISO systems, typical for continuous MIMO vehicles using CEUs 3.5 compensators, and design of SISO modern techniques closed loop control systems. Use of frequency response data to estimate Day Four Description unknown transfer functions • Modern Design of Sampled Data This course presents a set of classical MIMO Controllers: development and and modern flight control analysis Day Two analysis of digital MIMO systems, and design tools. These tools will be • Classical Design of Continuous development of discrete and sampled combined to form a design process Controllers Using SISO Tools (cont’d): data Linear Quadratic Regulator, that will enable the development Design of typical continuous lateral and weighting matrix selection, non-zero of flight control systems that are longitudinal control modes for MIMO set point problem, proportional integral implementable in “real world” aeronautical vehicles, implementation structure, control rate weighting vehicles. These techniques will be of perturbation controllers in non- structure, PIF structure, design of used to design typical aeronautical linear MIMO vehicles. Classical Design typical sampled data lateral and vehicles’ lateral and longitudinal of Sampled Data Controllers Using longitudinal control modes for MIMO controllers. SISO Tools: problem definition, develop vehicles using modern techniques models of sampler and ZOH, complex plane analysis of linear SISO sampled Day Five Target Audience data systems, analysis of closed loop • Output Feedback for Sampled Data Designed for individuals from SISO sampled data systems, z-plane Controllers: development of output government or industry who design, compensators, design of typical feedback design techniques, command simulate, implement, test or operate sampled data lateral and longitudinal generator tracker, output feedback-PIF- digital flight control systems or who control modes for continuous CGT MIMO sampled data controllers, need an introduction to classical and MIMO vehicles, implementation of design of typical sampled data lateral modern flight control concepts. perturbation controllers in non-linear and longitudinal control modes for MIMO vehicles MIMO vehicles using output feedback techniques Fee $2,445 A participant can expect to: Includes instruction, a course notebook, refreshments and five • review flight dynamics to highlight the key features of aircraft dynamics; lunches. • review Classical Single Input/Single Control Design Techniques in the Laplace The course notes are for participants Domain; only and are not for sale. • be introduced to Modern Multi-Input/Multi-Output Linear Quadratic Regulator Design Technique; • incorporate desirable Classical Controller features into the Linear Quadratic Certificate Track Regulator Optimization Problem by defining new state variables, enhanced This course is part of the Flight command structures and state estimation techniques; Control Systems Design Track. See • apply the Classical and Modern Design Techniques to design aircraft flight control page 10. systems that can be implemented in the real world. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 33 Online Course DURABILITY AND DAMAGE TOLERANCE CONCEPTS FOR AGING AIRCRAFT STRUCTURES (Online Course) Instructor: John Hall

Online Instruction This course delivery features streaming video and animated illustrations. Available anytime Participants will be guided through course sections and will have the flexibility to Class time 19 hours complete the sections and reading at their own time and pace. CEUs 1.9 Interaction with the instructor takes place via email.

Description Topics Design, analysis and testing fundamentals • Background to current aging airplane programs are used as an introduction to the effects of • Design objectives: safety, economics and responsibilities fatigue, accidental and corrosion damage • Damage sources: environmental deterioration, accidental and fatigue damage on the durability and damage tolerance of aircraft structure. Emphasis is placed on • Evaluation: loads, stresses, detail design, analysis and testing current programs used to assure continuing • Manufacture: processes and assembly airworthiness of aging aircraft structure. • Certification: fatigue and damage tolerance Principal topics are centered on commercial jet transport aircraft, but fundamentals are • Maintenance: inherent characteristics and operator responsibilities applicable to all types of aircraft. • Aging airplane programs: introduction, modifications, repairs, corrosion prevention and control, fatigue and widespread cracking, structural Target Audience maintenance program guidelines • Future airplanes: design and analysis, MSG-3-Revision 2 Designed for managers, engineers, maintenance and regulatory personnel in the aircraft industry who are involved in the evaluation, certification, regulation and maintenance of aging aircraft structure.

Fee “The class was indeed interesting and useful.” $1,245 $35 (USD) shipping within the U.S. — Online course participant $95 (USD) shipping to Canada and other international locations. Includes online instruction and course notebook. A participant can expect to better understand: The course notebook will be mailed upon receipt of payment. • basic aging airplane programs, including: The course notes are for participants only – modifications and are not for sale. – repairs – corrosion prevention control – fatigue (SSID/DTR) Certificate Track – widespread fatigue cracking This course is part of the Aircraft Maintenance • the potential effects of airplane aging on structural maintenance, including: and Safety Track. See page 10. – applicable design – evaluation – testing – manufacturing – certification procedures – maintenance procedures developed and used by operators and airplane manufacturers aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 34 ELECTRICAL WIRING INTERCONNECT SYSTEM (EWIS) AND FAA REQUIREMENTS (NEW) Instructor: C. Bruce Stephens

Day One Day Four Offering Location • Introduction • System Design and Analysis Location San Diego, California • The Electromagnetic • Fuel Tank Ignition Source Date September 15–19, 2014 Environment of Aircraft— Prevention Guidelines Course Number AA151140 Metallic and Composite Aircraft • Acceptable Methods, Techniques Requirements and Practices—Aircraft • Electromagnetic Interference Inspection and Repair Times/CEUs (EMI) • EWIS Workshop Monday–Thursday 8 a.m.–4 p.m. • Electromagnetic Compatibility Friday 8 a.m.–11:30 a.m. (EMC) Day Five Class time 31.5 hours • Electrical Bonding • CFR Compliance Statements CEUs 3.15 • Electrostatic Discharge (ESD) • Final EWIS Discussion and Questions • Precipitation Static (P-STATIC) • EWIS Final Exam presentations Description • High-Intensity Radiated Fields (HIRF) This course will discuss the FAA Code of Federal Regulations (CFR’s) and design concepts required • Lightning to ensure all aspects of aircraft electrical wiring and installation are safe. It will examine aircraft wiring as Day Two a system and review all Part 25 CFR’s related to EWIS FAA Certification. A review of FAA Advisory Circulars • Aircraft EWIS Best Practices Job and practical applications of the information will Aid—Background and Examples be conducted as teams will be selected to simulate • Certification of Electrical Wiring the EWIS certification process. EWIS requirements Interconnection Systems on for aircraft maintenance and inspection will also be Transport Category Airplanes discussed. The course will also include a high level overview of • EWIS Examples and Practical Electromagnetic Compatibility (EMC), High Intensity Applications Radiated Fields (HIRF), Lightning, Precipitation • EWIS Workshop Static, Electrostatic Discharge and Electrical Bonding requirements. Day Three • Certification Case Study Design Target Audience Example Electrical, Avionics, and HIRF/Lightning Technicians and • Electrical Equipment and Designers. Installations • Circuit Protective Devices Fee • Fire Protection Systems $2,445 • Electrical Supplies for Emergency Includes instruction, a course notebook, refreshments Conditions and five lunches. • Protection Against Injury The course notes are for participants only and are not • Electrical Wiring for sale. Interconnection Systems Instructions for Continued Airworthiness Using Enhanced Certificate Track Zonal Analysis Procedure This course is part of the Aerospace Compliance Track, Aircraft Maintenance and Safety Track and • EWIS Workshop Avionics and Avionic Components Track. See pages 9 and 10. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 35 San Diego ESSENTIALS OF EFFECTIVE TECHNICAL WRITING FOR ENGINEERING PROFESSIONALS (NEW) Instructor: Paul H. Park

Day One Offering Location Location San Diego, California • Introduction, Course Objectives, Organizing Documents, Preparing Figures Date September 18–19, 2014 • Exercise 1—Develop 2-page Exec Summary Module of Proposal or Report Course Number AA151180 • Exercise 2—Update Module and Add Bullet Statements • Lecture/Mini-Exercises—Big-4 Effective Writing Essentials Times/CEUs • Lecture/Mini-Exercises—Guidelines for Clear and Succinct Writing Thursday 8 a.m.–4 p.m. • Exercise 3—Edit Memo Friday 8 a.m.–11:30 a.m. Day Two Class time 10.5 hours • Exercise 4—Draft Proposal/Report Module CEUs 1.05 • Student Pairs Edit Proposals/Report Module • Student Pairs Review Proposal/Report Module Edits Description • Prepare Final Draft This course introduces elements • Review Edited Proposals/Reports with Class of effective technical writing and provides practice in using these elements. The course covers methods to organize documents, techniques for creating figures, guidelines for selecting sentence voice and tense, and guidelines for clear and succinct writing.

Target Audience Engineering professionals and engineering students

Fee $695 Includes instruction, handouts, refreshments and two lunches. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Management and Systems Track. See page 10. A participant can expect to learn: • a systematic method to organize and build technical documents—reports, proposals, processes; • basic techniques for creating data-rich, legible figures; • guidelines for selecting sentence voice and tense; • guidelines for clear, succinct, and lively technical prose. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Las Vegas and San Diego 36 FAA CERTIFICATION PROCEDURES AND AIRWORTHINESS REQUIREMENTS AS APPLIED TO MILITARY PROCUREMENT OF COMMERCIAL DERIVATIVE AIRCRAFT/SYSTEMS Instructors: Gilbert L. Thompson, Robert D. Adamson This course may be taught by either instructor, based on his availability.

Day One • Utilizing FAA and Industry Guide to Product Certification, specifically Offering Locations • Review of course content and class Project-Specific Certification Plan Location Las Vegas, Nevada exercise (PSCP) principles in the Request for Date March 4–6, 2014 • Overview of FAA Aircraft Certification Proposal (RFP) process (AIR) and Flight Standards (AFS) • Impact of FAA Safety Management Course Number AA141290 service organizations as they relate to practices Tuesday–Thursday 8 a.m.–4 p.m. military use of commercial derivative aircraft/systems • FAA Form 337/Field Approval process • Applicability of FAA Advisory Circulars, Location San Diego, California Day Three Notices and Orders Date September 15–17, 2014 • Type Certification Data Sheets (TCDS) • FAA “baseline” and “Project Specific Course Number AA151100 Service Agreement” (PSSA) services • Impact of Part 36, Noise Standards following Title 14, Code of Federal Monday–Wednesday 8 a.m.–4 p.m. • Airworthiness Directive (AD) process Regulations (CFR), Parts 1, 11, 21 applied to CDA • Parts Manufacturer Approval (PMA) • Bilateral Aviation Safety Agreements Time/CEUs process (BASA) and European Aviation Safety Class time 21 hours • Technical Standard Order Authorization Agency (EASA) (TSOA) process CEUs 2.1 • Impact of DoD acquisition policies as • Airworthiness Standards Parts 23, 25, exemplified by USAF Policy Directives 26, 27, 29 and 33 62-6, NAVAIR Instruction 13100.15 and Description • Part 183, Representatives of the Army Regulation 70-62 Overview of FAA functions and requirements Administrator, including Subpart D, • Federal Reimbursable Agreement AVS- applicable to Type Design Approval, Production Approval, Airworthiness Approval and Continued Organization Designation Authorization OA-ACE-12-3035 between DOT/FAA Airworthiness associated with military procured (ODA) and Armed Services of the United States commercial derivative aircraft and products. Course will focus on the unique military needs in procurement • Comparison of DoD/FAA airworthiness (customer versus contractor) of products meeting civil Day Two processes; application of MIL-HDBK- airworthiness requirements which are aligned with • Part 43 Maintenance, Preventive 516B, Airworthiness Certification military-specific mission/airworthiness goals. Maintenance, Rebuilding and Alteration Criteria; development of TACC/MACC • Eligibility of Department of Defense • Role of the FAA Military Certification Target Audience (DoD)/DoD contractor installations and Office (MCO) modification centers as FAA Part 145 Designed, and focused in scope, specifically for • FAA Order 8110.101, Type Certification U.S. Department of Defense (DoD), Department of Repair Stations Procedures for Military Commercial Homeland Security, U.S. Coast Guard and non-U.S. • Part 39 Airworthiness Directives Derivative Aircraft military procurement and airworthiness personnel, and associated military/supplier engineers, consultants • Flight Standards Aircraft Evaluation • Certification options for CDA; use and project directors involved in procurement of Group’s (AEG) role in aircraft certification of FAA Form 8130-31, Statement of commercial derivative aircraft (CDA) or equipment developed for use on CDA. Conformity–Military Aircraft • Special conditions, equivalent level of safety and exemption process and • AC20-169, Guidance for Certification issuance of Military and Special Missions Fee Modifications and Equipment for • Type Certification (TC) and $1,845 Commercial Derivative Aircraft (CDA) Supplemental Type Certification (STC) Includes instruction, a course notebook, CD, process (FAA Handbook 8110.4) refreshments and three lunches. The course notes are for participants only and are not What a participant can expect to learn: for sale. • how to plan, during the Request For Proposal (RFP) phase, for leveraging military mission needs with civil certification and embedding same within Certificate Track contract requirements; This course is part of the Aerospace Compliance Track. See page 9. • use of TACC and MACC in defining and optimizing civil certification of military mission requirements. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 37 San Diego FAA CONFORMITY, PRODUCTION AND AIRWORTHINESS CERTIFICATION APPROVAL REQUIREMENTS Instructor: Jim Reeves

Day One Offering Location Location San Diego, California • Review course content and identification of attendee key issues Date September 9–11, 2014 • Aircraft certification service versus flight standards Course Number AA151050 • Overview of 14 CFR Part 21 • Designee and delegations Times/CEUs • Rules, policy and guidance Tuesday–Thursday 8 a.m.–4 p.m. • FAA conformity process Class time 21 hours Day Two CEUs 2.1 • Production approvals • Quality system requirements Description • Quality System Audit Presents the fundamental FAA requirements to produce • Certificate management products, appliances and parts for installation on FAA- type certificated products. Includes FAA conformity • Airworthiness approvals process, quality assurance requirements, the FAA’s evaluation program, airworthiness requirements and Day Three certificate management. Also includes a broad overview • Airworthiness approvals of the Organizational Delegation Authorization (ODA) • Compliance and enforcement regulations, qualification, responsibilities, application, • Organizational Delegation Authorization (ODA) appointment, operation and management.

Target Audience Designed for government and industry (original equipment and suppliers) engineers, quality assurance personnel, Designated Airworthiness Representatives (DARs) and managers involved in the manufacture of “Mr. Reeves brings extensive experience to the class products, appliances and parts installed on civil aircraft and thoroughly explains the FAA perspective.” with FAA airworthiness certification. — Robert Salyers Air Tractor, Inc. Fee $1,845 Includes instruction, course notebook, refreshments and three lunches. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Aerospace Compliance Track. See page 9.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Seattle and San Diego 38 FAA FUNCTIONS AND REQUIREMENTS LEADING TO AIRWORTHINESS APPROVAL Instructors: Gilbert L. Thompson, Robert D. Adamson The course may be taught by either instructor, based on his availability. Day One • Certification Process Offering Locations Improvement (CPI), FAA and • Review of course content and Location Seattle, Washington identification of attendee key Industry Guide to Product issues Certification, Partnership for Date April 29–May 1, 2014 Safety Plan (PSP)/Project Specific Course Number AA141390 • Overview of FAA Aircraft Certification Plan (PSCP) Certification (AIR) and Flight Tuesday–Thursday 8 a.m.–4 p.m. Standards (AFS) service • Documentation of typical TC/ STC projects organization and functions Location San Diego, California • Safety Management concepts • Advisory Circular, Notice and Date September 10–12, 2014 Order process and issuance • FAA Form 337/Field Approval Course Number AA151070 • Federal Aviation Regulations (FAR) Parts 1 and 11 Day Three Wednesday–Friday 8 a.m.–4 p.m. • Continuation of typical TC and • FAR Part 21 and the Technical STC projects Standard Order Authorization Times/CEUs (TSOA) process • Relation of Parts 23 and 25 to Class time 21 hours Civil Aviation Regulations (CAR), CEUs 2.1 Day Two CARs 3 and 4b • Parts 43 and 45 • Developing Type Certification Description • Part 36 Noise Requirements Data Sheets (TCDS) Overview of the FAA organizational structure and • Part 39 Airworthiness Directives • Noise Certification Part 36; its function in aircraft certification, the rule-making Airworthiness Directive (AD) and advisory process, production rules applicable • Part 183 Representatives of the process, Part 39 to aircraft and aircraft components, subsequent Administrator, including Subpart • AEG’s involvement in MMEL, certification process and continued airworthiness. D, Organization Designation Course is specifically tailored toward civil Authorization (ODA); Flight maintenance and flight manuals airworthiness certification. Course is FAA-approved for Standards Aircraft Evaluation • Flight Standards Information IA renewal. Group’s (AEG) role in aircraft Management System (FSIMS), certification notices and orders related to Target Audience • Parts 23, 25, 26, 27, 29 and 33 airworthiness Designed for industry (airframe and vendor) • Rulemaking and special • Bilateral Aviation Safety engineers, design engineers, civil airworthiness conditions, process and issuance Agreements (BASA) engineers, consultants, project directors, aircraft modifiers, FAA Designated Engineering • Equivalent level of safety and • U.S./European Union Executive Agreement and the European Representatives (DERs) and coordinators, FAA exemption process organizational designees/authorized representatives Aviation Safety Agency (EASA) (ARs), industry and governmental quality assurance • Parts Manufacturer Approval inspectors and managers. (PMA) • International Civil Aviation Organization (ICAO) • Type Certification (TC) and Supplemental Type Certification Fee (STC) process (FAA Handbook $1,845 8110.4) Includes instruction, a course notebook, CD, refreshments and three lunches. “An essential course for anyone involved in The course notes are for participants only and are not the design, production and maintenance of aircraft.” for sale. — Marguerite Russell, Technical Publications Developer Flight Test Data Systems Certificate Track The Boeing Company This course is part of the Aerospace Compliance Track. See page 9. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 39 On-site Course FAA PARTS MANUFACTURER APPROVAL (PMA) PROCESS FOR AVIATION SUPPLIERS Instructor: Jim Reeves

Day One Day Three Offering Available as on-site course Contact us for a no-cost, no obligation • Introductions • PMA Process Flowchart proposal for an on-site course: • FAA Organization • PMA Manufacturing Inspection On-site Program Manager • Aircraft Certification Service and Flight District Office (MIDO) Approval, CFR Email [email protected] Standards Service 21 Subpart K Phone 785-864-8282 • Purpose of the PMA • Elements of a good PMA production quality system • Order 8110.42c Introduction—Review Times/CEUs Appendix List • Quality System Components TC, PC, PMA and TSOA Class time 21 hours • PMA Exceptions • Certificate Management of all FAA CEUs 2.1 • Quality System Requirements Production Approval Holders, • Roles of the FAA and Applicant in the including overview of the Quality Description PMA process System Audits • Review a Bilateral Agreement with a This course will introduce any Day Two Foreign Country person producing replacement • Product Specific Certification Plan and modification parts for sale for • Review Implementation Procedures for (PSCP) installation on a type-certificated Airworthiness (IPA) Foreign Approvals product how to get a PMA Approval. • Basis for Design Approval • Review and discussion This includes current suppliers to • Applicant’s data package • Conclusion FAA Type Certificate and Production • Special Requirements for Test and Certificate Holders. Computation Applications • Part marking requirements Target Audience • Responsibilities of PMA holders after Aviation part manufacturers/ approval suppliers who are seeking FAA Parts • Aircraft Certification Office (ACO) Manufacturer Approval. responsibilities • Designated Engineering Fee Representatives (DERs) and Includes instruction, course notebook Organization and CD. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Aerospace Compliance Track. See page 9.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 40 FAR 145 FOR AEROSPACE REPAIR AND MAINTENANCE ORGANIZATIONS Instructor: Paul Pendleton

Day One Day Three Offering Available as on-site course • Introduction • Parts and material receiving inspection, Contact us for a no-cost, no obligation FAA AC 20-154 • Review of all Federal Aviation proposal for an on-site course: Regulations (FARs) with focus on FAR • Special FAR (SFAR) 36 On-site Program Manager 145 • Applicability to FAR Part 121 Email [email protected] • Development of repair manual for a • Field approval of major repairs and Phone 785-864-8282 class airframe versus a limited airframe alterations using the FAA designee rating, FAA AC 145-9 process, FAA AC 43-210 Times/CEUs • Development of a repair manual for • Processing the FAA Form 337 for major Class time 21 hours local facility versus off-site locations repairs and major alterations of aircraft, and specialized services ratings, FAA engines, etc., FAA AC 43-9-1F CEUs 2.1 AC 145-9 • Overview of manual content in • Repairman certification, FAA AC 65-24 preparation for application of repair Description • Parts fabrication in repair stations, FAA station certification This course will introduce students AC 43-18 • Discussion and class quiz to the details of FAA Federal • Development of a Quality Manual for • Conclusion Aviation Regulation (FAR) 145 and its FAA Part 145, FAA AC 145-9 application process. Day Two • Repair stations in countries with FAA Target Audience BASA, IPA and IPM, FAA AC 145-7A Designed for aerospace repair and • Internal evaluation (audit) of all repair maintenance organization personnel stations, FAA AC 145-5 who are involved with FAR 145 certification. • Development of training programs, FAA AC 145-10 • Hazardous Material Training Fee • Fabrication of replacement parts, FAA Includes instruction, course notebook AC 43-18 and CD. • Identification of parts, FAA AC 43-213 The course notes are for participants only and are not for sale. • Use of commercial parts, FAA AC 43-18

Certificate Track This course is part of the Aerospace Compliance Track and the Aircraft Maintenance and Safety Track. See pages 9 and 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 41 On-site Course FLIGHT CONTROL ACTUATOR ANALYSIS AND DESIGN Instructor: Donald T. Ward

Day One Day Three Offering Available as on-site course Contact us for a no-cost, no obligation proposal • Introduction • Electrically powered actuation (Power-By-Wire or PBW) systems for an on-site course: • Overview of aircraft flight (continued) On-site Program Manager control surfaces, components and Email [email protected] functions: primary flight control, • Modeling and simulation of PBW Phone 785-864-8282 secondary flight control; trim and examples feel, power control units • Flight control system design • Advanced actuation concepts requirements Times/CEUs • Mechanically controlled actuation • Specifications and documents: Class time 31.5 hours schemes: modeling and simulation Power Control Unit (PCU) and CEUs 3.15 basics Power-Drive Unit (PDU) analysis • Electrically signaled (Fly-By-Wire and design or FBW) systems Description Day Four Provides an in-depth understanding of Day Two • PCU and PDU analysis and design actuators, sensors and other components of • Electrically signaled (FBW) (continued) flight control systems. Includes both analysis systems (continued) • Dynamic performance and and practical use of flight control system response components. Reviews good design practices • Modeling and simulation of FBW examples typically used in flight control system design. Day Five • Alternate command systems • Dynamic analysis and modeling Target Audience • Electrically powered actuation exercise (Power-By-Wire or PBW) systems Designed for recent graduates of engineering • PCU assembly and installation or for practicing engineers outside the • Quality assurance aerospace industry who need practical exposure to the types of actuation hardware, sensors and design practices used on both commercial and military aircraft. Students should be acquainted with control design software. (MATLAB/Simulink or Scilab are currently utilized in the course for example problems.)

Fee Includes instruction, a course notebook, CD and R-123 Aircraft Flight Control Actuation System Design by Eugene Raymond and Curt Chenoweth. The course notes are for participants only and are not for sale.

Certificate Track Donald T. Ward This course is part of the Flight Control Systems University of Kansas Continuing Education Design Track. See page 10. 2012 Distinguished Service Award Recipient

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Orlando 42 FLIGHT CONTROL AND HYDRAULIC SYSTEMS Instructor: Wayne Stout

Day One Day Four Offering Location • Introduction and background, • Mechanism fundamentals: Location Orlando, Florida system design methodology, mechanical advantage, gearing hydraulic system overview ratios, building block mechanisms Date November 17–21, 2014 • Hydraulic fundamentals: fluid (linkages, bellcranks, overcenter, Course Number AA151240 properties (density, viscosity, dwell or lost motion, addition/ amplification, yokes, cables, bulk modulus), fluid flow (tubes, Times/CEUs orifices, servo), spool valves, spool override and disconnects, valve control, pressure transients etc.), four bar linkages, gearing Monday–Thursday 8 a.m.–4 p.m. fundamentals, gearing systems in fluid flow, conservation of mass Friday 8 a.m.–11:30 a.m. and momentum, basic hydraulic including standard/planetary Class time 31.5 hours system modeling equations, gear trains, power screws, computer-aided modeling of nonlinearities, stiffness, examples CEUs 3.15 hydraulic systems, examples of mechanical systems • Flight control system design: Day Two flight control configurations Description • Hydraulic components: operation, (reversible, irreversible, fly-by- Covers fundamental design issues, analysis, design fundamental equations for each wire), mechanization of flap/slats, methodologies for aerospace hydraulic and flight control systems. Includes design requirements, component and component flight control system design issues, component description and operation, component sizing, components include impact of certification regulations, and system math modeling, component sizing, actuators, metering valves, relief flight control system design methodology and examples system layout rationale, system sizing and airframe valves, shuttle valves, pumps, integration. Emphasizes the fundamentals and motors, check valves and fuses, Day Five necessary engineering tools (both analytical and accumulators, reservoirs, pressure otherwise) needed to understand and design regulation and flow control, • Flight control system airframe aerospace hydraulic and flight control systems. examples integration, hydraulic system Practical examples and actual systems are integration, fault detection, fly-by- presented and discussed throughout the class. Day Three wire actuation • Servovalves (flapper, jet pipe and • Flight control system failure motor controlled) modes (jams, runaways, slow Target Audience • Power Control Units (PCUs) overs), safety analysis issues and Designed for system and component level redundancy engineers and managers, including airframe, • Hydraulic system design: basic vendor, industry, government and educators system configurations, power involved with aerospace mechanical systems. generation systems, landing gear control, brake systems, flaps/ slats, spoilers, steering, thrust Fee reversers, primary flight control, $2,445 actuation examples (mechanical Includes instruction, a course notebook, Aerospace and electrical) Hydraulic System by Wayne Stout, refreshments • Hydraulic system design issues, and five lunches. impact of certification regulations, “Appreciate KU offering a class The course notes are for participants only and are hydraulic system design like this! The KU team is very not for sale. methodology, failure modes, safety well organized and they do a analysis issues and redundancy, great job with these courses.” integration with mechanical Certificate Track systems — Janice Marshall This course is part of the Flight Control Systems Thales Avionics, Inc. Design Track. See page 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 43 San Diego FLIGHT TEST PRINCIPLES AND PRACTICES Instructors: Donald T. Ward, George Cusimano

Day One Day Four Offering Location Location San Diego, California • Flight test overview and introduction • Advanced performance methods: nonstabilized performance methods, Date September 8–12, 2014 • The atmosphere: properties, altimetry, pneumatic lag; air data turning performance, ground effect Course Number AA151040 principles and measurements: measurement, getting more for less airspeed, altitude, Mach number, from flight tests Times/CEUs alpha and beta • Static stability and control: • Mass, center of gravity and moment longitudinal and lateral-directional Monday–Friday 8 a.m.–4 p.m. of inertia determination static stability testing Class time 35 hours • Time/space position measurements • Dynamic stability and control: CEUs 3.5 dynamic mode characteristics and Day Two measurement • Handling qualities: Cooper- Description • Air data calibration methods: position error Harper scale, FAR and MIL-SPEC Introduction to and definition of the requirements, workload scale basic flight test process, application of • Temperature probe, angle of attack and sideslip calibration • Parameter identification: regression engineering principles to flight test and analysis, maximum likelihood description of common flight test practices: • Instrumentation system principles: estimation of derivatives a survey of the flight test discipline design requirements, static and embellished with a variety of examples dynamic response, calibration Day Five from completed flight test programs. • Data recording and processing • Thrust drag accounting, isolation methods: analog, digital, filtering and measurement of component Target Audience and signal conditioning drags • Proper use of digital bus data (MIL- Designed for all levels of engineers and • Structural flight tests: static loads, 1553, ARINC 429, 629) for flight managers in industry working on flight flutter testing; propulsion system testing: test projects, military and civil project piston, turboprop and turbofan • Flow visualization: tufts, flow cones, engineers, test pilots and flight test engines sublimating chemicals, liquid engineers, government research laboratory crystals, dyes, smoke injection; test personnel and FAA and other regulatory • In-flight measurement of thrust and methods power agency engineers. • Spin testing: test methods, safety Day Three issues Fee • Stall tests: stall speed determination, • Systems testing and evaluation: communication, navigation, SAS and $2,445 stall characteristics, stall protections systems autopilots Includes instruction, a course notebook, Introduction to Flight Test Engineering, • Flight test program planning: Volume I, by Don Ward, Thomas Strganac organization, milestones, flight and Rob Niewoehner, refreshments and cards, documentation, procedures, five lunches. safety issues “A great course that will The course notes are for participants only • Takeoff and landings and cruise no doubt provide a great basis and are not for sale. performance: speed, range and for my career in the flight test endurance and evaluation industry.” • Climb performance: test methods, — Dominic James Welman, Certificate Track correction to standard conditions, This course is part of the Flight Tests and specific energy concepts Graduate Flight Physics Engineer Aircraft Performance Track. See page 10. QinetiQ

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 44 FLIGHT TESTING UNMANNED AIRCRAFT—UNIQUE CHALLENGES Instructor: George Cusimano

Day One Offering Location • Introduction and history Location San Diego, California • Fundamentals of flight test Date September 15–17, 2014 • Typical user requirements Course Number AA151110 • Typical UAS architecture • The role of modeling and simulation in flight testing UAVs Times/CEUs • UAV design characteristics Monday–Wednesday 8 a.m.–4 p.m. • Flight test mission planning considerations Class time 21 hours Day Two CEUs 2.1 • Fundamentals of performance flight test • Fundamentals of stability and control flight test Description • Parameter identification methods Flight testing unmanned aircraft systems (UAS) presents unique challenges seldom seen in manned flight test • Risk management programs. The sources of most of these challenges result from the Development Test and Evaluation (DT&E) of Day Three the unmanned test vehicles. This course introduces the • Human factors considerations methods and challenges associated with flight testing • UAV flight test challenges including: both remotely piloted and command directed (a.k.a. autonomous) vehicles. The course discusses UAV design – Testing without a pilot and employment principles in order to help the student – Getting off the ground understand how UAVs are flight tested and why. – Envelope expansion – Testing contingencies Target Audience – See and avoid The course is designed for practicing flight test • Lessons learned in UAV flight testing engineers, test pilots, test managers, aircraft engineers, aircraft designers and educators who already possess a • Summary and wrap-up fundamental understanding of flight test principles and practices. The course content is appropriate for civilian, military and academic researchers.

Fee $1,845 Includes instruction, a course notebook and three lunches. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Flight Tests and Aircraft Performance Track. See page 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 45 Seattle and Orlando FUNDAMENTAL AVIONICS Instructors: Albert Helfrick, Brian Butka, William Barott The course may be taught by one instructor or a combination of instructors, based on their availability.

Day One Day Four Offering Locations Location Seattle, Washington • Early history of aviation and • Inertial navigation wireless Date April 28–May 2, 2014 • Laser gyros • History of regulatory and advisory • Random Navigation, RNAV Course Number AA141380 bodies • Required Navigation Performance, • Establishment of the National RNP Displays Location Orlando, Florida Airspace System, NAS • Human factors Date November 17–21, 2014 • Federal Aviation Regulations, FAR • Electromagnetic compatibility Course Number AA151250 • European regulatory and advisory agencies • High intensity radiated fields, HIRF Times/CEUs • Radio navigation • Lightning effects Monday–Thursday 8 a.m.–4 p.m. • Antennas and radio beams Friday 8 a.m.–2:45 p.m. • Nondirectional beacon Day Five Class time 33.75 hours • VHF Omni range Airborne environment, DO-160 CEUs 3.375 • Distance measuring, DME Failure analysis Safety assessment Day Two Description Design assurance levels This course is a comprehensive study of • Long-Range Navigation, LORAN Reliability prediction, MIL-HDBK avionics from the simple stand-alone systems • Landing Systems, ILS 217 to the latest integrated systems. The theory of • Radar altimeter operation is covered as well as the environment Software considerations, DO-178 and certification processes. • Ground proximity warning Hardware considerations, DO-254 systems Flight data recorder • Terrain Awareness and Warning Target Audience System. TAWS Cockpit voice recorder Designed for avionics engineers, electronic • Satellite navigation Reliability and safety analysis testing laboratory personnel, airframe systems and flight test engineers, government research • Global positioning system, GPS laboratory personnel, FAA DERs and military Day Three personnel procuring civil equipment. • Secondary radar, Mode A/C, Mode S Fee • Collision avoidance, TCAS $2,445 • Automatic Dependent “This is a good course for Includes instruction, course notebook, Surveillance, Broadcast, ADSB system engineers to take.” Principles of Avionics, by Albert Helfrick, • Weather radar supplemental materials, refreshments and five — Huong Dinh, System Engineer lunches. • Lightning detection Rockwell Collins The course notes are for participants only and • Airborne communication are not for sale. • Aeronautical telecommunications network Certificate Track • Data buses/networking This course is part of the Avionics and Avionic • Compass/gyros Components Track. See page 10. • Air data systems

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Las Vegas 46 FUNDAMENTALS OF PROJECT MANAGEMENT FOR AEROSPACE PROFESSIONALS Instructor: Herbert Tuttle

Day One Day Three Offering Location • Understanding project • Network diagrams, team Location Las Vegas, Nevada management, leadership, improvement activities, designate obstacles to successful projects, project teams Date March 4–7, 2014 definition of teams • Cost estimating, project cost Course Number AA141310 • Project definition and system, resources, time vs. cost distinguishing characteristics, trade off Times/CEUs resources, project management • Contingency, risk, cost/schedule Tuesday–Friday 8 a.m.–4 p.m. process, typical problems, the control, project organization, triple constraint, obstacles, informal organization, Class time 28 hours project outcomes, use of project organizational forms, team CEUs 2.8 teams strategies, team development and • Strategic issues, proposals, traditional management starting successful projects, Description contract negotiation, Day Four Designed to give aerospace professionals familiarity international projects and the • Project team, sources of people, with current project management techniques. true benefits of teamwork compromise, control, support Includes identifying the functions of a project team and management team; the integration of project team, coordination, interaction, Day Two management; work breakdown structures, interfaces, subcontractors, team dynamics, communications and transfers; estimating, planning, • Internal project planning, issues, team success, team development risk and challenges of the project manager; alternative working with the customer, use of and traditional management organizational structures; control and planning of time, software, team decision making, role of internal project manager, money and technical resources. Course attendees are planning hazards theories of motivation, asked to bring a current project management problem stimulating creativity, working from your team or organization. During class you • Work breakdown structure, will work on developing a reasonable solution and a statement of work, choosing team through group problems project plan to accomplish it. players • Project cost reporting, computers, project changes, handling • Time estimating and scheduling, Target Audience other planning methods, changes, team building exercises graphical tools, time estimating, • Project or program plans Designed for engineers and other technical professionals at all levels, and new project managers productive meetings, meeting presented by participants; responsible for small as well as large and long duration record keeping, goals of meetings projects evaluated and rated projects. This course is best suited to people who • Final observations and wrap up are new to project management and current project managers who want to hone their management skills.

Fee “I found the Program Management course $2,145 to be very helpful. We covered a lot of topics Includes instruction, a course notebook, Project and were able to have good discussion. Management: A Systems Approach to Planning, Scheduling, and Controlling, by Harold Kerzner, I took away a lot of questions from the refreshments and four lunches. training that will take back to my company.” The course notes are for participants only and are not — Orlando attendee for sale.

Certificate Track This course is part of the Management and Systems Track. See page 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 47 San Diego INTEGRATED MODULAR AVIONICS (IMA) AND DO-297 Instructor: Jeff Knickerbocker

Day One Day Two Offering Location Location San Diego, California • Introductions and background • DO-297 (continued) Date September 11–12, 2014 • What is IMA? • Technical highlights of DO-297 Course Number AA151080 • What are the benefits of IMA? • Design guidelines • History of IMA and supporting • Partitioning analysis certification guidance Times/CEUs • Health management • Overview of the IMA guidance material Thursday–Friday 8 a.m.–4 p.m. • Integration • TSO-C153 (Integrated Modular Class time 14 hours • Configuration files and configuration Avionics Hardware Elements) management CEUs 1.4 • Purpose of TSO-C153 • Certification approach of DO-297 • Limitations of TSO-C153 • Six certification tasks Description • Experiences to date with TSO-C153 • Life cycle processes This course provides the fundamentals • TSO-C153 contents for developing and integrating IMA • Life cycle data systems, using TSO-C153 (Integrated • Developing a minimum performance • FAA’s plans for recognizing DO-297 Modular Avionics Hardware Elements), specification per TSO-C153 • ARINC 653 Usage in IMA Systems FAA Advisory Circular 20-145 (Guidance • Unique aspects of TSO-C153 for Integrated Modular Avionics • Using TSO-C153, AC 20-145, DO-297 (IMA) that Implement TSO-C153 • FAA Advisory Circular 20-145 and ARINC 653 together Authorized Hardware Elements) and (Guidance for Integrated Modular DO-297 (Integrated Modular Avionics Avionics (IMA) that Implement • Common challenges in IMA (IMA) Development Guidance and TSO-C153 Authorized Hardware development and certification Certification Considerations). Practical Elements) • Practical tips for IMA development and exercises and in-class activities will be • Purpose of the Advisory Circular (AC) certification used to enhance the learning process. • Technical highlights from the AC • Roles and responsibilities Target Audience Enroll in this course and Designed for developers and • Considering TSO-C153 and AC 20- Complex Electronic Hardware integrators of integrated modular 145 from various user perspectives Development and DO-254 avionics systems. The focus will be on (e.g., avionics developer and aircraft (see page 30). identifying challenges with IMA and manufacturer) satisfying the regulatory guidance. • DO-297 (Integrated Modular Avionics Save money. The cost for the (IMA) Development Guidance and two courses combined is $2,445. To Certification Considerations) enroll in both courses, use course Fee number AA151090. • Overview of DO-297 $1,425 Includes instruction, course notebook, RTCA/DO-297 Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations, refreshments and two lunches. The course notes are for participants only and are not for sale. A participant can expect to: Certificate Track • gain valuable insight into the IMA development and certification processes; • understand the importance of IMA design assurance; This course is part of the Avionics and Avionic Components Track. See • obtain practical insight into how to address some of the common IMA challenges; page 10. • understand FAA’s IMA policy and guidance. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 48 MODELLING AND ANALYSIS OF DYNAMICAL SYSTEMS: A PRACTICAL APPROACH Instructor: Walt Silva

Day One • Nonlinear systems (time domain) Offering Available as on-site course • Introduction and motivation • Definitions Contact us for a no-cost, no obligation • Brief review of mathematical concepts • Equilibrium points proposal for an on-site course: • Mathematical classification of systems • Limit Cycle Oscillations (LCO) On-site Program Manager • Linear vs. nonlinear • Bifurcations and chaos Email [email protected] Phone 785-864-8282 • Time invariant vs. time varying • Example: logistic equation • Memory vs. memoryless • Nonlinear state-space models Times/CEUs • Deterministic vs. stochastic • Linearization Class time 21 hours • Examples • Nonlinear systems (frequency domain) CEUs 2.1 • Linear systems • Power Spectrum Density (PSD) • Continuous-time systems • Linear vs. nonlinear frequency Description • Definitions dynamics • Various examples This course covers a broad range of • Convolution practical methods that will enable the • Transform techniques (s-plane) Day Three participant to accurately model and analyze real-world dynamical systems • Discrete-time systems • MATLAB using MATLAB. Topics covered include • Definitions—discretization • Basic commands the mathematical classification of • Convolution • Continuous-time state-space models systems, continuous- and discrete- time systems; transform methods, • Transform techniques (z-plane) • Discrete-time state-space models digital signal processing, state-space Day Two • Frequency analysis modeling and the use of MATLAB and Simulink to develop these models. • Linear systems (cont’d) • System identification examples • Influence coefficients, Green’s functions • Simulink and ODEs • Block Library Target Audience The intended audience includes • Orthogonality and basis functions • Sources and sinks scientists, engineers, mathematicians • Digital Signal Processing (DSP) • Models and systems and anyone with a need to develop • State-space models • Simulations and understand mathematical models of real-world dynamical systems. • System identification • Open forum and discussion

Fee Includes instruction, course notebook, An Engineer’s Guide to MATLAB and Fundamentals of Signals and Systems. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Flight What a participant can expect to learn: Control Systems Design Track. See • how to model and analyze a broad range of dynamical systems; page 10. • how to physically interpret the mathematical responses of a dynamical system; • the physical meaning of nonlinearity and time-invariance. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 49 Las Vegas OPERATIONAL AIRCRAFT PERFORMANCE AND FLIGHT TEST PRACTICES Instructor: Mario Asselin

Day One Day Four Offering Location Location Las Vegas, Nevada • Introduction • Take-off performance, basic models Date March 3–7, 2014 • Atmospheric models • Flight test Course Number AA141270 • Airspeeds • Rejected takeoff • Position errors • Presenting the information to the flight crew (AFM, flight manuals) Times/CEUs • Weight and balance Monday–Friday 8 a.m.–4 p.m. Day Two Day Five Class time 35 hours • Stall speeds and stall testing • Landing performance CEUs 3.5 • Stall warning and stall identification • Presenting the information to the flight crew (AFM, flight manuals) • Required instrumentation and data Description reduction • Consideration for contaminated runways (CAR/JAR) Overview of airplane performance theory • Testing for low-speed drag, excess • Obstacle clearance and prediction, certification standards and thrust monitoring basic flight test practices. Course will focus • Check climbs • Accounting for high temperature on turbojet/turbofan-powered aircraft deviation for minimum altitude certified under JAR/CAR/14 CFR Part 25. • High-speed drag and basic flight flights envelope limits This standard will briefly be compared to military and Part 23 standards to • Flight Envelope show different approaches to safety, certification, operational and design Day Three “Course was fantastic. Covered an entire differences. • Aircraft range semester at school in one week.” • Measuring SAR — San Diego attendee Target Audience • Data reduction Designed for aeronautical engineers in • Presenting the information to the design or flight test departments, aircrews educators, aircrews with engineering • Climbing performance background and military personnel involved in managing fleets of 14 CFR Part • WAT limits; turning performance 25 (FAR 25)-certified aircraft.

Fee A participant can expect to: $2,445 • review basic airplane performance theory; Includes instruction, a course notebook, • determine what needs to be tested to build performance models; An Introduction to Aircraft Performance, by Mario Asselin, refreshments and five • determine the required instrumentation to best measure airplane performance; lunches. • understand the scatter normally expected during flight testing and how The course notes are for participants only appropriate feedback from engineering helps the flight crew minimize this and are not for sale. scatter; • develop performance models to match flight test results; Certificate Track • understand the safety level built-in certification requirements and their impact on airplane performance; This course is part of the Flight Tests and Aircraft Performance Track. See page 10. • understand how to show compliance to the certification authorities; • learn how to present the airplane performance information to the flight crew; • understand how to set operational limits to ensure continued operational safety. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 50 PRINCIPLES OF AEROELASTICITY Instructor: Thomas William Strganac

Day One Day Four Offering Location • Overview and foundation • Flutter identification Location San Diego, California • Introduction and historical • Review of flutter models Date September 15–19, 2014 review • The flutter boundary: civilian and Course Number AA151150 • Fundamentals: definitions, military requirements, matched similarity parameters and point flutter analysis aeroelastic stability boundaries • Case studies: examples of flutter Times/CEUs • Static aeroelasticity: divergence, analysis Monday–Thursday 8 a.m.–4 p.m. lift effectiveness, control • Experiments: ground vibration Friday 8 a.m.–2 p.m. effectiveness, reversal and active tests, wind tunnel tests suppression Class time 33 hours • Introduction to dynamic Day Five CEUs 3.3 aeroelasticity: gust response, • Practice flutter, buzz • Aeroservoelasticity for flutter Description Day Two suppression Provides an in-depth understanding of aeroelastic behavior for aerospace systems. Explores • Theory • Aeroelastic tailoring aeroelastic phenomena, structural dynamics and • Principles of mechanical • Wind tunnel tests fluid-structure-control interaction; also examines vibrations • Flight tests practical issues such as ground and flight • Modal methods • Nonlinear aeroelasticity: limit tests. Topics include solution methodologies, computational methods for aeroelastic analysis, • Structural dynamics cycle oscillations, store-induced instabilities development of the operational flight boundary, • Steady and quasi-steady aeroservoelasticity and contemporary issues such aerodynamics • Concluding remarks as limit cycle oscillations and related nonlinear pathologies in aeroelastic systems. Day Three • Theory Target Audience • Unsteady aerodynamics: Designed for engineers and technical managers “Theodorsen” aerodynamics, involved in aerospace vehicle design, analysis and numerical methods and approximations, strip theory, testing. vortex and doublet lattice methods Fee • Methods of analysis $2,445 • Governing equations for the Includes instruction; a course notebook; aeroelastic system “My background is primarily Aeroelasticity, by Raymond Bisplinghoff, Holt • Frequency domain methods: in linear dynamic loads Ashley and Robert Halfman; Introduction to Flight modal formulations, V-g analysis and I considered Test Engineering, Volume II, by Don Ward, Thomas diagrams, K-method (U.S. Dr. Strganac’s short course Strganac and Rob Niewoehner; refreshments and method) and P-k method (British to be a great introduction to five lunches. method) aeroelasticity and flutter.” The course notes are for participants only and are • Time domain methods not for sale. — John Bright Aeronautical Engineer Staff Lockheed Martin Aeronautics Co. Certificate Track This course is part of the Flight Tests and Aircraft Performance Track and Aircraft Design Track. See pages 9 and 10. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 51 Las Vegas PRINCIPLES OF AEROSPACE ENGINEERING Instructor: Wally Johnson

Day One Day Three Offering Location Location Las Vegas, Nevada • Introduction • Flight maneuvers—steady maneuvers, pull-up, pitch maneuvers, yaw Date March 3–7, 2014 • Atmospheric models and airspeed measurements—Calculation maneuvers, roll maneuvers Course Number AA141280 of aircraft design airspeeds. • Mechanics of materials—material Show examples of air properties behavior under loading, stress- Times/CEUs calculations. Show examples of strain relations, beam bending and airspeed unit conversions (i.e. true to buckling, yield, compressive, tensile Monday–Thursday 8 a.m.–4 p.m. calibrated to equivalent to indicated and fatigue strengths Friday 8 a.m.–11:30 a.m. to Mach number) • Mechanical vibrations and structural Class time 31.5 hours • Introduction to certification dynamics requirements—review of the various CEUs 3.15 • Aeroelasticity—static aeroelasticity: certification agencies, requirements, divergence, control effectiveness, and certificates, review of FAA reversal; dynamic aeroelasticity: gust Description regulatory and guidance materials. response, flutter and buffet Review of various of means of The objective of this course is to provide compliance an overview and integrated exposure Day Four to airplane aerodynamics, performance, • Introduction to aerodynamics— • Structural design envelopes—Derive propulsion, flight mechanics, mass review of basic aerodynamic structural design airspeeds, design properties, structural dynamics, concepts: low speed and high speed vertical load factors (V-n diagram), aeroelasticity, structural loads, structures, aerodynamics, airfoil fundamentals, weight-cg envelope ground testing, flight testing and finite wings, aircraft aerodynamics. certification. Lecture notes are supported Overview of wind tunnel testing, • Structural loads—external loads by showing examples using Basic overview of computational fluid classifications; gust loads, landing Aerospace Engineering software. This dynamics methods loads, ground loads, fatigue loads, course shows the relationship between wing loads, horizontal tail loads, aircraft certification requirements, Day Two vertical tail loads, fuselage loads and engineering analysis and testing. control surface loads • Weight and balance—calculation of mass properties: weight, center • Aircraft structures—structural Target Audience of gravity and moment of inertia; design concept, static strength design, establishing the weight-c.g. envelope, factor of safety, material selection, This course is intended as an overview show examples of weight-cg-inertia introduction to the finite element for non-aerospace engineering-degreed method, damage tolerance design professionals, managers, military and calculations of various payload/fuel load conditions government personnel who are involved in Day Five aircraft design and certification. • Introduction to propulsion—types of propulsion systems, thrust • Ground testing: instrumentations, calculations bird strike, landing gear drop test, Fee ground vibration, ground loads • Airplane performance—review $2,445 calibration, static loads tests and basic airplane performance theory; fatigue loads tests Includes instruction, a course notebook, airspeeds, takeoff, landing and cruise a copy of Basic Aerospace Engineering performance; climb performance; • Flight testing: stall speeds, software, refreshments and five lunches. turning performance, range and longitudinal stability and control, directional stability and control, The course notes are for participants only endurance and are not for sale. flutter, flight loads validation, • Flight mechanics—aircraft axis operational loads monitoring systems, aircraft equations of motion, static and lateral-directional stability, • Course Summary Certificate Track longitudinal and lateral-directional This course is part of the Aircraft Design applied forces and moments. Aircraft Track. See page 9. dynamic stability

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 52 PROCESS-BASED MANAGEMENT IN AEROSPACE: DEFINING, IMPROVING AND SUSTAINING PROCESSES Instructor: Michael Wallace

Day One Day Four Offering Available as on-site course • Introduction • Identifying and capitalizing Contact us for a no-cost, no obligation proposal on process improvement • Overview of aerospace for an on-site course: opportunities organizational processes On-site Program Manager • Needs for continuous improvement • Conducting a self-assessment Email [email protected] • Back to basics • Systemic approach to product Phone 785-864-8282 development • Basic principles • Enterprise process model • Data gathering methods Times/CEUs • The economics of quality • Decomposing processes Class time 35 hours • Quality management system • Setting performance goals CEUs 3.5 • Pitfalls and how to avoid them • Process ownership • Case studies • Critical success factors Description Provides basic principles and the tools and • Process mapping Day Five techniques of Process Based Management • Case studies (continued) Day Two (PBM) and delineates the strategies for • Advance process management successful implementation of PBM in an • Process measurement techniques and tools aerospace organization. Focuses on how to • Defining process measures • Performance improvement system depict an enterprise process view, develop process measures, define key components • Process measures at the • Knowledge management organizational level (balanced and identify critical success factors to maintain scorecard) • Process modeling the focus on priority requirements for managing processes to achieve sustainable • Identifying and controlling • Knowledge-based engineering performance improvements. Several aerospace variation • Artificial intelligence organizational case studies are used to • Diagnostic tools • Summary and wrap-up augment the theoretical components. • Basic Six Sigma tools • Benchmarking Target Audience • Change management Managers, engineers, quality, IT and planning • Risk management professionals in aerospace industry responsible for the identification, implementation and Day Three improvement of existing organizational • Cultural focus “This course opened my eyes for processes and development of new processes necessary to compete in the future. • Integration of strategy and process stuff that I never thought. It was management very good and will help me to • Role of the leadership team help people from my company.” Fee • Team based decision-making — Las Vegas attendee Includes instruction and a course notebook. methods The course notes are for participants only and • Self-directed work teams are not for sale. • High-performance work teams • Organizational relationships Certificate Track • Facilitation skills This course is part of the Management and Systems Track. See page 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 53 On-site Course PROPULSION SYSTEMS FOR UAVS AND GENERAL AVIATION AIRCRAFT Instructor: Ray Taghavi

Day One Day Three Offering Available as on-site course Contact us for a no-cost, no obligation • Overview: Fundamentals of aircraft • Aircraft reciprocating engines propulsion systems, engine types and (continued): carburetion and fuel proposal for an on-site course: aircraft engine selection injection systems, FA DEC; magneto On-site Program Manager • Aircraft reciprocating engines: spark (high and low tension), battery and Email [email protected] electronic ignition systems, ignition Phone 785-864-8282 ignition and diesel engines: theory and cycle analysis, four stroke and boosters and spark plugs two stroke cycles; brake horsepower, • Rotary engines: propeller: theory, Times/CEUs indicated horsepower and friction types airfoils, material, governors, horsepower; engine parameter, feathering, reversing, synchronizing, Class time 35 hours efficiencies, classifications and scaling synchrophasing, de-icing, anti-icing CEUs 3.5 laws; practical issues and reduction gears Day Two Day Four Description • Aircraft reciprocating engines • Small gas turbine engines: cycles, inlets, Provides in-depth understanding of (continued): components and compressors, combustors, turbines, state-of-the-art propulsion issues for classification: cylinder, piston, exhaust systems, thrust reversers and UAVs and general aviation aircraft, connecting rod, crankshaft, crankcase, noise suppressors; turbojet, turboprop, including propulsion options, cycle valves and valve operating mechanism; turboshaft, turbofan and propfan analysis, principles of operation, lubrication systems, pumps, filters, engines systems, components, performance oil coolers, etc.; induction system, and efficiency calculations. supercharging, cooling (air and Day Five liquid), exhaust engine installation • Engine noise: sources, suppression, and compound engine; engine knocks Target Audience measurement techniques and practical (pre-ignition and detonation), aviation issues Designed for propulsion engineers, fuels, octane and performance number, • Foreign Object Damage (FOD): ice, aircraft designers, aerospace industry backfiring and afterfiring sand, bird managers, educators, research and development engineers from NASA, • Engines for special applications: UAVs, FAA and other government agencies. RPVs, HALE, blimps

Fee Includes instruction and a course notebook. The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Aircraft Design Track. See page 9.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Online Course 54 RELIABILITY AND 1309 DESIGN ANALYSIS FOR AIRCRAFT SYSTEMS (Online Course) Instructor: David L. Stanislaw

This course addresses the analysis techniques that an applicant needs to know when Offering Online Instruction designing and certifying complex systems on a modern aircraft, according to the FAR 1309 rules. Available anytime Class time 28 hours Participants are guided through the 28 course sections and have the flexibility to CEUs 2.8 complete the sections and readings on their own time within a six-month time frame. Interaction with the instructor takes place via email. Description Lesson Sections and Title Covers requirements of FARs 23.1309, 1 National Transportation Safety Board Accident Statistics 25.1309, 27.1309 and 29.1309 from 2 Learning from an Analysis of Power Industry Accidents fundamental analysis techniques to system integration; includes construction 3 AOPA Nall Report and Boeing Statistical Summary of failure mode and effects analysis, 4 Pilot Causes of Accidents—Dr. Milton Survey criticality analysis and fault trees. Includes 5 Safety in Aviation—Dr. Ir. H. Wittenberg detailed review of SAE ARP 4754 and ARP 6 Historical 1309 Rules 4761. Principles apply to all critical and 7 Understanding FAR 25.1309 essential aircraft systems. 8 Built-in—Test and Probability Perspective Fault Tree Handbook 9 RTCA DO-167 Airborne Electronics Reliability Target Audience 10 MIL—HDBK—217 Reliability Prediction of Electronic Equipment AFSC 7 Part Designed for Parts 23, 25, 27 and 29 Derating Guidelines system certification engineers, airframe 11 RAC Electronic Parts Reliability Data system designers, FAA-Designated 12 RAC Nonelectric Parts Reliability Data Engineering Representatives (DERs), 13 RAC Failure Mode/Mechanism Distributions aircraft certification personnel and military personnel procuring civil 14 DOD—HDBK—763 Human Engineering Procedures Guide equipment. 15 DOT/FAA/RD—93/5 Human Factors for Flight Deck Certification 16 JAR—VLA—1309, FAR 23.1309 and FAR 25.1309 Review 17 FAA Advisory Circulars Fee 18 SAE ARP4761 Safety Assessment Guidelines SAE ARP4754 Guidelines $1,485 19 MIL—STD—1629 Procedures for Performing a Failure Mode, Effects and $35 (USD) shipping within the U.S. Criticality Analysis $95 (USD) shipping to Canada and other 20 RTCA DO—178B Software Considerations in Airborne Systems international locations. 21 RTCA DO—254 Design Assurance Guidance for Airborne Electronic Hardware Fee includes instruction online, two 22 FAA Order N8110.37 Delegated Functions and Authorized Areas course notebooks, Fault Tree Handbook, 23 FAA AC 23.1309 Equipment, Systems and Installations by D.F. Haasle, SAE ARP 4754A—Guidelines 24 AC 25.1309 System Design and Analysis for Development of Civil Aircraft and 25 AMJ 25.1309 Advisory Material Joint Systems and SAE ARP 4761—Guidelines and Methods for Conducting the Safety 26 AC 25—19 Certification Maintenance Requirements Assessment Process on Civil Airborne 27 Databus Architectures and Interference Systems and Equipment. 28 Electric Lavatory Heater Exercise The course notes are for participants only and are not for sale. The course notebook and supplemental readings will be mailed upon receipt of payment. Certificate Track This course is part of the Aircraft Maintenance and Safety Track and Aerospace Compliance Track. See pages 9 and 10.

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 55 California, Maryland ROTORCRAFT VIBRATION: ANALYSIS AND PRACTICAL REDUCTION METHODS Instructor: Richard L. Bielawa

Day One Day Three Offering Location Location California, Maryland • Introduction: overview of rotorcraft • Fuselage vibrations (continued): modal structural dynamic problems and identification, techniques for achieving Date June 9–13, 2014 solutions response modification, antiresonance Course Number AA141420 • Mathematical tools: linear systems, theory, methods for vibration alleviation, Fourier analysis, damping, multiple- elastomeric devices, vibration testing degree-of-freedom systems, natural applied to material characterization Times/CEUs modes, resonance, stability • Linear stability analysis methods: Monday–Thursday 8 a.m.–4 p.m. • Rotational dynamics and gyroscopics: constant coefficient systems, force phasing Friday 8 a.m.–11:30 a.m. simplified gyroscope equation, matrices, Floquet theory, frequency- domain methods Class time 31.5 hours precessional characteristics of rotors • Blade aeromechanical instabilities: CEUs 3.15 • Dynamics of rotating slender beams: hinged rigid blades, effects of elastic air mass dynamics, quasi-steady restraints about the hinges, the Euler aerodynamics, pitch-flap-lag and flap-lag Description beam and basic DEQ for transverse instabilities bending, rotor speed characteristics • Problem session Material is presented for acquiring familiarity with both the underlying and fan plots, out-of-plane vs. inplane physics and the analytical tools needed bending, Yntema charts and numerical Day Four methods for bending modes, the two- for addressing rotorcraft vibration • Linear unsteady aerodynamics: general bladed rotor, torsional dynamics, coupling phenomena. Topics include a review of frequency domain theories, finite state appropriate mathematical techniques, issues, experimental verification and formulations gyroscopic theory, blade natural tracking and balancing, blade section frequency characteristics, drive system properties, the SECT_PRT computer code, • Bending-torsion flutter: basic flutter dynamics, vibration alleviation devices, blade natural frequencies, the BLAD_ theory, bending-torsion of rotor blades, rotorcraft instability phenomena and general analysis methods testing procedures. While some new FREQ computer code analysis techniques are introduced, • Problem session • Nonlinear aeroelastic stability analyses: the course will address familiarization nonlinear unsteady aerodynamics, stall with the physics using traditional flutter, BOOT and SHOT methodology. Day Two • Transverse vibration characteristics: • Rotor-fuselage coupled instabilities: the Jeffcott rotor model, subcritical propeller-nacelle whirl flutter, ground Target Audience and supercritical operation, pseudo- resonance, air resonance Designed for those engineers and gyroscopic effects, whirl speeds and • Software for ground and air resonance educators involved in rotorcraft modes and rotor instabilities calculations research, design, development and/ • Basic balancing techniques or testing who seek an understanding • Problem session of and solutions to rotorcraft vibration • Torsional natural frequencies of issues in contemporary rotorcraft. shafting systems: element equivalences, Day Five basic natural frequency calculations, • Testing for dynamics at model and full Fee branched gear systems, drive system for scales: model scaling law, instrumentation a typical rotorcraft, drive system natural and test procedures, methods for $2,445 frequencies, the TORS_HDS computer instability quenching code, problem session Includes instruction, a course notebook, • Methods for quantifying stability CD, Rotary Wing Structural Dynamics and • Problem session Aeroelasticity, Second Edition, by Richard L. • Special topics: aeroelastic optimization, Bielawa, refreshments and five lunches. • Fuselage vibrations basic issues: forced composite blade design, drive system response and vibrations, the rotor as an The course notes are for participants compatibility with engine/fuel control excitation source and filter, rotor-fuselage only and are not for sale. systems-analysis techniques, stabilization interaction, 1P vibrations, the two-bladed rotor • Summary and future trends Certificate Track • Full-scale vibration testing of real systems: This course is part of the Flight Tests suspension and excitation techniques, and Aircraft Performance Track. See instrumentation, typical shake-test results page 10. for helicopters, operational modal analysis aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Las Vegas 56 RTCA DO-160 QUALIFICATION: PURPOSE, TESTING AND DESIGN CONSIDERATIONS Instructor: Ernie Condon

Day One Day Three Offering Location • Aircraft environment • Magnetic effect Location Las Vegas, Nevada • Overview of RTCA and DO-160 • Power input Date March 4–7, 2014 • Advisory Circular AC 21-16G • Voltage spike Course Number AA141320 • Requirements development and • Audio frequency conducted management susceptibility Times/CEUs • Conditions of tests • Induced signal susceptibility Tuesday–Friday 8 a.m.–4 p.m. • Temperature and altitude Day Four Class time 28 hours • Temperature variation • RF susceptibility CEUs 2.8 • Humidity • RF emission • Shock and crash safety • Lightning indirect susceptibility Description • Vibration • Lightning direct effects This class is designed to educate system engineers, • Explosion proof hardware design engineers and test engineers in the • ESD aspects of DO-160 as it pertains to the equipment Day Two qualification in support of aircraft certification. For system and hardware engineers, the intent is to educate and • Waterproofness empower them to develop equipment designs that are • Fluids susceptibility compliant with DO-160 by design and avoid expensive redesigns to correct issues found late in the development • Sand and dust cycle during test. For test engineers, it is intended to assist them to properly develop test plans for their products. • Fungus resist For each test section of DO-160, we provide Purpose, • Salt fog Adverse Effects, Categories, a high level step-by-step through the test procedure, and Design Considerations • Icing for passing the test. Also included is an overview of a • Flammability top-down requirements management approach (systems engineering), review of related FAA advisory material, and overview grounding and bonding, wire shielding practices, and lightning protection for composites.

Target Audience “Very informative course. Instructor’s knowledge This class is designed for system engineers responsible of the subject and his experience as DER also adds for developing requirements for airborne electronic equipment; hardware design engineers responsible for tremendous value to course content. His sense of building such equipment and test engineers responsible humor also kept the course lively and interesting.” for writing test plans. — Tanveer Shakeel, Mechanical Systems Engineer Pilatus Aircraft Limited Fee $2,145 Includes instruction, a course notebook, DO-160 Environmental Conditions and Test Procedures for Airborne Equipment, refreshments and four lunches. What a participant can expect to learn: The course notes are for participants only and are not for sale. • the purpose of each test, and the adverse effects that the test is intended to prevent; Certificate Track • the ability to properly assign test categories and test levels; This course is part of the Avionics and Avionic • a basic understanding of each test procedure; Components Track. See page 10. • design considerations to meet the test requirements. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 57 San Diego SOFTWARE SAFETY, CERTIFICATION AND DO-178C Instructor: Jeff Knickerbocker

Day One Day Three Offering Location Location San Diego, California • Introductions and background • Quality assurance (QA) objectives, QA philosophy, SQA approaches, Date September 15–18, 2014 • Differences between DO-178B and DO-178C certification liaison objectives, life Course Number AA151120 cycle data • DO-178C supplemental documents and where they fit • Supplements including DO-330— Times/CEUs Tool Qualification, DO-331—Model • Overview of existing standards Based Development, DO-332— Monday–Thursday 8 a.m.–4 p.m. related to software safety Object Oriented, and DO-333— Class time 28 hours • Tie between the system, safety and Formal Methods CEUs 2.8 software processes • Special topics—partitioning and • History, purpose, framework and protection, structural coverage, layout of DO-178C dead and deactivated code, Description service history, Commercial- • Reading the Annex A Tables Provides the fundamentals of developing and Off-The-Shelf (COTS) software assessing software to the standard RTCA/DO-178B • Configuration management, FAA software-related policy and and RTCA-DO-178C Software Considerations in configuration management guidance—software review process, Airborne Systems and Equipment Certification as objectives and terminology, control user-modifiable and field-loadable well as associated RTCA/DO-178C supplements in categories software, change impact analysis, DO-330, DO-331, DO-332 and DO-333. Similarities tool qualification, previously and differences to RTCA/DO-278A for CNS/ATM equipment will also be addressed. The course also Day Two developed software, software provides insight into the FAA’s software review • Development and integration/ reuse, integrated modular avionics, process, the FAA’s software policy, practical keys for test processes—development databases (DO-200A), complex successful software development and certification, objectives, high-level requirements, hardware (DO-254) common pitfalls of software development and traceability, design (low-level software challenges facing the aviation community. Day Four Practical exercises and in-class activities will be used requirements and architecture), to enhance the learning process. code/integration, integration/test • Assessing compliance—the objectives, normal and robustness Software Job-Aid testing Target Audience • Planning process • Verification processes—overview • Common pitfalls Designed for software developers, avionics of verification, verification of engineers, systems integrators, aircraft designers requirements, design, code and • Software challenges facing the and others involved in development or testing aviation industry: off-shore implementation of safety-critical software. The development, use of real-time focus is on civil aviation, certification and use of RTCA/DO-178C; however, the concepts may be operating systems and other applicable for other safety domains, such as military, commercially available components, medical, nuclear and automotive. software reuse

Fee $2,145 Includes instruction, a course notebook, the RTCA/DO- A participant can expect to: 178C Software Considerations in Airborne Systems and • develop and document efficient RTCA/DO-178C and DO-278A compliant Equipment Certification, refreshments and four lunches. processes; The course notes are for participants only and are not for sale. • create, capture and implement compliant requirements, design data and source code; Certificate Track • evaluate compliance to RTCA/DO-178C and understand the how to integrate DO-178C supplements; This course is part of the Avionics and • generate and adhere to effective verification strategies; Avionic Components Track. See page 10. • understand FAA’s software-related policy and guidance. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 58 STRESS ANALYSIS FOR AEROSPACE STRUCTURES (NEW) Instructor: Dennis C. Philpot

Day One Day Three Offering Location • Introduction • Analysis of Bolted Joints Location San Diego, California • Engineering Mechanics Review • Anatomy of a Bolted Joint (Free Body Diagram) Date September 16–19, 2014 • Introduction to Solid Mechanics • Estimating Joint Constants Course Number AA151170 • The Importance and Usefulness of Free Body • The Bolted Joint Diagram Diagrams • Calculation of Critical External Load • Two-Dimensional Theory of Elasticity • Failure Modes of Bolted Joints Times/CEUs • The Airy Stress Functions • Analysis of Bolts Loaded in Tension Tuesday–Friday 8 a.m.–4 p.m. • Analysis of Trusses • Analysis of Bolts Loaded in Shear Class time 28 hours • Analysis of Beams • Interaction Equation for Combined Loading CEUs 2.8 • Stability Analysis of Columns • Fatigue and Life Prediction Analysis • Analysis of Torsion Rods • A Brief History of Fatigue Failure Description • Energy Methods in Mechanical Analysis • Mechanism of Fatigue Failure This course is designed for the practicing • The Usefulness of Energy Methods • Fatigue Stress Concentration Factor and engineer who has an interest in the various • Energy Theorems Notch Sensitivity aspects of stress analysis in aerospace structural- mechanical design and would like to enhance • The Principle of Stationary Potential Energy • Endurance Limit Modifying Factors his or her expertise in this important field. Topics include engineering mechanics, deterministic • Strain Energy in a Variety of Structural • Modified Goodman Approach stress analysis, prevention of failure of ductile Elements • Gerber and ASME-elliptic relations and brittle materials, fatigue and fracture • The Rayleigh-Ritz Method mechanics, analysis of bolted joints, dynamic • Fatigue Crack Propagation and Paris’ Law loading and design optimization. Throughout • Lagrange’s Equations of Motion the course, equal attention is given to both the • Damage Tolerance and Fracture Control theory and practice of classical analysis as well • Finite Element Method Discussion as modern (numerical/computational) methods Day Four used in the industry. Day Two • Dynamic Loading • Failure Prevention of Engineering Materials • A Survey of Dynamic Loads Target Audience • The Stress Analyst’s Primary Task • What We Mean by “Quasi-Static Loads” • Design engineers who would like to become • Deterministic vs. Probabilistic Stress Analysis • Mode Shapes, Boundary Conditions and more familiar with the techniques and • Design Criteria and Product Specifications Natural Frequencies modern practices of stress analysis to help them be more efficient and productive in • Computation of Margins of Safety • Equations of Motion for Second-Order their work Systems • Failure by Material Distortion • Mechanical engineers who have been out • Response of Second-Order Systems to of college for a while and need to become • Ductile Rupture after Extensive Deformation Harmonic Loads more competent in the area of stress analysis • Sudden Fracture of Brittle Materials due to a particular job assignment or new • Response of Second-Order Systems to Shock career opportunity that requires expertise in • Progressive Fracture through Material Fatigue Loading analyzing structures • Fundamentals of Deterministic Stress Analysis • Introduction to Random Vibration • Department managers whose staff are involved in stress analysis work • Definition of Stress • Linear Response to Random Vibration • Generalized Hook’s Law • Numerical Optimization Fee • Equilibrium of a 2-D Stress Element • Introduction and Motivation $2,145 • Derivation of the Principal Stresses • The Optimization Problem Includes instruction, a course notebook, • Mohr’s Circle of Stress • Unconstrained and Constrained Design refreshments and four lunches. Problems • Static Failure Theories for Ductile Failure The course notes are for participants only and • Static Failure Theories for Brittle Failure • Optimization Software are not for sale. • Stress Concentration Factors in Mechanical • Structural Optimization Design • The Finite Element Method Certificate Track • Linear Elastic Fracture Mechanics (LEFM) • Multidiscipline Design Optimization This course is part of the Aircraft Design Track. Approach • Closing Remarks See page 9. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 59 San Diego STRUCTURAL COMPOSITES Instructor: Mark S. Ewing

Day One Day Four Offering Location Location San Diego, California • Introduction/historical • Composite laminate/part/ review of composites usage assembly design guidelines Date September 15–19, 2014 • Constituent materials— • Lamination rules Course Number AA151160 fibers, matrix • Hygro-thermal effects • Analysis tools/formulas to • Interlaminar and free-edge Times/CEUs predict mechanical properties effects of fibers, resins, plies Monday–Friday 8 a.m.–4 p.m. • Durability/environmental Class time 35 hours • Manufacturing introduction issues (impact, fatigue, temp, humidity, EME) CEUs 3.5 Day Two • Design problems • Analysis tools/formulas Description to predict laminate (stack) Day Five elastic properties (classical An introduction to high performance composite materials, lamination theory, ABD • Software tools for stress, covering both engineering and manufacturing of composite parts manufacturing and assemblies. Class starts with the basic material properties of matrices) the constituents (fiber and matrix), how they combine to form • Constituent materials— • Design project continued plies and how to obtain ply properties, how plies combine to weaves, foam and honeycomb form laminates and how to obtain the laminate properties. Other • Summary and wrap-up engineering topics include stress analysis, failure criteria and cores, adhesives testing methods. To further reinforce the learning process, case • Coupon level testing studies and lessons learned are discussed. Towards the end of methods, how to use and the week, the class becomes more participatory in nature, as the class breaks up into 4–5 person teams, each working on design interpret the data projects aimed at building confidence with the material and cover • Manufacturing high areas of special interest or weakness. The teams will be asked to performance composites produce a preliminary design package consisting of drawings and sketches, loads, stress and weight analysis, material selection, • Sandwich cores, adhesives, fabrication process description, tool design, and preliminary cost fasteners and production rate analysis. Day Three “This course is exactly Target Audience • Failure theories and their limitations, proper use of the what I needed. The course has proven very helpful to (1) those wanting a broad theories Composites are now overview and/or a crash course in composites, (2) experienced engineers looking for a refresher course, (3) stress engineers • Inspection methods showing up everywhere. wanting to understand how composites really work or fail and Understanding fiber • Manufacturing discussions what to look out for when analyzing parts, data and margins, (4) orientation and the effects practicing engineers and managers with metal experience wishing (cure cycles, processing, to expand their skill set, (5) anyone wanting to jump into the field defects, inspection) of lightning is something but does not know how to go about it, and (6) engineering teams that I was needing embarking on new projects involving composites. • Tooling design, issues, materials, costs for proper composites • Bonded and bolted joints, repair design schemes. Fee how to design and analyze A top notch course $2,445 and presentation.” Includes instruction, a course notebook, refreshments and five — Harlon Parchment lunches. US Coast Guard The course notes are for participants only and are not for sale.

Certificate Track This course is part of the Aircraft Structures Track. See page 10. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 On-site Course 60 SUBCONTRACT MANAGEMENT IN AEROSPACE ORGANIZATIONS Instructor: Robert Ternes

Day One Day Three Offering Available as on-site course • Overview of course goals and • Delivery considerations Contact us for a no-cost, no obligation proposal for discussion of intended outcomes • Contract close-out activities and an on-site course: • Discussion of typical aerospace the tools and techniques used On-site Program Manager environment and needs • Application of special quality Email [email protected] • Review of contents of agreement activities such as First Article Phone 785-864-8282 • Discussion of risk mitigation inspections techniques • Configuration management Times/CEUs issues and tools • Discussion of negotiation tools Class time 21 hours • Cost limitations • Cost and risk limitation techniques CEUs 2.1 • How to clarify communication issues • Communication of status (when, how, what) to all parties Description • How to identify and manage schedule considerations • Collection and sharing of lessons Nearly every aerospace organization now learned develops products with subcontracted activities. • How to identify and implement Unfortunately, this practice frequently leads to opportunities • Class exercise/summary/ evaluation inefficiencies and increased risks. Subcontract • Class exercise/summary of day and Program managers bear the majority of this increased risk. This course is designed to provide Day Two you with tools to reduce that risk and increase • Tasks to perform during contract the effectiveness of the subcontractors that you execution manage. The processes, tools and techniques applied to managing lower-tier subcontracts • Tools and techniques used to are thoroughly covered and examples of both measure and control quality and successful and unsuccessful cases are discussed, as progress well as integration with existing policies. • Corrective actions: when, why and how Target Audience • Risk management techniques Development or project managers responsible • Cost and schedule considerations for managing the lower tier aerospace/aviation during execution phase suppliers contracted to deliver product on schedule • Communications upward, and within the required cost, quality and regulatory downward and horizontally envelopes typical of an aerospace product. • Class exercise/summary of day Fee Includes instruction and a course notebook. The course notes are for participants only and are not for sale.

Certificate Track A participant can expect to learn: This course is part of the Management and Systems • critical items that should be in every subcontract; Track. See page 10. • ways to measure subcontractor effectiveness; • better ways to create management and progress reports; • methods to improve the effectiveness of the subcontract manager; • techniques to recover when problems occur. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 61 San Diego SUSTAINMENT AND CONTINUED AIRWORTHINESS FOR AIRCRAFT STRUCTURES Instructor: Marv Nuss

Day One Day Three Offering Location Location San Diego, California • Background of sustainment • The importance of non-destructive requirements. Focus on evolution evaluation for damage tolerance Date September 8–11, 2014 of FAA design, maintenance and based inspection programs. Course Number AA151010 inspection regulations related to Introduction to common methods continued airworthiness and discussion about reliability and probability of detection (POD) Times/CEUs • Overview of fatigue management programs (FMP) as they relate to • Class exercise Monday–Thursday 8 a.m.–4 p.m. structural sustainment. Similarity • The importance of complete Class time 28 hours between civil and military Instructions for Continued CEUs 2.8 requirements Airworthiness (ICA). Discussion • Static strength analysis for repairs of regulatory requirements and and alterations, including a class recommended ICA content Description exercise • FMPs—how static strength, Introduction to aircraft sustainment and fatigue strength, damage tolerance, continued airworthiness requirements. Use Day Two of basic static, fatigue and damage tolerance inspection reliability and ICA fit analysis methods for repairs and alterations. • Aircraft flight profiles and spectrum together. Address widespread fatigue Best practices for setting up fatigue development for use in fatigue damage (WFD) and limitations of management programs and documentation evaluations, including a class exercise FMPs of instructions for continued airworthiness. • Aircraft fatigue analysis for Exposure to regulations, compliance policy Day Four and guidance, and technical references. Class repairs and alterations using basic exercises provide hands-on experience of concepts—material properties, stress • Repair and alteration approvals simple analysis methods. Relevant reference concentrations, Miner’s rule using supplemental type certificates material provided with class notes. • Class exercise and field approvals. Return to service approvals, service difficulty • Aircraft damage tolerance analysis reporting, major/minor repairs. How Target Audience for repairs and alterations using basic operators use MSG-3 process concepts—material properties, stress Designed for engineers, regulators, • Corrosion as it relates to sustainment maintainers, inspectors and their managers intensity, residual strength, crack working continued airworthiness design growth • Continuing airworthiness for and compliance. Typical organizations are • Class exercise composite structure commercial and military aircraft OEM and operator sustainment groups, air logistics • Risk assessment and risk centers, repair stations and regulatory management concepts oversight agencies. • Related topics, special issues, and wrap up Fee $2,145 Includes course notebook, CD, refreshments “Combination between academic theories and and four lunches. real case applications to efficiently explain aircraft The course notes are for participants only structure and continued airworthiness really worked and are not for sale. well so that I could cover from the overall concept to practical implementation. I really recommend to try Certificate Track this course to deepen your knowledge as well as to This course is part of the Aircraft Structures figure out how to apply in real situation.” Track, Aerospace Compliance Track and — Jung Soo Ho, Captain Aircraft Maintenance and Safety Track. See pages 9 and 10. DAPA

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 62 UNMANNED AIRCRAFT SYSTEM SOFTWARE AIRWORTHINESS Instructor: Willie J. Fitzpatrick, Jr.

Day One Offering Location • Introduction and overview of UAS software requirements Location San Diego, California • Software acquisition/development and relationship to software Date September 9–11, 2014 airworthiness in unmanned aircraft systems Course Number AA151060 • Software airworthiness in the context of the system safety/ airworthiness program • Software airworthiness products during the system life-cycle Times/CEUs • Software airworthiness assessment process during the system life-cycle Tuesday–Thursday 8 a.m.–4 p.m. Class time 21 hours Day Two CEUs 2.1 • Assessment of planning and requirements analysis • Assessment of preliminary and architectural design Description • Assessment of detailed design Covers the software airworthiness requirements • Assessment of coding and unit test for unmanned aircraft systems. It will address the development and airworthiness evaluation of • Assessment of software integration and formal qualification test complex integrated software intensive unmanned • Assessment of system integration test and aircraft integration/ground aircraft systems as well as the relationship between test/flight test the acquisition/development processes for these systems and the key software airworthiness Day Three assessment processes. The course also identifies the deliverables, artifact requirements and approaches • Developing recommendations for formal flight release/airworthiness for documenting the software airworthiness release to approval authority assurance case, which is required to ultimately • Documenting the UAS software airworthiness assurance case provide the certification/qualification basis for approval of the airworthiness of the unmanned • Useful guidebooks, handbooks and procedures in UAS software aircraft system. airworthiness • Keys to successful software airworthiness process implementation for UAS Target Audience • Problem areas and concerns This course is intended for managers, systems engineers, software system safety engineers and • Future trends in UAS software airworthiness software engineers who design, develop or integrate unmanned aircraft systems or evaluate these systems to provide the qualification/certification basis for their software airworthiness.

Fee $1,845 Includes instruction, course notebook, CD and three lunches. The course notes are for participants only and are not A participant can expect to learn: for sale. • key elements required to evaluate or achieve the successful airworthiness substantiation of Unmanned Aircraft System software; Certificate Track • techniques and approaches for documenting and evaluating the This course is part of the Avionics and Avionic software substantiation/safety case for acceptance by the Unmanned Components Track. See page 10. Aircraft System Airworthiness Qualification/Certification Authority; • the application of acquired knowledge and skills to real world scenarios. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 63 Instructor Bios OUR OUTSTANDING INSTRUCTORS

Robert D. Adamson holds an M.S.A.E. degree from the Delft University of Technology in The Netherlands and a Ph.D. in aerospace FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement engineering from The University of Kansas. of Commercial Derivative Aircraft/Systems, p. 36 FAA Functions and Requirements Leading to Mario Asselin Airworthiness Approval, p. 38 Airplane Performance: Theory, Applications and Certification (Online Course), p. 24 Robert D. Adamson is a private consultant with more than 30 years of experience in the design, certification Operational Aircraft Performance and Flight Test and management of FAR Part 23 and Part 25 aircraft Practices, p. 49 projects. He was employed by Raytheon Aircraft for Mario Asselin is chairman of Asselin, Inc., a company 15 years, holding positions of propulsion engineer, that provides engineering services in performance, system safety engineer, Designated Engineering stability and control. He is manager flight test center Representative (DER) and Airworthiness Engineer engineering for Bombardier Flight Test Center in (AR) before joining the FAA in 1998. During his FAA Wichita, KS, and is an FAA flight analyst DER. Asselin tenure, he held positions as a propulsion specialist and previously held positions as Manager Flight Test Team program manager for Continued Operational Safety CSeries at the Bombardier Flight Test Center in Wichita, in the Wichita Aircraft Certification Office. He has a senior manager of engineering flight test with Honda B.S. from Southwestern and completed post-graduate Aircraft Corporation, vice president of engineering with requirements from Embry-Riddle University. Sino Swearingen Aircraft Corporation, Learjet’s chief of stability and control at the Bombardier Flight Test Willem A.J. Anemaat Center in Wichita, chief technical for the aerodynamic Airplane Flight Dynamics: Open and Closed Loop, design and certification of Bombardier’s CRJ-900 and p. 23 Transport Canada DAD. He has taught courses for the Royal Military College of Canada, McGill University Airplane Preliminary Design, p. 25 and Concordia University in Montreal. He is the Airplane Aerodynamic Design and Subsonic Wind author of An Introduction to Aircraft Performance. Tunnel Testing, p. 22 Asselin holds a B.E. in mechanical engineering from the Royal Military College of Canada and an M.Sc.A. Willem A.J. Anemaat is president and co-founder in aerothermodynamics from École Polytechnique of of Design, Analysis and Research Corporation Montreal. (DARcorporation), an aeronautical engineering and prototype development company. DARcorporation specializes in airplane design and engineering Richard L. Bielawa consulting services, wind and water tunnel testing and Rotorcraft Vibration: Analysis and Practical design and testing of wind energy devices. Anemaat is Reduction Methods, p. 55 the software architect for the Advanced Aircraft Analysis Richard L. Bielawa, president of R.L. Bielawa Associates, software, an airplane preliminary design tool. He has Inc., has consulted for numerous aerospace companies in been actively involved with more than 350 airplane diverse areas relating to rotary-wing structural dynamics design projects and has run many subsonic wind tunnel and aeroelasticity, wind energy systems development and tests for clients. Anemaat has more than 25 publications the flight dynamics of spacecraft. Bielawa has more than in the field of airplane design and analysis. He is the 40 years of experience in teaching and industrial and recipient of the SAE 2010 Forest R. McFarland Award, academic-based research. He served as lecturer in the a member of the AIAA Aircraft Design Technical department of mechanical and aerospace engineering Committee, an AIAA Associate Fellow and an associate at UCLA, senior research engineer at the department editor for the AIAA Journal of Aircraft. Anemaat of aerospace engineering at the Georgia Institute of

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Technology and associate professor in the department Board of Trustees for the Association for Unmanned of mechanical engineering, aeronautical engineering Vehicle Systems International. He is the 2003 recipient of and mechanics at Rensselaer Polytechnic Institute. the SAE Clarence L. “Kelly” Johnson Aerospace Vehicle Previously, Bielawa was a senior research engineer at Design and Development Award. He is a Fellow of the United Technologies Research Center. He holds a B.S.E. AIAA, an instrument-rated commercial pilot and flight from the University of Illinois and an M.S.E. from instructor. Chaput holds a B.S., M.S. and Ph.D. from Princeton University, both in aerospace engineering, and Texas A&M University, all in aerospace engineering. a Ph.D. from the Massachusetts Institute of Technology in aeronautics and astronautics engineering. Richard Colgren Conceptual Design of Unmanned Aircraft Systems, Brian Butka p. 31 Fundamental Avionics, p. 45 Richard Colgren is a former associate professor of Brian Butka is an associate professor of electrical, aerospace engineering at the University of Kansas computer, software and systems engineering at Embry- and is vice president of Viking Aerospace. He has 30 Riddle Aeronautical University in Daytona Beach, years of professional experience within the aerospace Florida. His research interests are in autonomous aerial industry. He has been an adjunct professor at the vehicles, safety-critical hardware design and advanced University of Southern California and California State passive radar applications. He has more than 12 years of University, Long Beach and Fresno. His research focus analog/mixed signal and VLSI circuit design experience is on intelligent vehicle systems and controls. Colgren at Integrated Device Technology (IDT) where he was is an Associate Fellow of the AIAA, has more than 130 a principal engineer. Prior to IDT, he was an assistant publications and holds four patents. Colgren received professor for six years at the United States Naval a B.S. in aeronautical and astronautical engineering Academy. He has also served as an adjunct professor at from the University of Washington, an M.S. in electrical Georgia Institute of Technology. Earlier in his career, he engineering from the University of Southern California was process design engineer at Westinghouse Electric and a Ph.D. in electrical engineering with an emphasis Corporation and product engineer at Texas Instruments. in systems, and a minor in aerospace engineering, from Butka has a B.S. in electrical engineering from the University of Southern California. Syracuse University, and an M.S. and Ph.D. in electrical engineering, both from Georgia Institute of Technology. Ernie Condon Aircraft Lightning: Requirements, Component Armand Chaput Testing, Aircraft Testing and Certification, p. 19 Conceptual Design of Unmanned Aircraft Systems, RTCA DO-160 Qualification: Purpose, Testing and p. 31 Design Considerations, p. 56

Armand Chaput is a senior lecturer in aerospace Ernie Condon has 28 years of engineering experience engineering and engineering mechanics at the with Hawker Beechcraft. He is a Certification Engineer University of Texas at Austin where he teaches (DER) in the HIRF/lightning field for Part 23 and unmanned air system engineering design and serves as Part 25 aircraft, with considerable experience in the director of the Air System Engineering Laboratory. He certification of carbon fiber aircraft. In addition, he is retired from Lockheed Martin Aeronautics Company has been a consultant DER in HIRF/lightning and where he was a senior technical fellow and member of conducting training in electromagnetic effects to the air system design and integration technical staff. departments with Hawker Beechcraft. Condon is a While at Lockheed Martin Aeronautics, he supported a research consultant at WSU/National Institute for range of advanced technology programs, most recently Aviation Research (NIAR) for the characterization of as weight czar and chief weight control engineer for electromagnetic effects to carbon fiber aircraft. Condon the F-35 Joint Strike Fighter Program. He has served as received a B.S. in electrical engineering from Wichita a member of the USAF Scientific Advisory Board, the State University. Naval Studies Board of the National Academy and the

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Guil Cornejo Bill Donovan Aircraft Engine Vibration Analysis, Turbine and Conceptual Design of Unmanned Aircraft Systems, Reciprocating Engines: FAA Item 28489, p. 17 p. 31

Guil Cornejo is president of RPM & Predictive Engr., Bill Donovan is president of Pulse Aerospace, LLC, in a rotating-machinery consulting, process-vibration Lawrence, Kansas. While doing graduate work at the remediation and training company. Cornejo has more University of Kansas, Donovan worked as a research than 30 years of experience in the mitigation of out-of- assistant in the KU Flight Test Laboratory and worked limit process-vibrations of gas-turbines, reciprocating as the chief designer of the Meridian unmanned aircraft engines, load-gearbox, centrifugal compressor/ system, a 1,100 lb., 26-foot wingspan UAS designed pumps, generators, electric-motors and both industrial to measure ice thickness and bed surface topology in training and industrial research. Career experience Antarctica and Greenland. Donovan has worked on the includes submarine noise mitigation at Mare Island, development of several new unmanned aircraft systems, CA and propulsion gear balancing/noise-analysis at including the Hawkeye UAS, the Wolverine helicopter Westinghouse in Sunnyvale, California, as well as UAS and the Aggressor II helicopter UAS. Donovan 20 years at Solar Turbines in San Diego, California. holds a B.S. and M.S. in aerospace engineering from Cornejo holds a B.S. in mechanical engineering from the University of Kansas and is currently completing the University of California, Davis, and both an M.S. in a doctorate of engineering program in aerospace mechanical design and a terminal Engineer Degree in engineering at KU. vibrations and acoustics from Stanford University. David R. Downing George Cusimano Digital Flight Control Systems: Analysis and Design, Flight Test Principles and Practices, p. 43 p. 32 Flight Testing Unmanned Aircraft—Unique David R. Downing is a professor emeritus of aerospace Challenges, p. 44 engineering at the University of Kansas. He taught courses and did research in advanced flight control, George Cusimano has more than 40 years of experience instrumentation systems and flight testing. Downing in research, development, and test of important was formerly an aerospace engineer at NASA Langley leading edge technologies. He has flight-tested complex Research Center, a systems engineer at the NASA systems, such as the F-117, B-2, X-33 (single stage to Electronics Research Center and an assistant professor orbit prototype), DarkStar UAV and X-35 (Joint Strike of systems engineering at Boston University. He received Fighter prototype). In addition to multiple postings as a B.S.E. in aerospace engineering and an M.S.E. in a flight test engineer, George was: the Director of Test instrumentation engineering from the University of and Evaluation for the F-117 System Program Office; the Michigan. He also earned an S.C.D. in instrumentation Chief of Flight Test Engineering for the B-2 Combined engineering from the Massachusetts Institute of Test Force; the Deputy Director of Joint STARS Technology. Combined Test Force; and the Director of Flight Test at the Lockheed Martin Skunk Works. George has also taught at the National Test Pilot School and has served Mark S. Ewing as a Technical Advisor to the United States Air Force. He Aircraft Structural Loads: Requirements, Analysis, retired from the United States Air Force as a colonel after Testing and Certification, p. 21 24 years of service. George holds a B.S. in mechanical Structural Composites, p. 59 engineering and an M.S. in industrial engineering from Arizona State University. He is a graduate of the USAF Mark S. Ewing is former chairman of the aerospace Test Pilot School and a Fellow of the Society of Flight engineering department and is currently the director Test Engineers. of the Flight Research Laboratory at the University of Kansas. Previously, he served as a senior research engineer in the structures division at Wright Laboratory,

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Wright-Patterson Air Force Base, and as an associate Bill Goodwine professor of engineering mechanics at the U.S. Air Force Applied Nonlinear Control and Analysis, p. 26 Academy. His research interests include structural vibrations and structural acoustics, especially as Bill Goodwine is an associate professor in the related to fiber-reinforced composites. Ewing is a department of aerospace and mechanical engineering at past recipient of the University of Kansas School of the University of Notre Dame. His research and teaching Engineering Outstanding Educator Award. He holds a focus on nonlinear control and dynamical systems, B.S. in engineering mechanics from the U.S. Air Force with particular emphasis on geometric methods and Academy, an M.S. in mechanical engineering and a hybrid systems. He received his M.S. and Ph.D. from the Ph.D. in engineering mechanics, both from Ohio State California Institute of Technology. He was the recipient University. of a National Science Foundation CAREER award and numerous departmental, college, university and ASEE Willie J. Fitzpatrick, Jr. teaching awards. Unmanned Aircraft System Software Airworthiness, p. 62 John Hall Durability and Damage Tolerance Concepts for Willie J. Fitzpatrick, Jr., has more than 37 years of Aging Aircraft Structures (Online Course), p. 33 experience in the software/systems engineering area. His experience includes the development and assessment John Hall began his career in England before joining The of automatic control systems, systems engineering and Boeing Company in 1966 as a fatigue analysis specialist software engineering on various aviation and missile on the 747. Later he joined a group of specialist engineers systems. He is currently serving as subject matter responsible for developing company-wide design, expert in software airworthiness and software safety analytical procedures and training programs for fatigue, in the Software Engineering Directorate (SED) of the damage tolerance and corrosion control. He was a member U.S. Army Research, Development, and Engineering of structures working groups responsible for developing Command’s Aviation and Missile Research Development new and aging airplane structural maintenance and and Engineering Center. Fitzpatrick served for over inspection programs. He was made a Technical Fellow of 12 years as the Chief, Aviation Division, SED and was The Boeing Company for his contributions. responsible for the management of life cycle software engineering support and software airworthiness Albert Helfrick assessments for several aviation systems, including Apache, Blackhawk, Chinook and Kiowa aircrafts and Fundamental Avionics, p. 45 unmanned aircraft systems. Albert Helfrick is the former chair of the electrical Fitzpatrick was honored by the Huntsville Association and systems engineering department at Embry-Riddle of Technical Societies (HATS) as the recipient of the Aeronautical University. Previously, he was director Sixth Annual Joseph C. Moquin Award in 2011. He of engineering for Tel-Instrument Electronics, a was recognized as the IEEE Huntsville Section 2011 manufacturer of avionics test equipment. Before entering Professional of the Year and 2002 Outstanding Engineer. academia, he was a self-employed consulting engineer He has served in various officer capacities for the IEEE for four years where he and his company designed fire Huntsville Section, including Section Chair for 2007 and and security systems, consumer items and avionics. 2008. Fitzpatrick holds a B.S. in electrical engineering He has 49 years of experience in various areas of from Tuskegee University, an M.S. in electrical engineering including communications, navigation, engineering from Stanford University and a Ph.D. in precision testing and measurement, radar and security industrial and systems engineering from the University systems. He performed radiation hardening on military of Alabama–Huntsville. avionics, designed test equipment for the emerging cable television industry, designed general aviation avionics for Cessna Aircraft and precision parameter measuring and magnetic systems for Dowty Industries. Helfrick is the author of 12 books, numerous contributions to

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 67 Instructor Bios encyclopedias, handbooks and other collections. He issues and evaluating and/or preparing certification has more than 100 technical papers and presentations, documentation for regulations compliance. She has served as an expert witness in a number of civil cases worked on numerous aviation projects including thrust and testified before Congress. He holds five U.S. patents, reverser systems, passenger-to-cargo conversions, is a registered professional engineer in New Jersey, a smoke detection/fire suppression systems, interiors, Life Senior Member of the IEEE, and an associate fellow rotorcraft medical LOX system, display/avionics systems, of the AIAA. Helfrick has received the AIAA Dr. John pressurization systems and engine control systems. Ruth Digital Avionics award. He holds a B.S. in physics Marge also has several years of safety engineering from Upsala College, M.S. in mathematics from New experience with defense systems and NASA payloads. Jersey Institute of Technology and a Ph.D. in applied She holds a B.S. in safety engineering from Texas A&M science from Clayton University. University and an M.S. in systems management from Florida Institute of Technology. Wally Johnson Aircraft Structural Loads: Requirements, Analysis, Jeff Knickerbocker Testing and Certification, p. 20 Complex Electronic Hardware Development and DO-254, p. 30 Principles of Aerospace Engineering, p. 51 Integrated Modular Avionics (IMA) and DO-297, Wally Johnson is a senior loads engineer and the p. 47 president of Loads and Dynamics Group Company. He is a structural loads consultant Designated Engineering Software Safety, Certification and DO-178C, p. 57 Representative (DER) for FAR 23 and FAR 25 categories. Jeff Knickerbocker is a consulting DER with nearly His responsibilities include design, fatigue, static, 30 years of experience as a systems/software engineer. dynamic, flight and ground loads analysis. Johnson has He has led technical teams in designing, developing 24 years of loads experience. Previously, he worked at and verifying real-time embedded software and AEH Boeing BDS in Wichita as a senior engineer. He also devices. In addition to industry affiliations, he also served as a technical specialist and an FAA DER at provides consulting and training services to the FAA Raytheon Aircraft Company. He has served as a member and other non-U.S. regulatory agencies. In 2002, he and of the Aviation Rulemaking Advisory Committee group his wife started Sunrise Certification & Consulting. working to harmonize the FARs and JARs in the area of Knickerbocker has a B.S. in physics and an M.S. in loads and dynamics. Johnson also has worked as a senior software engineering. loads engineer at Learjet. He holds a B.S. and M.S. in aerospace engineering from Wichita State University. Michael Mohaghegh Marge Jones Aircraft Structures Design and Analysis, p. 21 Commercial Aircraft Safety Assessment and 1309 Michael Mohaghegh is a Boeing Technical Fellow Design Analysis, p. 28 in Stress Analysis and Technology Support, with 45 years of experience in designing and analyzing Marge Jones is a system safety consultant specializing aircraft structures (707, 737, 747, B2, 767, 777, 787) and in commercial aircraft certification. She has been an developing technology needs, roadmaps and design FAA DER for safety analysis in structures, power plant, standards. He is the chief editor for the Boeing Design and systems and equipment for more than 24 years. She Principles manuals. Previously, he was principal lead is also a certified safety professional in system safety. engineer, manager and FAA DER for the Boeing Marge provides safety consultant/product safety services Company. Mohaghegh is the director of the Modern to the aircraft industry and has been involved in a Aircraft Structures Certificate Program at the University variety of STCs and TCs, many requiring specialized of Washington. He is the developer and instructor safety assessments. Her area of safety consultation for courses on stress analysis, finite element, fatigue, includes defining system architecture and detailed fracture, composites, airplane components and repairs design and safety requirements, performing safety at The Boeing Company. Mohaghegh has published analyses, developing design solutions to safety related aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 68 in the Journal of Applied Mechanics, Journal of for 18 years as a structural fatigue analyst at Bell Helicopter Aircraft, International Journal of Mechanical Sciences, and McDonnell Aircraft companies. He was involved in International Journal of Mechanical Engineering several design, in-service, and test projects on helicopters Education, and the Boeing AERO magazine. He and fighter aircraft. He was also on an on-site design team received his B.S. and M.S. in structural engineering in Spain. Nuss has a B.S. in aerospace engineering from the from the University of California, Berkeley, and his University of Kansas and did graduate study in engineering Ph.D. in engineering mechanics from the University of mechanics at the University of Texas–Arlington. Washington. Paul H. Park Steven L. Morris Essentials of Effective Technical Writing for Aircraft Icing: Meteorology, Protective Systems, Engineering Professionals (new), p. 35 Instrumentation and Certification, p. 18 Paul H. Park is a retired Lockheed Martin engineer Steven L. Morris is a Senior Managing Consultant with more than 35 years’ experience in advanced and Colorado Manager of Colorado Operations for aircraft design. During his career he led preliminary Engineering Systems Inc. (ESI), Colorado Springs, design teams in developing advanced fighters, bombers, Colorado. Morris served as an officer and engineer in the rotorcraft, and hypersonic vehicles. He led the U.S. Air Force for more than 24 years. His experience configuration design effort for the F-35 program, serving includes teaching, research and consulting in the areas as Air Vehicle Integration IPT lead and subsequently of airplane design, stability and control, aerodynamics, Deputy Chief Engineer. Park also led and authored major flight simulation, aircraft icing and accident sections of proposal technical volumes and reports for reconstruction. He is a co-author of Introduction to the F-35, Joint Multirole Rotorcraft, National Aerospace Aircraft Flight Mechanics: Performance, Static Stability, Plane, Next-Generation Long-Range Strike, and Air Dynamic Stability, and Classical Feedback Control. Force R&D programs. He is the author of this course, Morris is an Associate Fellow of AIAA and is a member which he has taught to engineers at Lockheed Martin, and Chair on the SAE Aircraft Icing Technology Bell Helicopter, and engineering students at major Committee. He received a B.S. in engineering universities. Park received his undergraduate degree in sciences from the U. S. Air Force Academy, an M.S. in mechanical engineering from University of Pennsylvania, aeronautical engineering from the Air Force Institute of and holds graduate degrees in aerospace engineering Technology and a Ph.D. in aerospace engineering from from Princeton University and Stanford University. He Texas A&M University. has authored six published papers on aircraft design and was a recipient of the 2002 AIAA Aircraft Design Award. Marv Nuss Sustainment and Continued Airworthiness for Paul Pendleton Aircraft Structures, p. 61 FAR 145 for Aerospace Repair and Maintenance Organizations, p. 40 Marv Nuss is the owner of Nuss Sustainment Solutions, an aircraft engineering consulting and training business. He Paul Pendleton recently retired from the Federal has consulted and/or trained on certification, continued Aviation Administration where he worked in the airworthiness, and aircraft research on four continents. Wichita Aircraft Certification Office (ACO) and Marv has over 40 years of experience in aircraft fatigue, Military Certification Office (MCO). While with the damage tolerance and continued airworthiness. He has ACO, Pendleton worked on Bilateral Aviation Safety worked FAA Part 23, 25 and 27 and Army, Navy and Air Agreements (BASA) with various nations, including Force projects. Nuss retired from the FAA in December as a team leader on the BASA with Russia. With the 2011 after serving more than 20 years in a variety of MCO, Pendleton worked as a program manager and engineering and management roles at the Small Airplane engineer on commercial derivative aircraft. Previously, Certification Directorate. He was involved in a broad he worked at Beech Aircraft and Learjet in Wichita, spectrum of continued airworthiness issues for all sizes and Kansas, acting as an FAA Designated Engineering classes of aircraft. Prior to joining the FAA, Nuss worked Representative (DER) to develop, certify and manage an

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FAA approved repair station, as well as a test pilot and Company. In his current position as chief technologist, engineer at the National Test Pilot School in Mojave, Structures and Methods, Philpot is responsible for California. Pendleton has a bachelor’s degree in aircraft the structural integrity of Alliant Techsystems (ATK) mechanical engineering from Parks College of Saint products and oversees the structural analyses performed Louis University. at ATK Defense Electronic Systems and subcontractors that support ATK programs. He also serves as the D. Mike Phillips test director for environmental testing (thermal and mechanical) that are conducted for the purpose of Aerospace Applications of Systems Engineering, hardware development, acceptance, and qualification. p. 16 Philpot currently leads the ATK Mechanical Analysis D. Mike Phillips is a principal research engineer at Council and has authored numerous internal processes, the Software Engineering Institute, a federally funded standards and design criteria for mechanical design and research and development center sponsored by the development contracts. U.S. Department of Defense and operated by Carnegie Mellon University. He led a team that created the CMMI Jim Reeves Product Suite, successfully describing key practices FAA Conformity, Production and Airworthiness for both systems and software engineering. He is the Certification Approval Requirements, p. 37 co-author of CMMI-ACQ: Guidelines for Improving the Acquisition of Products and Services, which is in its FAA Parts Manufacturer Approval (PMA) Process for second edition. As an Air Force senior officer, Phillips Aviation Suppliers, p. 39 led an Air Force program office’s development and Jim Reeves joined the FAA Atlanta Manufacturing acquisition of the software-intensive B-2 Spirit stealth Inspection District Office (MIDO) in 1978 as an aviation bomber using integrated product teams. He holds a safety inspector manufacturing. He then served as B.S. in astronautical engineering from the U.S. Air manager of the Atlanta Manufacturing Inspection Force Academy, an M.S. in nuclear engineering from District Office for 28 years. Major activities during Georgia Tech, an M.S. in systems management from his tenure with FAA included development of the the University of Southern California, an M.A. in FAA Designee Standardization Course, assigned ASI international affairs from Salve Regina College and an for Embraer San Jose Dos Campos, Brazil 1982–1987, M.A. in national security and strategic studies from the FAA bilateral team to China in 1995 and Malaysia in Naval War College. 1996, ACSEP Team, England 1988, participation in the development of the Certificate Management Information Dennis C. Philpot Systems (CMIS) and participation in the development Stress Analysis for Aerospace Structures (new), p. 58 of the Aircraft Certification System Evaluation Program (ACSEP). Reeves participated in or was directly involved Dennis C. Philpot began his career in the aerospace with 18 type certificate programs and production industry in 1983 at the Rocketdyne Division of Rockwell certificate issuances. International, where he was involved in several diverse programs, including the Space Shuttle Main Engines, Jan Roskam the National Aerospace Plane, and the International Space Station. In support of these and other programs, Airplane Performance: Theory, Applications and Philpot served as both a stress analyst and as a structural Certification (Online Course), p. 24 dynamics engineer. During the mid to late 1990s, Jan Roskam is the emeritus Ackers Distinguished Philpot performed structural analysis on two different Professor of Aerospace Engineering at the University fighter aircraft contracts. These included the F/A-18 of Kansas. His university honors include the 2003 E/F program for Northrop-Grumman and the Joint Chancellors Club Career Teaching Award and five- Strike Fighter (JSF) for the Lockheed-Martin Skunk time winner of Aerospace Engineering Educator of the Works. He also served as a principal structural analyst Year selected by graduating seniors. In October 2007, on two launch systems—the Kistler reusable launch Roskam received the prestigious AIAA Aircraft Design system and the Delta IV EELV, developed by the Boeing Award for Lifetime Achievement in airplane design,

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 70 airplane design education, configuration design and David L. Stanislaw flight dynamics education. The author of 15 textbooks, Reliability and 1309 Design Analysis for Aircraft Roskam has had industrial experience with three major Systems (Online Course), p. 54 aircraft companies and has been actively involved in the design and development of more than 50 aircraft David L. Stanislaw is an independent consultant in programs. He is a Fellow of AIAA and the Society of avionics with emphasis on civil aviation. He held Automotive Engineers. Roskam received an M.S. in engineering assignments in airborne systems design and aeronautical engineering from the Delft University of later assumed responsibility for avionics and electrical Technology, The Netherlands, and a Ph.D. in aeronautics engineering at the airframe level. Stanislaw was an FAA and astronautics from the University of Washington. DER for more than 15 years and has conducted seminars on all phases of aircraft electronics. The holder of several Wayne R. Sand radar patents, Stanislaw was a member of RTCA and has participated in international symposiums. He held Aviation Weather Hazards, p. 27 a commercial pilot rating. Stanislaw received a B.S. in Aircraft Icing: Meteorology, Protective Systems, electron physics from LaSalle College. Instrumentation and Certification, p. 18

Wayne R. Sand is an aviation weather consultant C. Bruce Stephens with expertise in aircraft icing tests, analysis of icing Aircraft Lightning: Requirements, Component accidents and development of icing instrumentation. Testing, Aircraft Testing and Certification, p. 19 He also has extensive expertise in convective weather, Electrical Wiring Interconnect System (EWIS) and winter weather and mountain weather. As former deputy FAA Requirements (new), p. 34 director of the Research Applications Program at the National Center for Atmospheric Research, he developed C. Bruce Stephens is an FAA DER consultant at Learjet aviation weather technology for the FAA. Previously, and a consultant DER at his company, Stephens Sand was a member of the atmospheric science Aviation, with a wealth of experience in high intensity department at the University of Wyoming. He also radiated fields (HIRF) and lightning. Stephens retired conducted research on thunderstorms and convective from Hawker Beechcraft after 28 years of service. He icing while at the South Dakota School of Mines and has HIRF/Lightning experience on both Part 23 and Technology. Sand is co-holder of a patent on a technique Part 25 including composite aircraft. Stephens is a Six- for the remote detection of aircraft icing conditions. He Sigma/Lean Master Black Belt consultant, developing holds a B.S. in mathematics and physical science from implementation and training materials, and teaches at Montana State University, an M.S. in meteorology from a number of universities, including Webster University the South Dakota School of Mines and Technology and and Southwestern College. He also owns the company a Ph.D. in atmospheric science from the University of Learning 4.U. Stephens has an executive M.B.A. and Wyoming. M.S. in management from Friends University and a B.S. in industrial technology from Wichita State University. Walt Silva Modelling and Analysis of Dynamical Systems: A Wayne Stout Practical Approach, p. 48 Flight Control and Hydraulic Systems, p. 42

Walt Silva is currently a senior research scientist at the Wayne Stout is an independent consultant with a NASA Langley Research Center. Silva’s interests include technical specialization in design, analysis, simulation computational methods, nonlinear dynamics and and certification of aircraft mechanical systems. system identification. He received a B.S. in aerospace He has more than 30 years of experience in aircraft engineering from Boston University, an M.S. in mechanical systems as an independent consultant aerospace engineering from the Polytechnic University and at Bombardier Aerospace–Learjet, The Boeing (formerly known as the Polytechnic Institute of NY) Company and Honeywell. Stout has held positions of and a Ph.D. in applied mathematics from the College of engineering specialist, systems integrator and chief William & Mary. engineer. His experience covers all design phases from aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 71 Instructor Bios concept to final product across commercial, military and R. Teetor Educational Award from SAE, the John E. space products. In addition, Stout has been an adjunct and Winifred E. Sharp Award from the KU School of professor at Wichita State University and is an FAA DER Engineering, Henry E. Gould Award from KU School in flight controls, hydraulics, ECS, pressurization and of Engineering and four-time winner of the Aerospace door mechanisms. Stout received a B.S. in mechanical Engineering Outstanding Educator Award from the engineering from the South Dakota School of Mines and seniors of the department of aerospace engineering. Dr. Technology, an M.S. in aeronautical engineering from Taghavi received an M.S. from Northrop University and Wichita State University and a Ph.D. in engineering a Ph.D. from the University of Kansas, both in aerospace from Wichita State University. engineering.

Thomas William Strganac Robert Ternes Advanced Flight Tests, p. 13 Subcontract Management in Aerospace Organizations, p. 60 Principles of Aeroelasticity, p. 50 Robert Ternes is a senior program manager at Atego Since 1989, Thomas Strganac has served as a professor Aerospace Services, and is a consultant specializing in of aerospace engineering at Texas A&M University. His subcontract management for aerospace organizations, research and engineering activities focus on aeroelastic aircraft certification and project management. Mr. phenomena, structural dynamics, fluid-structure Ternes currently manages the PMO for Atego, where interaction, limit cycle oscillations and related nonlinear he directs the efforts of a broad range of consulting mechanics. From 1975 to 1989, Thomas served as a activities. He has provided subcontractor selection, research engineer at NASA’s Langley Research Center direction and leadership for a wide range of companies and as an aerospace engineer at NASA’s Goddard including Boeing, Airbus, Lockheed, United Flight Space Center. Thomas is an Associate Fellow of Technologies, AAR Corporation, Crane Aerospace, the AIAA and a registered professional engineer. He BAE Systems, Raytheon Corporation, WindRiver, received his B.S. from North Carolina State University Ultra Electronics and Mectron. Prior to Atego, he and his M.S. from Texas A&M University, both in was a program manager at Honeywell International, aerospace engineering, and received his Doctorate in a program manager at Motorola, Inc., and a systems engineering mechanics from Virginia Tech. engineer at IBM. Mr. Ternes managed subcontractors in programs that included specialized semiconductors, Ray Taghavi cellular handsets, computer hardware and software, the Propulsion Systems for UAVs and General Aviation build and launch of the Iridium space satellite system, Aircraft, p. 53 custom air transport airframe modifications and several classified aerospace projects. His experiences also Ray Taghavi is a professor of aerospace engineering at include software CMM and CMMI implementation the University of Kansas where he teaches courses in and use in large programs, and system integration. Mr. jet propulsion, rocket propulsion, aircraft reciprocating Ternes has a B.S. in Engineering and Applied Sciences engines, fluid mechanics, aerodynamics, advanced from Yale University where he focused on business and experimental techniques and instrumentation. technology. He has a Program Management Professional Previously, he was a research engineer at NASA Lewis (PMP) certification. Research Center conducting experimental research on supersonic jet noise reduction techniques, acoustic excitation of free shear layers and stability and control of swirling flows. He is the co-inventor and patent holder for a supersonic vortex generator. He is a Fellow of the American Society of Mechanical Engineers and an Associate Fellow of the American Institute of Aeronautics & Astronautics. He was the recipient of the Abe M. Zarem Educator Award from AIAA, the Ralph

aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 72

Gilbert L. Thompson C.P. (Case) van Dam FAA Certification Procedures and Airworthiness Aerodynamic Design Improvements: High-Lift and Requirements as Applied to Military Procurement Cruise, p. 14 of Commercial Derivative Aircraft/Systems, p. 36 C.P. “Case” van Dam is the Warren and Leta Giedt FAA Functions and Requirements Leading to Endowed Professor and Chair of Mechanical and Airworthiness Approval, p. 38 Aerospace engineering at the University of California Gilbert L. Thompson is a private consultant in aircraft at Davis and heads the California Wind Energy certification. He has more than 33 years of experience in Collaborative; a partnership between the University domestic and international aircraft certification with the of California and the California Energy Commission. FAA. He also has served as a systems engineer; project Before joining UC Davis in 1985, he was a National manager; Manager, Systems and Equipment Branch; Research Council (NRC) post-doctoral researcher at Manager, Los Angeles Aircraft Certification Office; and the NASA Langley Research Center, and a research Assistant Manager, Transport Airplane Directorate. engineer at Vigyan Research Associates in Hampton, His certification experience includes the Robinson R22/ Virginia. Van Dam’s current research includes wind R44 rotorcraft, Lockheed L1011, McDonnell Douglas energy engineering, aerodynamic drag prediction and DC-8, DC-9, DC-10, MD-80, MD-90, KC-10A, MD-11, reduction, high-lift aerodynamics, and active control MDHI 369/500NOTAR, MDHI 600, MDHI 900, the first of aerodynamic loads. He has extensive experience concurrent and cooperative joint FAA/Joint Aviation in computational aerodynamics, wind-tunnel Authorities certification of the Boeing 717-200, and experimentation and flight testing; teaches industry development of the criteria for civil certification of the short courses on aircraft aerodynamic performance and military Globemaster C-17. In 1999, he was the recipient of wind energy; has consulted for aircraft, wind energy, the Aviation Week and Space Technology Laurels Award and sailing yacht manufacturers; and has served on for outstanding achievement in the field of aeronautics/ review committees for various government agencies and propulsion. He holds a B.S. in aerospace engineering from research organizations. He received B.S. and M.S. degrees the University of Michigan and a B.A. in mathematics from the Delft University of Technology, the Netherlands, from Bellarmine University, Louisville, Kentucky. and M.S. and Doctor of Engineering degrees from the University of Kansas, all in aerospace engineering. Herbert Tuttle Paul Vijgen Fundamentals of Project Management for Aerospace Professionals, p. 46 Aerodynamic Design Improvements: High-Lift and Cruise, p. 14 Herbert Tuttle is Professor, Director of Project & Engineering Management and Assistant Dean of Paul Vijgen is an Associate Technical Fellow in Engineering for the KU Edwards Campus. He has Washington supporting aerodynamic research, design instructed there for the past 20 years. In his previous and development—currently focusing on fuel-burn 20 years of professional practice, he was a management reduction technologies. Starting at NASA Langley in consultant, project manager, project engineer and 1985, he has been involved with application studies and manufacturing manager with various companies. Tuttle flight tests of laminar flow and other drag-reduction holds two undergraduate and three graduate degrees in methods to wings, fuselages and nacelles. Flight research areas of engineering and management. He has instructed activities include high-lift flows, wake-vortex development project management internationally and is Certified and supersonic turbulent flows. He supported appendage International Project Manager, CIPM©, a Fellow of the design and testing for U.S. syndicates in two previous American Academy of Project Management, a member America’s Cup campaigns. Vijgen received an M.S. from of the Project Management Institute, the American the Delft University of Technology, The Netherlands, and Society for the advancement of Project Management and a doctorate degree from the University of Kansas—both International Project Management Association. He has in Aerospace Engineering. published many articles, contributed to number of books and speaks publicly on Achieving Results in Project Management. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 73 Instructor Bios

Marco Villa Max Vozoff Commercial Space—What It Means and the Issues Commercial Space—What It Means and the Issues It Raises (new), p. 29 It Raises (new), p. 29

Dr. Marco Villa is a partner in mv2space, LLC, a Max Vozoff is currently an aerospace business Business Development and Strategy consultancy development consultant dedicated to seeing innovative dedicated to seeing innovative small companies grow and small companies in the space sector grow and flourish, to flourish. Marco worked as system engineer and project help build a stable and robust commercial space sector. manager for Swales Aerospace and as a contractor for Previously he was SpaceX’s Director of Civil Business NASA Wallops and the US Air Force. This time provided Development, Senior Design Engineer at NASA’s Jet Marco with a broad understanding of spacecraft systems Propulsion Laboratory (JPL), and a communications as he performed leading roles for many innovative engineer for commercial companies. At SpaceX, Max small satellite and launch vehicle systems, including was responsible for writing and winning proposals that the Air Force sponsored TacSat 3 spacecraft and the resulted in over $1.9 billion of business from NASA. Autonomous Flight Safety System. In 2007, Marco joined Max then managed these highly successful programs Space Exploration Technologies (SpaceX), as the Director for nearly 4 years, including being responsible for of Mission Operations. Some of his responsibilities were development of the Dragon spacecraft. Max’s business over the selection and training of operators, ground development responsibilities brought him into regular segment architecture, mission planning, and the final contact with the highest levels of many commercial integration, on-orbit operations and recovery of the spacecraft manufacturers and users internationally, as Dragon spacecraft. Marco was integral in the effort to well as civil and defense management personnel within secure and successfully execute $2.5B in contracts for the US Government. This yielded a wealth of knowledge, ISS cargo resupply and crewed Dragon development insight and ongoing relationships that Max is now programs, while also supporting the sales and business leveraging to help multiple clients in the space industry development department. A certified Mission Director define and implement business strategy, win awards for Dragon missions to the International Space Station, and raise funding. Max has been at the forefront of the Marco has been part of multiple successful missions, emerging “commercial space” or “NewSpace” industry including lead roles over ISS approach and departure. since before its recent rise to prominence and has spoken Marco has a Bachelor’s Degree in Aerospace Engineering and written about a wide variety of relevant topics in 1999 from Politecnico di Milano, a Master’s Degree including the challenges it faces. He holds a Bachelor’s in Aerospace Engineering (Composite Materials) from degree in Electrical Engineering (Communications) the University of Kansas in 2002. He also earned his from Curtin University in Western Australia and a Master’s Degree in Engineering Management (Program Masters Degree in Aerospace Engineering (Astronautics) Management) followed by his PhD in Aerospace from the University of Southern California (USC). Engineering (Space Management) in 2005. Michael Wallace Roelof Vos Process-Based Management in Aerospace: Aerodynamic Design of Transport Aircraft (new), Defining, Improving and Sustaining Processes, p. 52 p. 15 Michael Wallace is an aerospace process management Roelof Vos is an assistant professor at the Aerospace consultant with specializations in knowledge-based Engineering Department of Delft University of engineering and lean manufacturing and information Technology. He teaches undergraduate courses in technology. During his 26 years with The Boeing conceptual airplane design and two graduate courses Company, Wallace led the design and implementation on aerodynamic design of transport aircraft and of quality improvement techniques including process- fighter aircraft. He obtained an MSc degree from Delft based management, knowledge-based engineering and University of Technology and a Ph.D. degree from quality management in several in-house processes. As The University of Kansas. His research focuses on the a project manager with The Boeing Company, he was development and implementation of design tools for instrumental in introducing process management in conventional and unconventional airplane configurations. aeroshortcourses.ku.edu/air Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 74 factory and office environs and defining and leading Mark K. Wilson process improvement projects that encompassed Aerospace Applications of Systems Engineering, enhancements in lean manufacturing and information p. 16 technology. Since retiring from The Boeing Company, Wallace is a frequent presenter on process-based Mark K. Wilson, president of Mark Wilson Consulting, management, along with other related topics such as is a systems engineering and aerospace consultant with project management, lean manufacturing and system more than 45 years of systems engineering acquisition analysis. He was a Baldrige Examiner with the Kansas experience. He is a founding director and chief operating Award for Excellence and a board member of the Kansas officer of Aerospace Technologies Associates, LLC, and Center for Performance Excellence. Wallace has an an associate with Dayton Aerospace, Inc. Wilson, a M.B.A. from Wichita State University with extensive member of the Senior Executive Service, completed his study in business and constitutional law and a B.S. in Air Force career as Director of the Air Force Center for mathematics from the University of Kansas. Systems Engineering, Air Force Institute of Technology (AFIT), Wright Patterson Air Force Base, Ohio. He Donald T. Ward served as the Technical Advisor for systems engineering at the Aeronautical Systems Center and as Technical Aerospace Applications of Systems Engineering, Director in the Headquarters of Air Force Material p. 16 Command (AFMC), Directorate of Engineering and Advanced Flight Tests, p. 13 Technical Management. He was Director of Engineering in the C-17 System Program Office at the Aeronautical Flight Control Actuator Analysis and Design, p. 41 Systems Center, where he directed all aspects of systems Flight Test Principles and Practices, p. 43 engineering necessary to develop, produce and sustain the C-17 Weapon System. He also worked on numerous Donald T. Ward is a professor emeritus of aerospace weapon systems including the B-2 bomber and the F-15 engineering at Texas A&M University and a former fighter. Wilson earned his B.S. in aerospace engineering director of its Flight Mechanics Laboratory. Previously, from Purdue University. He is a Sloan Fellow and holds he served 23 years as an officer in the United States an M.S. in management from Stanford University and Air Force, retiring as a colonel. His last military an M.S. in management science from the University of assignment was as Wing Commander of the 4950th Dayton. Test Wing at Wright-Patterson Air Force Base. Earlier tours included Commandant of the USAF Test Pilot School and Director of the F-15 Joint Test Force at Edwards Air Force Base. A Fellow of the AIAA, Ward is the senior co-author of two textbooks, Introduction to Flight Test Engineering, Volumes I and II. He is a member of the Society of Flight Test Engineers and the Society of Experimental Test Pilots. Ward holds a B.S. in aeronautical engineering from the University of Texas, an M.S. in astronautics from the Air Force Institute of Technology and a Ph.D. in aerospace engineering from Mississippi State University. Dr. Ward is currently the manager of a Model Based Systems Engineering project designed to radically improve the integration process for complex, software-intensive systems through the use of virtual integration. He has taught short courses for the Kansas University Continuing Education Division for over 30 years.

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