1 2010 Course University of Kansas Catalog

Singapore Seattle Fort Worth San Diego Kansas City O rlando March April June September October November

www.ContinuingEd.ku.edu/aero Toll-free in the U.S.: 877-404-5823 or 785-864-5823 www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 2 Letter from the Director

Dear Aerospace Colleague,

I am pleased to present you with the 2010 brochure of the University of Kansas Aerospace Short Course Program, which has a 33-year history of successful aerospace and avionics training for industries and governments worldwide.

In 1977, the Department of Aerospace Engineering at the University of Kansas (KU) teamed with KU Continuing Education to offer professional development opportunities to the aerospace industry. Backed by the department’s world-class faculty, KU Continuing Education developed short courses that allowed industry professionals to learn the latest technological advances and research developments. During the last 33 years, more than 26,000 aerospace industry professionals from across the United States and 57 countries have benefited from these state-of-the-art courses.

First offered only on the KU campus, the short courses have since been conducted throughout the United States and in many other countries. Today, the University of Kansas offers 42 aerospace short courses, from Airplane Preliminary Design to Fundamental Avionics. Enclosed in this brochure are the descriptions of the courses offered by our program at publicly announced venues and also information specifically for those who are interested in holding courses at their own location. All of our courses, including the ones offered at public venues, can be offered as in-house classes.

Our 2009 Singapore public classes were well-received by the local, regional and European aerospace industries, and we will continue conducting our public classes in Singapore in 2010 by presenting three of our popular courses that are suitable for prospective Singapore attendees. See page 5 for a list of those courses.

In 2010, we are introducing three new aerospace short courses: Applied Nonlinear Control and Analysis, a five-day class taught by Bill Goodwine Integrated Modular Avionics and DO-297, a two-day class taught by Leanna Rierson Airborne Equipment Design and RTCA DO-160, a four-day class taught by Ken Vranish

We have recently introduced a multimedia-based aerospace short course, titled Airplane Performance: Theory, Applications and Certification, taught by Dr. Jan Roskam, mediated by Mario Asselin and delivered online. It has already gained tremendous attention and continues to receive enrollments.

In 2010, we also are introducing a Certificate Program for participants who have attended multiple aerospace short courses from the University of Kansas. Please don’t forget to check the following page if you have attended or will attend more than one aerospace short course in the certificate track and wish to receive a combined certificate.

Last but not the least, in 2010 we are bringing back our live video-based short courses with newly acquired video-conferencing equipment. This is an affordable alternative to attending public courses or in-house classes. The details are on the following page.

While we enjoyed an extremely productive 2009, we are saddened to inform you that we lost one of our long-time instructors, Bill Schweikhard, who passed away on July 12, 2009. He joined our program in 1978, while he was a professor at KU, and taught for the last time in April 2009 at our Seattle public courses. Like many of you, we miss him. We promise to continue his teaching legacy though our service in future years.

We wish to thank all of the companies who have supported us through the years by sending your employees to our courses. Without your patronage, we could not have been successful. Our participants are past, present and future, and we hope that we continue to provide you with the world-class aerospace training that you expect and deserve. We look forward to seeing you in 2010!

In 2010, we will be able to offer discounts to multiple participants from the same company for the same course, all enrolling at the same time. See page 7 for more information.

Sincerely,

Soma Chakrabarti, Ph.D. Director, Aerospace Short Course Program www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 3 Introducing the KU Aerospace Short Course Program Certificate Track and Live Video Presentations If you have attended or will attend more than one face-to-face Certificate Tracks (in person) aerospace short course, you may be interested in Aerospace Compliance obtaining a certificate for participating in any four courses listed in the following tracks. For more information, please • FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/ visit www.ContinuingEd.ku.edu/aero/certificates. Systems • FAA Functions and Requirements Leading to Airworthiness Approval T o Receive a Combined/Group Certificate • FAA Conformity, Production and Airworthiness Certification If you have taken courses in the past, and you’re interested in a Approval Requirements certificate, you will need to provide the following information • Commercial Aircraft Safety Assessment and 1309 Design Analysis • Aircraft Icing: Meteorology, Protective Systems, Instrumentation and to ask for issuing certificates: Certification • Your full name Aircraft Design • The calendar year(s) when you attended the classes • Airplane Preliminary Design • The course titles and the instructors • Aerodynamic Design Improvements: High-Lift and Cruise • Airplane Flight Dynamics: Open and Closed Loop • The public course venue or company facility where each • Conceptual Design of Unmanned Aircraft Systems class was held • Helicopter Performance, Stability and Control • The project numbers of the courses provided on your individual course certificates Aircraft Maintenance and Safety • Developing a Premier Aircraft Preventive Maintenance Program • Your current address and phone number Based on the Principles of Reliability-Centered Maintenance (RCM) • A nominal fee for shipping and handling • Commercial Aircraft Safety Assessment and 1309 Design Analysis • Durability and Damage Tolerance Concepts for Aging Aircraft • Aircraft Icing: Meteorology, Protective Systems, Instrumentation and Certification Live Video Presentations of University of • Aviation Weather Hazards • Understanding and Controlling Corrosion of Aircraft Structures Kansas Aerospace Classes KU’s video classroom can reach your employees around Aircraft Structures the world. The state-of-the-art video classroom at KU • Aircraft Structural Loads: Requirements, Analysis, Testing and Continuing Education allows you to reach as many as Certification eight international locations simultaneously in real-time. • Aircraft Structures Design and Analysis Using the latest advances from Polycom Pro-Motion video • Structural Composites technology and Creston audio/video, you can train all • Understanding and Controlling Corrosion of Aircraft Structures your employees while saving thousands of dollars in travel Avionics and Avionic Components expenses. Located in the Central Time Zone, the video classroom allows you to conveniently reach every corner • Fundamental Avionics • Integrated Modular Avionics and DO-297 of the North American continent during regular business • Complex Electronic Hardware Development and DO-254 hours, and other countries based on their time zones. • Airborne Equipment Design and RTCA DO-160 • Software Safety, Certification and DO-178B This video classroom offers a great learning environment and an affordable alternative to face-to-face classes. The Flight Control Systems Design courses can be presented in their standard version or • Applied Nonlinear Control and Analysis they can be customized like on-site courses. While the • Flight Control and Hydraulic Systems technology is the room’s hallmark, the space is also true • Digital Flight Control Systems: Analysis and Design to its roots as a place of learning. The room is quiet and • Flight Control Actuator Analysis and Design well lit, so even if you do not use all its technological Flight Tests and Aircraft Performance marvels, it provides a wonderful atmosphere for learning or conducting business. • Flight Test Principles and Practices • Advanced Flight Tests • Operational Aircraft Performance and Flight Test Practices To organize a live video class, please contact Kim • Airplane Flight Dynamics: Open and Closed Loop Hunsinger, Assistant Director of Program Management • Acquisition of Digital Flight Test Data from Avionics Busses: and Marketing at 785‑864-4758 or [email protected]. Techniques for Practical Flight Test Applications • Principles of Aeroelasticity • Rotorcraft Structural Dynamics and Aeroelasticity

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 4 2010 KU Aerospace Short Courses List

Advanced Flight Tests ...... 10 Aerodynamic Design Improvements: High-Lift and Cruise ...... 11 Aerospace Applications of Systems Engineering ...... 12 Airborne Equipment Design and RTCA DO-160 (new) ...... 13 Aircraft Icing: Meteorology, Protective Systems, Instrumentation, and Certification ...... 14 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification ...... 15 Aircraft Structures Design and Analysis ...... 16 Airplane Flight Dynamics: Open and Closed Loop ...... 17 Airplane Performance: Theory, Applications and Certification (Computer-based course) ...... 18 Airplane Preliminary Design ...... 19 Applied Nonlinear Control and Analysis (new) ...... 20 Aviation Weather Hazards ...... 21 Commercial Aircraft Safety Assessment and 1309 Design Analysis ...... 22 Complex Electronic Hardware Development and DO-254 ...... 23 Conceptual Design of Unmanned Aircraft Systems ...... 24 Developing a Premier Aircraft Preventive Maintenance Program Based on the Principles of Reliability-Centered Maintenance (RCM) . 25 Digital Flight Control Systems: Analysis and Design ...... 26 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems ...... 27 FAA Conformity, Production and Airworthiness Certification Approval Requirements ...... 28 FAA Functions and Requirements Leading to Airworthiness Approval ...... 29 Flight Control and Hydraulic Systems ...... 30 Flight Test Principles and Practices ...... 31 Fundamental Avionics ...... 32 Helicopter Performance, Stability and Control ...... 33 Integrated Modular Avionics (IMA) and DO-297 (new) ...... 34 Operational Aircraft Performance and Flight Test Practices ...... 35 Principles of Aeroelasticity ...... 36 Principles of Aerospace Engineering ...... 37 Project Management for Aerospace Professionals ...... 38 Reliability and 1309 Design Analysis for Aircraft Systems (Computer-based course) ...... 39 Software Safety, Certification and DO-178B ...... 40 Structural Composites ...... 41

Letter from the Director ...... 2 Individual Course Listings ...... 10 Certificate Track and Video Presentation ...... 3 Instructor Biographies ...... 42 On-site Aerospace Short Courses ...... 6 Registration Form ...... Back Cover General Information ...... 7 Lodging and Travel Information ...... 8

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 5 2010 KU Aerospace Short Course Schedule

S ingapore Crowne Plaza Changi Airport Course # Fee March 1–5 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification • Wally Johnson AA101300 $2,595 March 1–5 Commercial Aircraft Safety Assessment and 1309 Design Analysis • Marge Jones AA101310 $2,595 March 1–5 Fundamental Avionics • Albert Helfrick AA101320 $2,595

S eattle Doubletree Guest Suites Southcenter April 26–30 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification • Wally Johnson AA101330 $2,295 April 26–30 Airplane Preliminary Design • Jan Roskam AA101340 $2,295 April 26–30 Flight Test Principles and Practices • Donald T. Ward AA101350 $2,295 April 26–30 Fundamental Avionics • Albert Helfrick AA101360 $2,295 April 26–30 Principles of Aeroelasticity • Thomas William Strganac AA101370 $2,295 April 27–29 FAA Functions and Requirements Leading to Airworthiness Approval • Gilbert L. Thompson, Everett W. Pittman AA101380 $1,695 April 27–30 Aviation Weather Hazards • Wayne R. Sand AA101390 $1,995

F ort Worth American Airlines Training and Conference Center: A Dolce Conference Hotel June 14–17 Commercial Aircraft Safety Assessment and 1309 Design Analysis • Marge Jones AA101400 $1,995 June 14–18 Aircraft Structures Design and Analysis • Michael Mohaghegh, Mark S. Ewing AA101410 $2,295 June 14–18 Helicopter Performance, Stability and Control • Ray Prouty AA101420 $2,295

S an Diego Marriott Mission Valley Sept. 13–17 Aerodynamic Design Improvements: High-Lift and Cruise • Paul Vijgen, Case van Dam AA111000 $2,295 Sept. 13–17 Airplane Flight Dynamics: Open and Closed Loop • Jan Roskam AA111010 $2,295 Sept. 13–17 Digital Flight Control Systems: Analysis and Design • Dave Downing AA111020 $2,295 Sept. 13–17 Fundamental Avionics • Albert Helfrick AA111030 $2,295 Sept. 13–17 Helicopter Performance, Stability and Control • Ray Prouty AA111040 $2,295 Sept. 13–17 Project Management for Aerospace Professionals • Herb Tuttle AA111050 $2,295 Sept. 13–17 Structural Composites • Max Kismarton AA111060 $2,295 Sept. 15–17 FAA Functions and Requirements Leading to Airworthiness Approval • Gilbert L. Thompson, Everett W. Pittman AA111070 $1,695

S an Diego Marriott Mission Valley Sept. 20–21 Integrated Modular Avionics (IMA) and DO-297 (NEW) • Leanna Rierson AA111080 $1,295 Sept. 20–22 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems • Gilbert L. Thompson, Everett W. Pittman AA111090 $1,695 Sept. 20–24 Applied Nonlinear Control and Analysis (NEW) • Bill Goodwine AA111100 $2,295 Sept. 20–24 Flight Test Principles and Practices • Donald T. Ward AA111110 $2,295 Sept. 20–24 Principles of Aerospace Engineering • Wally Johnson AA111120 $2,295 Sept. 21–23 Developing a Premier Aircraft Preventive Maintenance Program Based on the Principles of Reliability-Centered Maintenance (RCM) • Neil Bloom AA111130 $1,695 Sept. 21–24 Aircraft Icing: Meteorology, Protective Systems, Instrumentation and Certification • Wayne R. Sand, Steve Morris AA111140 $1,995 Sept. 22–24 Complex Electronic Hardware Development and DO-254 • Leanna Rierson AA111150 $1,695 Sept. 20–24 Combine AA111080 and AA111150 (SAVE $) • Leanna Rierson AA111160 $2,295

Kansas City Crowne Plaza Downtown Oct. 18–21 Airborne Equipment Design and RTCA DO-160 (NEW) • Ken Vranish AA111170 $1,995 Oct. 18–21 Commercial Aircraft Safety Assessment and 1309 Design Analysis • Marge Jones AA111180 $1,995 Oct. 18–22 Aerospace Applications of Systems Engineering • Donald T. Ward, Mike Phillips, Mark Wilson AA111190 $2,295 Oct. 18–22 Fundamental Avionics • Albert Helfrick AA111200 $2,295

O rlando Doubletree Resort Orlando–International Drive Nov. 15–19 Advanced Flight Tests • Donald T. Ward, Thomas William Strganac AA111210 $2,295 Nov. 15–19 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification • Wally Johnson AA111220 $2,295 Nov. 15–19 Conceptual Design of Unmanned Aircraft Systems • Armand Chaput AA111230 $2,295 Nov. 15–19 Flight Control and Hydraulic Systems • Wayne Stout AA111240 $2,295 Nov. 15–19 Fundamental Avionics • Albert Helfrick AA111250 $2,295 Nov. 15–19 Operational Aircraft Performance and Flight Test Practices • Mario Asselin AA111260 $2,295 Nov. 16–18 FAA Conformity, Production and Airworthiness Certification Approval Requirements • Donald Plouffe AA111270 $1,695 Nov. 16–19 Software Safety, Certification and DO-178B • Leanna Rierson AA111280 $1,995 www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 6 On-site Aerospace Short Courses Realize substantial savings by bringing our outstanding instructors to your workplace!

All University of Kansas Aerospace Short F requently Asked Questions I ndustry Leaders Who Have Courses are also available for on-site Where can you provide in-house Supported the KU Aerospace presentations. In addition to the courses training? Short Course Program listed in this brochure, we offer courses Anywhere in the world, except in the Airbus designed specifically for on-site delivery. travel warning countries listed by the Read descriptions of all courses available U.S. Department of State. BAE Systems for on-site delivery at our Web site at Bell Helicopter Textron www.ContinuingEd.ku.edu/aero. What does the company provide? You provide the attendees, a classroom The Boeing Company and audio-visual equipment such as Bombardier-Learjet, Inc. a projector and a screen. We will send Contact Us Cessna Aircraft Company you a description of the course needs O btain a no-cost, no‑obligation in advance to prepare for the class. If DCA-BR (Organização Brasileira para proposal for an on-site class that you cannot provide a classroom, we o Desenvolvimento da Certificação your employees will benefit from. can set up a course at a nearby hotel Aeronáutica) or conference center for an additional Embraer-Empresa Brasileira de Zach Gredlics charge. Aeronáutica S.A. On-site Program Manager What does KU provide? European Aviation Safety Agency E-mail [email protected] KU provides the instructors’ honoraria, his Federal Aviation Administration Phone 785-864-1066 or her travel, all course materials, shipping Garmin Fax 785-864-5074 and customs charges, certificates with CEUs for participants who attend all days, GE Aviation course evaluation and coordination. Gulfstream Aerospace Corporation Benefits of KU On-Site Can the course content be modified? Hawker Beechcraft Corporation Training Absolutely. Instructors can tailor Honeywell, Inc. When you choose the KU Aerospace instruction to emphasize areas that best Lockheed Martin Corporation Short Course Program for your on-site accommodate your group. training, you: NASA • Work directly with the instructors to How is an on-site course price National Aerospace Laboratory of The customize training that meets your determined? Netherlands To make it cost-effective for all specific needs Northrop Grumman Corporation parties, we base our course fees on • Discuss issues that affect your 20 participants and offer substantial Pilatus Aircraft Ltd. company without jeopardizing discounts for each additional participant. QinetiQ Ltd. proprietary information We also have worked with organizations • Pay only for the training you need to form consortiums with other area Rockwell Collins companies to share costs. • Train when it fits your schedule SAAB Aircraft AB The course fee of an on-site class • Incur lower costs per participant Samsung depends on the instructors’ honoraria, Sierra Nevada Corporation • Save employee travel expenses the instructors’ travel reimbursements, • Reduce the time employees are away the cost of the course materials specific Sikorsky Aircraft Corporation from work for that class and the shipping costs of Spirit AeroSystems the course materials. • Train as a team to enhance project SR Technics management. How far in advance do you need to Transport Canada schedule a course? United States Department of Defense In order to schedule the instructor(s) and (Air Force, Army, Navy, Marines and order the course materials, we request at Coast Guard) least 8 to 12 weeks of lead time prior to the actual course date.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 7

General Information www.ContinuingEd.ku.edu/aero E-mail: [email protected] • Phone: 785-864-5823, or toll-free within the U.S. 877-404-5823 • Fax: 785-864-4871 Mail: KU Continuing Education • Aerospace Short Course Program • 1515 Saint Andrews Drive • Lawrence, Kansas 66047-1619 • USA

E nroll Anytime Late Payment Fee Complete the registration form on the back cover to enroll by All course fees are due at the time the class is held. KU allows a mail or fax. To enroll online, visit www.ContinuingEd.ku.edu/aero. 30-day grace period. Any fees that remain unpaid after 30 days following the class will be assessed a late fee of $100. Enrollment is limited and will be accepted in order of receipt by Continuing Education. We recommend that you register as R efund/Cancellation Policy soon as possible so that you can secure your place and we can We encourage you to send a qualified substitute if you cannot prepare the proper amount of course material. Pre-registration attend. A full refund of registration fees will be available if is required for your protection in case of course cancellation. requested in writing and received two weeks before a course. After that date, refunds will be made, but an administrative fee A confirmation letter will be mailed, faxed or e-mailed to each may be assessed. No refunds will be made after 30 calendar enrollee prior to the short course. Travel information will be days following the event. included and will also be available on the Web site. If you do not receive a confirmation packet, please contact us at one of The University of Kansas Continuing Education reserves the the above numbers. right to cancel any short course and return all fees in the event of insufficient registration, instructor illness or national Lodging and travel information for each class site can be found emergency. The liability of the University of Kansas is limited on pages 8 and 9. to the registration fee. The University of Kansas will not be responsible for any losses incurred by the registrants including, Discounts but not limited to, airline cancellation charges or hotel deposits. Group discounts are available for companies registering more than two people for the same class at the same time. All Class participants eligible for the discount will be billed together on Location: The course location will be included in your the same invoice. The discount rates are as follows: confirmation letter. Smoking is limited to outside the building. No audio or video recording is permitted. 3–4 People 05% discount 5–9 People 10% discount Accessibility: We accommodate persons with disabilities. 10–14 People 15% discount Please call our office or mark the space indicated on the 15+ People 20% discount registration form, and an aerospace short course staff member will contact you to discuss your needs. To assure Also ask about our on-site program. For more information, see accommodation, please register at least two weeks before page 6. the start of the event, earlier if possible. F ees/Billing Course Schedule: The University of Kansas Continuing Education and/or its instructors reserve the right to adjust All fees are payable in U.S. dollars and are due at the time the course outlines, schedules, and/or materials. Class times and class is held. Fees are listed on each course page. total hours are approximate and may be adjusted by the We accept all MasterCard, VISA, Discover and American Express. instructor(s) as the situation warrants. You may mail a company check in U.S. dollars to the University Instructors: The University of Kansas Continuing Education of Kansas Continuing Education, 1515 Saint Andrews Drive, reserves the right to substitute an equally qualified instructor Lawrence, KS 66047-1619, U.S.A. Please make checks payable in the event of faculty illness or other circumstances beyond to The University of Kansas, and please include your invoice its control. If an equally qualified instructor is not available, number on your check. the class will be cancelled. You may wire payment in U.S. dollars to US Bank of Lawrence, Certificate of Attendance: A Certificate of Attendance will be 900 Massachusetts, Lawrence, Kansas 66044, U.S.A. In the wire awarded to each participant who is present for 100 percent of you must refer to KU Aerospace Continuing Education and the class. include your invoice number. Please be sure to include any bank transfer fees. For account and ACH or routing number, Continuing Education Units (CEUs) are available but may not please call 785-864-5823. be used for college credit.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 8 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. • Visit www.ContinuingEd.ku.edu/aero/locations.php for helpful Internet links.

S ingapore S eattle, Washington F ort Worth, Texas March 1–5, 2010 April 26–30, 2010 June 14–18, 2010 Crowne Plaza Hotel–Changi Airport Doubletree Guest Suites Southcenter, American Airlines Training and 75 Airport Boulevard #01-01 16500 Southcenter Parkway Conference Center: A Dolce Singapore 819664 Seattle, Washington 98188 Conference Hotel 4501 Highway 360 South The hotel is located within the immediate A limited number of rooms have been vicinity of Singapore Changi Airport and is reserved at the Doubletree Guest Suites Fort Worth, Texas 76155 linked to Terminal 3 via covered walkways. Southcenter for course attendees. The A limited number of rooms have been Guests can also reach the hotel from rate is $129 for a standard single/double reserved at the American Airlines Training Terminals 1 and 2 via Changi Airport’s room plus local occupancy taxes. These & Conference Center for course attendees. automated People Mover System. If you are rooms will be held as a block, unless The rate is $129 for a standard room plus coming from within Singapore the hotel is depleted, until April 7, 2010, at which applicable state and local occupancy easily accessible by car, MRT train or bus. time they will be released to the public. taxes. These rooms will be held as a After April 7, room rate and availability A limited number of rooms have been block, unless depleted, until May 13, cannot be guaranteed. To make your reserved at the Crowne Plaza Hotel 2010, at which time they will be released reservation call 206-575-8220 or (toll-free Changi Airport for course attendees. The to the public. After May 13, room rate worldwide) 800-222-8733. State that you daily rate is S$240 (Singapore dollars) and availability cannot be guaranteed. will be attending a University of Kansas plus taxes, for a King Deluxe room with To make your reservation call 817-956- aerospace short course and give the breakfast and Internet. These rooms will 6030 or (toll-free Worldwide) 800-777- group code UOK. All reservations must be held as a block, unless depleted, until 6464. State that you will be attending be guaranteed with a major credit card. January 26, 2010, at which time they will a University of Kansas aerospace short be released to the public. After January Self-parking at the hotel is free for course. The group code is 10000115483. 26, room rate and availability cannot be attendees. All reservations must be guaranteed with guaranteed. The Seattle-Tacoma International Airport a major credit card. To make your reservations by phone, (SEA) is 3.5 miles (5.6 km) from the hotel. Self-parking at the hotel is free for please call 800-381-9553 (toll-free The hotel provides free shuttle service attendees. worldwide) and ask for the special rate for 6 a.m. to 11 p.m.; no reservation is the Aerospace Short Course Program at the required. The hotel shuttle courtesy The Dallas Fort Worth Airport (DFW) is 3.5 Crowne Plaza Hotel–Changi Airport. Our phone is located on the baggage claim miles (5.6 km) from the hotel. The hotel group code is UE2. To make a reservation level. Make sure to take the shuttle for the provides a complimentary shuttle to and directly with the hotel, call +65-68235300. Doubletree Guest Suites Southcenter. from DFW from 6:30 a.m. to 10:30 p.m. No All reservations must be accompanied by reservations are required. To request a The Doubletree Guest Suites Southcenter a first night room deposit or guaranteed shuttle, call 817-956-1000. also offers complimentary shuttle to the with a major credit card. NEW light rail train station. Getting to Dallas Love Field Airport (DAL) is 17 miles Participants are responsible for their own downtown Seattle is easy using this new (27.4 km) from the hotel. SuperShuttle parking fees. Self-parking is available at transit system. provides transportation for $33 each the hotel for S$18 a day. way. (Fees are subject to change.) Arrangements can be made online at Please be sure to review any travel and entry www.supershuttle.com or by calling requirements that may exist between your 817-329-2000 or (toll-free in the United country of residence and Singapore. Visit States) 800-258-3826. Be sure to use our the Singapore Immigrations & Checkpoint group code UPBP7. Authority Web site (http://www.ica.gov.sg/ page.aspx?pageid=95&secid=94) for any restrictions/requirements that may apply to your country.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 9

S an Diego, California Kansas City, Missouri O rlando, Florida September 13–17 and October 18–22, 2010 November 15–19, 2010 September 20–24, 2010 Crowne Plaza Kansas City Downtown Doubletree Resort Orlando– San Diego Marriott Mission Valley 1301 Wyandotte International Drive 8757 Rio San Diego Drive Kansas City, Missouri 64105 10100 International Drive Orlando, Florida 32821 San Diego, California 92108 A limited number of rooms have been A limited number of rooms have been reserved at the Crowne Plaza Kansas City A limited number of rooms have been reserved at the San Diego Marriott Mission Downtown for course attendees. The rate reserved at the Doubletree Resort Valley for course attendees. The rate is the is $107 for a standard single/double room Orlando–International Drive (formerly U.S. federal government per diem. At this plus applicable state and local occupancy known as the International Plaza Resort) time, the rate is $137 for a single/double taxes. These rooms will be held as a block, for course attendees. The rate is $119 room plus applicable state and local unless depleted, until September 17, 2010, for a standard single/double room plus occupancy taxes. These rooms will be held at which time they will be released to applicable state and local occupancy as a block, unless depleted, until August 10, the public. After September 17, room rate taxes. These rooms will be held as a block, 2010, at which time they will be released to and availability cannot be guaranteed. To unless depleted, until October 11, 2010, the public. After August 10, room rate and make a reservation call 816-474-6664 or at which time they will be released to availability cannot be guaranteed. To make (toll-free Worldwide) 800-227-6963. State the public. After October 11, room rate your reservation call 619-692-3800 or (toll- that you will be attending a University of and availability cannot be guaranteed. free worldwide) 800-228-9290. State that Kansas aerospace short course and give For reservations call 407-352-1100 or you will be attending a University of Kansas the group code AER. All reservations must (toll-free worldwide) 800-327-0363. State aerospace short course and give the group be guaranteed by credit card, guest check that you will be attending a University of code KANKANA. All reservations must be or money order. Kansas aerospace short course. No group code number was available at the time guaranteed with a major credit card. Participants are responsible for their own of publishing. All reservations must be parking fees. The Crowne Plaza Kansas Participants are responsible for their own guaranteed by credit card, guest check or City Downtown will offer a discounted parking fees. The San Diego Marriott money order. Mission Valley will offer a discounted rate rate of $6.50 a day for overnight self- of $7 a day for overnight self-parking and parking and day guests. Self-parking at the hotel is free for attendees. day guests. The Kansas City International Airport (KCI) The San Diego International Airport is 19 miles (30.6 km) from the Crowne The Orlando International Airport (ORL) is (SAN) is 8.1 miles (13 km) from the hotel. Plaza Kansas City Downtown hotel. 13 miles (20.9 km) from the Doubletree SuperShuttle provides transportation for SuperShuttle provides transportation for Resort Orlando–International Drive. $12 each way to/from the Marriott Mission $17 each way to/from the hotel. (Fees are OrlandoFREEAirportToHotelShuttle.com Valley hotel. (Fees are subject to change.) subject to change.) Arrangements can be provides round-trip transportation The shuttle picks up at all ground made online at www.supershuttle.com or between the Orlando International transportation islands; no reservations are by calling 817-329-2000 or (toll-free in the Airport and the hotel for $23. (Fees are required. SuperShuttle customer service United States) 800-258-3826. Be sure to subject to change.) Reservations are numbers are 858-974-8885 or (toll-free in use the group code UPBP7. required and can be made online at www. the United States) 800-258-3826. orlandofreeshuttle.com or call 866-219-3733 (toll–free in the United States). This service does not take walk- ups. Shuttle hours are approximately 5:30 a.m. to 10 p.m. Mears Transportation provides 24-hour shuttle service for $18 one-way or $29 round trip. Reservations can be made on- line only at www.mearstransportation.com. (Fees are subject to change.) Walk-up service is available at the Mears Transportation kiosk on Level One of the airport (follow signs to Ground Transportation). If you are planning to attend one of our programs in the United States, and you are not a U.S. citizen, please visit http://travel.state.gov/visa/visa_1750.html for visa information.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 10 Orlando Advanced Flight Tests I nstructors: Donald T. Ward and Thomas William Strganac

O rlando, Florida Daye On measures of merit, unsteady lift, thrust November 15–19, 2010 • Why such advanced tests? Basic vector control, vortex control AA111210 philosophy and attitudes, overview • Experimental tools for preflight of documents describing governing preparation: water tunnel tests and flow Monday–Thursday 8 a.m.–4 p.m. regulations, history visualization tools, static wind tunnel Friday 8 a.m.–2 p.m. • Fundamental principles of aeroelasticity: tests, dynamic wind tunnel tests, rotary balance tests Class time 33 hrs. description of static and dynamic CEUs 3.3 aeroelastic phenomena; definitions, terminology and assumptions; limitations Dayr Fou of theory; flutter analysis; development of Description • Instrumentation for post-stall flight tests: basic aeroelastic equations; interpretation sensors needed and their specifications; Provides practical knowledge of supporting analyses needed to plan a series of flutter pre-test planning and preparation: data envelope expansion tests safely and • Experimental and analytical tools used requirements, flight test team preparation comprehensively. Includes procedures in preflight preparation: modal methods, and training, flight simulation; maneuver for post-stall certification and ground vibration tests and analysis, wind monitoring in real time for envelope demonstration of new or significantly tunnel test techniques, interpretation of expansion dynamically similar wind tunnel model data modified airplane designs to meet • Emergency recovery devices: types of civil or military requirements. devices available, sizing and other design Dayo Tw constraints, validation T arget Audience • Instrumentation for flutter envelope • Subsystem modifications for post-stall Designed for practicing and entry- expansion: suitable sensors, near real- testing: additional pilot restraint devices, level flight test engineers and time data analysis control system modifications, propulsion managers, aircraft engineers and • Subcritical response techniques, system modifications aircraft designers. interpretation of supporting analyses • Recommended recovery techniques; interpreting post-stall flight test results: F ee $2,295 • Interpreting test results: analyzing real- time data, postflight analysis of data analyzing real-time data, postflight Includes instruction, a course analysis of data notebook, Introduction to Flight Test • Expanding the envelope: excitation Engineering, Volumes I and II, by Donald methods, clearance to 85% flutter T. Ward, Thomas William Strganac and envelopes, example programs Day Five Rob Niewohner; AGARD Report #776 • Discussions of limit cycle oscillations • Guidelines and discipline for conducting Aircraft Dynamics at High Angles of advanced flight tests: test team training, Attack; refreshments and five lunches. incremental buildup to critical conditions, Day Three use of simulation, independent review The course notebook is for teams participants only and not for sale. • Foundations of post-stall flight testing: definitions of stall, departure, post-stall • Planning for efficiency in data collection gyrations and spins; description of spin and data management: tailoring the modes and spin phases; development of scope of the tests to the requirement; large disturbance equations of motion; identifying critical parts of the envelope; idealized flight path in a spin; balance combining maneuvers and integration of aerodynamic and inertial forcing of backup test points; using all available functions; autorotation and its causes; tools: real-time monitoring, automated effect of damping derivatives; effect of inserts; shared data processing between mass distribution; simplification of post- test site and home site stall equations of motion • Contingency planning: attrition of • Aerodynamic conditions for dynamic resources, backup support facilities, equilibrium: pitching moment safety guidelines and documentation; equilibrium, rolling and yawing moment course wrap-up and critique equilibrium; design goals and trends to provide post-stall capability: agility

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 11 Aerodynamic Design Improvements: High-Lift and Cruise I nstructors: C.P. (Case) van Dam and Paul Vijgen

Daye On Day Three S an Diego, California • Aircraft design and the importance of • Induced-drag reduction ranging from September 13–17, 2010 drag on fuel efficiency, operational cost classic linear theory to active reduction AA111000 and the environmental impact concepts including wingtip turbines and • Empirical drag prediction including scale tip blowing Monday–Friday 8 a.m.–4 p.m. effects on aircraft drag and examples of • Experimental techniques for laminar and Class time 35 hrs. drag estimates for several aircraft turbulent flows CEUs 3.5 • History of laminar flow for drag reduction • Impact of high-lift on performance • Natural laminar flow design, application, and economics of general aviation and Description certification and viability subsonic transport aircraft Covers recent advances in high- • Laminar flow control and hybrid laminar • Physics of single-element airfoils at high- lift systems and aerodynamics as flow control design and application lift including types of stall characteristics, well as cruise drag prediction and considerations including suction system Reynolds and Mach number effects reduction. Includes discussion of considerations numerical methods and experimental techniques for performance analysis • CFD-based drag prediction and Dayr Fou of wings and bodies and boundary- decomposition • High-lift physics of swept and unswept layer transition prediction/detection. single-element wings Dayo Tw • Physics of three-dimensional high-lift T arget Audience • Critical factors in CFD-based prediction systems including features of 3D high-lift Designed for engineers and managers flows and lessons from high Reynolds involved in the aerodynamic design • Boundary-layer transition prediction number tests and analysis of airplanes, rotorcraft and analysis ranging from empirical and other vehicles. to Parabolic Stability Equation (PSE) • Importance of boundary-layer transition, and Direct Numerical Simulation (DNS) relaminarization and roughness (icing, techniques rain) effects on high-lift aerodynamics F ee: $2,295 Includes instruction, course notebook, • Supersonic laminar flow including • Overview and survey of high-lift systems; refreshments and five lunches. boundary-layer instability, transition types of high-lift systems including mechanisms and control methods at support and actuation systems The course notebook is for supersonic speeds • High-lift computational aerodynamics participants only and not for sale. • Wave drag reduction at transonic and methods supersonic conditions • Passive and active methods for turbulent Day Five drag reduction • Passive and active flow separation control • Conceptual studies of high-lift systems including multidisciplinary approaches • High-lift characteristics of unconventional systems and configurations including canard and tandem-wing configurations, Upper Surface Blowing (USB), Externally Blown Flaps (EBF) and Circulation Control Wings (CCW) • High-lift flight experiments involving general aviation and transport type airplanes • Final observations

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 12 Kansas City Aerospace Applications of Systems Engineering I nstructors: Donald T. Ward, Mark Wilson and Mike Phillips

Kansas City, Missouri Daye On Day Three October 18–22, 2010 • Overview and terminology • Write code and system realization AA111190 • Acquisition and supply (creating a shared • Technical analysis and evaluation vision) • Tailoring the process (how much SE is Monday–Friday 8 a.m.–4 p.m. • Technical management (the planning enough?) Class time 35 hrs. exercise) • Configuration management CEUs 3.5 • Evolutionary acquisition, spiral development and open systems Description Dayr Fou Based on evolving systems • Applying systems engineering to engineering standards, EIA/IS 632 Dayo Tw hardware (NASA X-38 Case Study) and IEEE P1220 and Version 3.1 of • Technical management (just teamwork— • Class exercise (applying principles of the INCOSE Systems Engineering or integrated teaming) systems engineering) Handbook. Provides a working • Technical management (risk knowledge of all elements, management and performance tools) technical and managerial, involved Day Five • System design (requirements—second in systems engineering as applied • Software intensive systems engineering time around) to aerospace systems of varying (lessons learned) complexity. Concentrates on the • Functional analysis/allocation most troublesome areas in systems • Intensive systems engineering (case • Solution definition development: requirements studies) derivation, documentation, • Course summary and wrap-up allocations, verification and control. Hardware and software systems case studies from several sectors of the aerospace industry will be used as systems development examples. Techniques have been used on many DoD and NASA programs and also are applicable to commercial and civilian projects.

T arget Audience Designed for systems engineers at all levels and program managers developing large or small systems.

F ee $2,295 Includes instruction, a course notebook, INCOSE Systems Engineering Handbook, supplemental material, refreshments and five lunches. The course notebook is for participants only and not for sale. Great blend of principles and practices. I appreciated the numerous practical examples of applied systems engineering in previous projects. The instructors brought both a seasoned perspective and fresh examples of practices useful for today’s systems engineer. Shiloh Fischer, Lt. Col. U.S. Air Force www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Kansas City 13 Airborne Equipment Design and RTCA DO-160 (NEW) I nstructor: Ken Vranish

Daye On Day Three Kansas City, Missouri • History and background of why DO-160 • Magnetic effect October 18–21, 2010 • Explanation of aircraft environment • Power input AA111170 • Overview of DO-160 • Voltage spike Monday–Thursday 8 a.m.–4 p.m. • Developing requirements to ensure DO- • Audio frequency conducted susceptibility Class time 28 hrs. 160 compliance in equipment designs • Induced signal susceptibility CEUs 2.8 - Temperature and altitude - Temp variation Day Four Description - Humidity • RF susceptibility This class is designed to educate system engineers, hardware design - Shock and crash safety • RF emission engineers and test engineers in the - Vibration • Lightning indirect susceptibility aspects of DO-160 as it pertains to the designs of airborne electronic - Explosion proof • Lightning direct effects equipment. For system and hardware • Review requirements development engineers, the intent is to educate Dayo Tw and empower them to develop • Waterproofness equipment designs that are compliant with DO-160 by design and avoid • Fluids susceptibility expensive redesigns to correct issues • Sand and dust found late in the development cycle during test. For test engineers, it is • Fungus resist intended to assist them in properly • Salt fog developing test plans for their • Icing products.

• ESD T arget Audience • Flammability This class is designed for system • The aircraft atmospheric radiation engineers responsible for developing environment requirements for airborne electronic equipment; hardware design engineers responsible for building such equipment and test engineers responsible for writing test plans.

F ee $1,995 Includes instruction, a course notebook, DO-160 Environmental Conditions and Test Procedures for Airborne Equipment, refreshments and four lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 14 San Diego Aircraft Icing: Meteorology, Protective Systems, Instrumentation and Certification I nstructors: Wayne R. Sand and Steven L. Morris

S an Diego, California Daye On Day Three September 21–24, 2010 • Icing hazard description • Ice accretion characteristics AA111140 • Atmospheric aerosols • Effects of ice on aircraft performance • Cloud physics of icing • Anti-ice systems Tuesday–Friday 8 a.m.–4 p.m. • Ground icing, atmospheric cooling • De-ice systems Class time 28 hrs. mechanisms CEUs 2.8 • Icing instrumentation, icing environment • Conceptual cloud modes: convective • Icing detection Description clouds, stratiform clouds • Skew-T, Log P adiabatic diagrams Covers meteorology and physics of Dayr Fou aircraft icing; forecasting, finding and • Effect of SLD on aircraft avoiding icing conditions; designing Dayo Tw and evaluating ice protection systems; • Engine icing considerations and certification of aircraft for flight • Icing environment analysis using Skew-T, • Ice-testing methods into known icing conditions. Log P • Assessment of icing potential • Certification and regulations T arget Audience • Critical icing parameters, theory and • Computational methods Designed for aerospace engineers, measurements • Review and discussion flight test and design engineers, test • Meteorology of supercooled large drops pilots, line pilots, meteorologists, FAA engineers and Designated • Finding/avoiding icing conditions Engineering Representatives (DERs) • New and current icing research and program managers. • Internet resources F ee $1,995 Includes instruction, course notebook, reference materials, refreshments and four lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Singapore | Seattle | Orlando 15 Aircraft Structural Loads: Requirements, Analysis, Testing and Certification I nstructor: Wally Johnson

Daye On Dayr Fou S ingapore • Introduction and background • Wing loads analysis March 1–5, 2010 • AA101300 • Basic aerodynamics overview • Horizontal tail loads analysis Monday–Thursday 8:30 a.m.–4:30 p.m. • Mass properties calculations and • Vertical tail loads analysis Friday 8:30 a.m.–Noon weight • Fuselage loads analysis Class time 31.5 hrs. CEUs 3.15 • External loads classifications (e.g., • Control surface and high-lift devices static loads, fatigue, dynamic, limit, loads analysis ultimate, inertia, etc.) S eattle, Washington • Data requirements and other April 26–30, 2010 • AA101330 disciplines’ involvement in the loads Day Five Monday–Thursday 8 a.m.–4 p.m. process • Miscellaneous loads (e.g., cabin Friday 8 a.m.–11:30 a.m. pressure, emergency landing, fuel • Certification requirements pressure loads, etc.) Class time 31.5 hrs. • External loads process steps from CEUs 3.15 • Static and fatigue test loads day one to certification day • Flight loads validation (e.g., ground O rlando, Florida loads calibration, in-flight loads November 15–19, 2010 • AA111220 Dayo Tw measurements) • Structural design airspeeds Monday–Thursday 8 a.m.–4 p.m. • Structural loads certifications Friday 8 a.m.–11:30 a.m. derivations process • Flight loads envelopes Class time 31.5 hrs. • Structural loads reduction CEUs 3.15 • V-n diagrams suggestions • Balancing tail loads derivations • Course summary and wrap-up Description • Pitch maneuvers analysis (e.g., Provides an overview of aircraft structural abrupt pitch up, abrupt pitch down, external loads analysis, including: criteria, design, checked pitch) analysis, fatigue, certification, validation and • Roll maneuver analysis testing. It covers FAR 23 and FAR 25 Airplane Loads Requirements; however, the concepts may be applicable for military structural requirements. Day Three Loads calculations examples using BASICLOADS • Yaw maneuver and engine out software will be demonstrated throughout the analysis course week. A copy of BASICLOADS software will be provided to attendees. • Basic structural dynamics overview • Static and dynamic gust analysis T arget Audience • Landing loads analysis Designed for practicing engineers and • Ground handling maneuver loads engineering managers whose responsibilities analysis include aircraft structures. • Fatigue loads analysis Fee $2,595 Singapore $2,295 All other locations Includes instruction, a course notebook, a copy of BASICLOADS software, refreshments and five lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 16 Fort Worth Aircraft Structures Design and Analysis I nstructor: Michael Mohaghegh and Mark S. Ewing This course may be taught by one or both instructors.

F ort Worth, Texas Daye On Day Three June 14–18, 2010 • Structural design overview: evolution • Design to static strength: mechanical AA101410 of structural design criteria; FAA joints and fittings; bonded and welded airworthiness regulations; structural joints; design exercise; highly loaded Monday–Friday 8 a.m.–4 p.m. design concepts, load paths tension structures; combined loads Class time 35 hrs. • Design requirements and validation of • Thin-walled structures: review of CEUs 3.5 aircraft loads: materials and fasteners, bending and torsion for compact beams; flutter and vibrations, static strengths, introduction to shear flow analysis of Description durability and damage tolerance, thin-walled beams; analysis exercise; crashworthiness, producibility, semi-tension field beams; design exercise; Introduction to analysis and design of maintainability and environment/discrete introduction to the finite element aircraft structures, including design events method criteria, structural design concepts, loads and load paths, metallic and composite materials; static strength, Dayo Tw Dayr Fou buckling and crippling, durability and • Metals: failure modes, design allowables • Design to buckling and stiffness: buckling damage tolerance; practical design testing; failure stacking sequence, of thin-walled structures, design exercise considerations and certification repeated loads; processing • Component design: wings and and repairs. Analysis exercises and a • Fiber-reinforced composites: laminated empennages, fuselage, landing gear, design project are included to involve composite performance; failure modes engine attachments, control surfaces students in the learning process. and properties; processing; moisture protection T arget Audience Day Five • Material selection: aluminum, titanium, • Design for damage tolerance: historical Designed for engineers, educators steel, composites and future materials; context of safe life, fail safety and damage and engineering managers whose design exercise responsibilities include aircraft tolerance; tolerating crack growth in structures. structures; widespread damage; testing; inspection; design exercise F ee $2,295 • Design for durability: fatigue, corrosion Includes instruction, a course • Design considerations: design notebook, refreshments and five for manufacture, design process lunches. management The course notebook is for • Certification: analysis and validation participants only and not for sale. requirements, component and full-scale air-craft testing requirements • Continued airworthiness: aging fleet, repairs

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 17 Airplane Flight Dynamics: Open and Closed Loop I nstructor: Jan Roskam

Daye On and irreversible, actuator sizing and S an Diego, California • The general airplane equations of hydraulic system design considerations. September 13–17, 2010 motion: reduction to steady state and • Applications of the perturbed state AA111010 to perturbed state motions; emphasis: equations of motion—complete and derivation, assumptions and applications approximate longitudinal transfer Monday–Friday 8 a.m.–4 p.m. • Review of basic aerodynamic concepts: functions; short period, phugoid, Class time 35 hrs. airfoils—lift, drag and pitching moment, third mode, connections with static CEUs 3.5 lift-curve slope, aerodynamic center; longitudinal stability, sensitivity analyses, Mach effects; fuselage and nacelles— equivalent stability derivatives; complete destabilizing effect in pitch and in yaw; and approximate lateral-directional Description wings, canards and tails—lift, drag and transfer functions—roll mode, spiral Overview of airplane static and pitching moments; lift-curve slope; mode, Dutch roll mode and lateral dynamic stability and control theory aerodynamic center; downwash; control phugoid, connections with static lateral- and applications, classical control power; Mach effects directional stability, sensitivity analyses, theory and applications to airplane equivalent stability derivatives • Longitudinal aerodynamic forces and control systems. moments: stability and control derivatives Dayr Fou for the steady state and for the perturbed • Review of handling qualities criteria; MIL- T arget Audience state, example applications and F-8785C and FARs, Cooper-Harper ratings, Designed for aeronautical, control interpretations relation to system redundancy, the system and simulator engineers, airworthiness code pilots with engineering background, Dayo Tw government research laboratory • Lateral-directional aerodynamic forces • Introduction to Bode plots: method of personnel and educators. and moments: stability and control asymptotic approximations, interpretations derivatives for the steady state and of Bode plots, airplane Bode plots, for the perturbed state, example applications of inverse Bode method; F ee $2,295 applications and interpretations introduction to linear feedback systems, the Includes instruction, Airplane Flight root-locus method and the Bode method • Thrust forces and moments: steady state Dynamics and Automatic Flight to synthesize control systems and perturbed state Controls, Parts I–II; Airplane Design, • Introduction to human pilot transfer Parts IV, VI, and VII; Roskam’s Airplane • The concept of static stability: definition, functions; analysis of airplane-plus-pilot-in- War Stories and Lessons Learned in implications and applications the-loop controllability; synthesis of stability Aircraft Design, all by Jan Roskam, • Applications of the steady state airplane augmentation systems—yaw dampers, refreshments and five lunches. equations of motion: longitudinal moment pitch dampers; effect of flight condition, equilibrium, the airplane trim diagram sensor orientation and servo dynamics (conventional, canard and flying wing), airplane neutral point, elevator-speed Day Five gradients, the nose-wheel lift-off problem; • f Synthesis o stability augmentation neutral and maneuver point (stick fixed) systems—yaw dampers, pitch dampers, α-feedback, β-feedback; effect of flight • Applications of the steady state airplane condition, sensor orientation and servo equations of motion: lateral-directional dynamics; basic autopilot modes; moment equilibrium, minimum control longitudinal modes—attitude hold, speed with engine-out control-wheel steering, altitude hold, speed Day Three control and Mach trim; lateral-directional • Effects of the flight control system: modes— bank-angle hold, heading reversible and irreversible flight controls; hold, localizer and glide-slope control, control surface hinge moments, stick automatic landing; coupling problems— and pedal forces, force trim; stick-force roll-pitch and roll-yaw coupling, pitch gradients with speed and with load rate coupling into the lateral-directional factor; neutral and maneuver point stick modes, nonlinear response behavior; free; effect of tabs—trim-tab, geared-tab, effects of aeroelasticity—aileron reversal, servo-tab, spring-tab; effect of down- wing divergence, control power reduction; spring and bob-weight; flight control effect of aeroelasticity on airplane stability system design considerations—reversible derivatives; example applications www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 18 Online Instruction Airplane Performance: Theory, Applications and Certification (Computer-based course) I nstructor: Jan Roskam, Mediated by Mario Asselin

O nline Instruction Course Overview We are excited to present this new Available anytime • Review of airfoil characteristics dynamic learning opportunity featuring Dr. Jan Roskam and Mario Asselin. • Review of wing characteristics AA101480 This state-of-the-art course delivery • Airplane drag breakdown features streaming video, animated Class time 28 hrs. illustrations, and the quality you would CEUs 2.8 • Drag prediction and use of wind tunnel expect from the University of Kansas data Aerospace Short Course Program. Description • Fundamentals of stability and control and Participants will be guided through various Overview of airplane performance the effect on performance course topics and will have the flexibility and prediction, performance • Fundamentals of flight mechanics to complete the sections at their own time applications, certification standards and pace. The course mediator will guide and the effects of stability and control • Take-off performance: prediction and you through a series of projects and will on performance. regulations: FAR/JAR 23/25 help answer any questions. • Landing performance: prediction and You will also have access to a discussion T arget Audience regulations forum so that you can communicate with Designed for aeronautical engineers, others taking the course. pilots with an engineering • Climb and drift-down performance background, simulator engineers, • Propeller and jet engine performance government research laboratory personnel and university faculty. • Range and endurance • Performance presentations for flight F ee $1,295 plus manuals $45 (USD) shipping within the U.S. $110 (USD) shipping to Canada and • Maneuvering performance stalls, buffet, turns, spins international destinations Includes online instruction, Airplane • Airplane weight sizing to required Aerodynamics and Performance, by mission performance C. Edward Lan and Jan Roskam and • Wing and powerplant matching to Airplane Design, Parts I, II, and VII, by Jan performance requirements Roskam. • Applications to regional jets • Fundamentals of flight testing for performance determination • Configuration design and its effect on performance • Payload-range and profit potential • Direct operating cost of airplanes • Bonus material: Inertial Roll Coupling lecture by Dr. Jan Roskam

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Seattle 19 Airplane Preliminary Design I nstructor: Jan Roskam

Daye On and retraction volume; take-off rotation; Class S eattle, Washington Review of drag polar breakdown for subsonic I weight and balance prediction; the c.g. April 26–30, 2010 and supersonic airplanes, rapid method for excursion diagram; Class I moment of inertia drag polar prediction, check of drag polar prediction; importance of establishing control AA101340 realism; review of fundamentals of flight over weight; preliminary structural arrangement mechanics: take-off and landing characteristics, for metallic and composite airframes; Monday–Friday 8 a.m.–4 p.m. range, endurance and maneuvering, the manufacturing and materials considerations; payload-range diagram; preliminary sizing of the V-n diagram; Class II weight, balance and Class time 35 hrs. airplane take-off weight, empty weight and moment of inertia prediction; fundamentals of CEUs 3.5 fuel weight for a given mission specification: static longitudinal stability; the trim diagram, applications; sensitivity of take-off weight to trim considerations for conventional, canard changes in payload, empty weight, range, and three-surface designs, tail and canard stall Description endurance, lift-to-drag ratio, and specific fuel Overview of the design decision- consumption; role of sensitivity analyses in Dayr Fou making process and relation of design directing program-oriented research and Continuation of fundamentals of static to manufacturing, maintainability development: applications; performance longitudinal stability; deep stall and how to and cost-effectiveness. Applicable to constraint analyses: relation between wing design for recoverability, effects of the flight jet transport, turbo-prop commuter loading and thrust-to-weight ratio (or wing control system; control force versus speed loading and weight-to-power ratio) for the transport, military and general and load factor gradients; flying quality aviation aircraft. following cases: stall speed, take-off field length considerations; additional stability and control and landing field length, statistical method for considerations; effect of flaps; minimum control estimating preliminary drag polars, review and speed with asymmetric thrust; take-off rotation T arget Audience effect of airworthiness regulations and the effect of landing gear location; review Designed for aeronautical engineers, of dynamic stability concepts and prediction Dayo Tw methods; short period, phugoid, spiral roll and pilots with some engineering Continuation of performance constraint Dutch roll modes; flying quality criteria: before background, government research analyses: relation between wing loading and and after failures in flight crucial systems; the laboratory personnel, engineering thrust-to-weight ratio (or wing loading and role and limitations of stability augmentation; managers and educators. weight-to-power ratio) for the following cases: review of control surface sizing criteria: trim, climb and climb rate (AEO and OEI), cruise maneuvering and stability augmentation; speed, and maneuvering; the matching of initial system gain determination; sensitivity F ee $2,295 all performance constraints and preliminary analyses and their use in early design decision Includes instruction, Airplane selection of wing area and thrust required: making; flight control system layout and design Aerodynamics and Performance by applications; preliminary configuration considerations; mechanical and hydraulically C. Edward Lan and Jan Roskam, powered flight controls; layout design selection; what drives unique (advanced) Airplane Design, Parts I–VIII, Lessons configurations? Discussion of conventional, considerations for redundant “flight-crucial” canard and three-surface configurations; systems: architectures associated with various Learned in Aircraft Design and Airplane fundamentals of configuration design, step-by- types; safety and survivability considerations; War Stories, all by Jan Roskam, step analysis of the feasibility of configurations: the airworthiness code; fundamental refreshments and five lunches. applications; fundamentals of fuselage and considerations in fuel system layout design; wing layout design; aerodynamic, structural sizing criteria; some do’s and don’ts; layout and and manufacturing considerations; effect of design considerations for “other” systems: de- airworthiness regulations; high-lift and lateral icing, water and waste water control design considerations; handling quality requirements; icing effects; layout design of Day Five horizontal tail, vertical tail and/or canard; static Landing gear design revisited, shock absorber stability and control considerations; the X-plot design, structural integration of the landing and the trim diagram; stable and unstable pitch gear, some do’s and don’ts; factors to be breaks; effect of control power nonlinearities; considered in estimation of: research and icing effects development cost and manufacturing and operating cost; the concept of airplane life cycle Day Three cost: does it matter in commercial programs? Fundamentals of powerplant integration: Discussion of 81 rules for “design for low cost;” inlet sizing, nozzle configuration, clearance the break-even point, estimation of airplane envelopes, installation considerations, “net worth” and its effect on program decision accessibility considerations, maintenance making; other factors in airplane program considerations; effect of engine location decision making, finding a market niche, risk on weight, stability and control; minimum reduction through technology validation, control speed considerations; fundamentals design to cost; lessons learned in past of landing gear layout design; tip-over criteria; programs: do we really learn them? FOD considerations; retraction kinematics www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 20 San Diego Applied Nonlinear Control and Analysis (NEW) Instructor: Bill Goodwine

S an Diego, California Daye On Dayr Fou September 20–24, 2010 • Identifying nonlinear phenomena such • Feedback linearization AA111100 as multiple equilibria, bifurcations, chaos, • Center manifold theory and stability nonunique and multiple solutions, limit • Bifurcation theory Monday–Friday 8 a.m.–4 p.m. cycles, finite escape time, sub- and super- harmonic response, etc. Class time 35 hrs. CEUs 3.5 • Nomenclature and definitions Day Five • The theory and process of linearization • Introduction to hybrid (switching) systems Description • The method of harmonic balance • Stability of hybrid systems under arbitrary This course covers analysis methods • Introduction to describing functions for nonlinear dynamical systems switching with the primary applications to • Stability of hybrid systems under feedback control. It is particularly Dayo Tw controlled switching designed for control engineers who • Describing functions examples are facing challenges due to more • Stability of hybrid systems under state- tightly integrated systems and systems • Nonlinear stability and Lyapunov dependent switching governed by controllers with switching functions behavior or logic. The nonlinear control • Control and the direct Lyapunov method applications covered are overviews • Methods for determining Lyapunov of describing functions, the direct functions Lyapunov method, the Lur’e problem and circle criterion, the small gain theorm, adaptive control, feedback Day Three linearization (dynamic inversion) and • The Lur’e problem, circle criterion and hybrid systems. The theoretical content, Popov Criterion which is the basis for understanding the control applications, consists of • The small gain theorem and applications identifying nonlinear phenomena, the • Stability of nonlinear nonautonomous process and theory of linearization, systems and boundedness Lyapunov stability, boundedness, center • Adaptive control manifold theory and bifurcations.

T arget Audience Designed for managers and engineers who work in the analysis and design of modern control systems.

F ee $2,295 Includes instruction, course notebook, supplemental material, refreshments and five lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Seattle 21 Aviation Weather Hazards I nstructor: Wayne R. Sand

Daye On • Icing forecasts: NWS forecasts; S eattle, Washington • Thunderstorms and strong convective experimental forecasts; cloud type April 27–30, 2010 forecasts, cumuliform (max intermittent) clouds: basic conceptual models, single- AA101390 cell storms, multi-cell storms and line and stratiform (max continuous); orographic influence storms Tuesday–Friday 8 a.m.–4 p.m. • Aircraft performance effects: de-iced • Stability and instability, storm tops and Class time 28 hrs. vertical motion and anti-iced aircraft; unprotected components; lift, drag, weight and CEUs 2.8 • Turbulence: causes and results, intensity, climb considerations; pilot action tornadoes considerations Description • Lightning: causes and results, composite • Icing sensors: in situ, remote, passive Examines the key weather hazards aircraft, lightning detection networks that affect all of aviation and provides • Detailed sensors for certification: • Heavy rain: raindrops and drop sizes, an in-depth understanding of the supercooled liquid water content, droplet most serious aviation weather hazards precipitation intensity, effects on sizes, temperature performance faced by all aspects of aviation. • How to find and/or avoid icing conditions Materials and instruction are designed • Radar: airborne weather radar, WSR-88D to provide enough depth to enable (NEXRAD), Stormscope pilots to make preflight and in-flight Dayr Fou • Hail: mechanisms to develop hail, visual weather-related decisions intelligently. and radar detection • Mountain weather: differential heating, Designed to provide flight test mountain and valley winds, channeling and design engineers the basic winds, thunderstorms, waves, rotors, information necessary to consider Dayo Tw density altitude weather factors when designing • Windshear: physics of microbursts, • Low ceiling and visibility: fog, various aircraft and aircraft components. stability and instability, precipitation types; snow, rain; low ceilings; conditional Flight dispatchers also will gain loading, evaporation, dry and wet forecasts, chance and occasional insight into aviation weather hazards, microbursts which should substantially enhance • Weather-related accident statistics: their ability to make weather-related • Gust fronts: thunderstorm generated, problem areas, NTSB and AOPA statistics, decisions. Course materials are also cold fronts, structure specific accident discussions designed to be used by RPV designers • Windshear training aid: detection signals, • New systems: ASOS, GOES, ADDS, and operators to better deal with flight crew actions AFSS, data link, rapid update cycle, new weather as it affects these vehicles. • Clear air turbulence: jet stream, display and depiction concepts, air traffic New weather data, products and thunderstorm wake, instability, waves, controller weather, others information sources will be discussed. deformation zones • Review and questions • Detection Systems: Terminal Doppler T arget Audience Weather Radar, Low-Level Windshear Designed for pilots, test pilots, Alert Systems, airborne forward-look meteorologists, flight test engineers, systems, airborne in situ systems, design engineers, dispatchers, RPV integrated terminal weather information designers and operators, government system and research laboratory personnel and educators. • Accidents: discussion of key accidents F ee $1,995 Day Three Includes instruction, a course • Basic icing physics: supercooled liquid notebook, refreshments and four water content, droplet sizes, temperature lunches. • Intensity and character: light, moderate, The course notebook is for and severe; continuous and intermittent; participants only and not for sale. collection efficiency; rime, clear and mixed

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 22 Singapore | Fort Worth | Kansas City Commercial Aircraft Safety Assessment and 1309 Design Analysis I nstructor: Marge Jones

S ingapore Daye On Day Three March 1–5, 2010 • AA101310 • System safety basics including • Failure Mode and Effects Analysis Monday–Thursday 8:30 a.m.–4:30 p.m. importance of structured systematic (FMEA)/Failure Mode Effects Friday 8:30 am.–Noon evaluations, system safety and Summary (FMES) reliability concepts and philosophies, Class time 31.5 hrs. • Reliability block diagrams and understanding 1309 regulations, and dependency diagrams CEUs 3.15 accident statistics/data • Fault Tree Analysis (FTA) concepts, F ort Worth, Texas • Overview of the SAE ARP 4761 Safety modeling techniques and examples, June 14–17, 2010 • AA101400 Assessment process for commercial qualitative evaluation (cutsets), aviation, aircraft and system Kansas City, Missouri quantitative evaluation, importance Functional Hazard Assessments and measures, and software tools October 18–21, 2010 • AA111180 allocating safety requirements • Class FMEA and FTA exercise All U.S. locations: Monday–Thursday 8 a.m.–4 p.m. Dayo Tw Class time 28 hrs. • System architecture concepts and Dayr Fou CEUs 2.8 design assurance levels including SAE • Common cause analysis: particular ARP 4754 Certification Considerations risk, zonal and common mode Description for Highly-Integrated or Complex • System safety assessment Covers safety assessment requirements of Aircraft Systems, DO-254 Certification FARs 23.1309, 25.1309, 27.1309 and 29.1309 Considerations for Airborne Complex • Tailoring methods to aircraft from fundamental analysis techniques to Electronic Hardware and RTCA modifications system integration; including Function DO-178 Software Considerations in Hazard Assessments, Failure Mode Effects Airborne Systems Analysis, Fault Tree Analysis and System Safety • Preliminary System Safety Assessments. Includes detailed review of SAE Assessments ARP 4754 and 4761. Principles apply to all critical and essential aircraft systems, as well as • Failure rate prediction techniques TC and STC projects. and class exercise

T arget Audience Designed for Parts 23, 25, 27 and 29 system certification engineers, system designers, FAA Designated Engineering Representatives (DER), aircraft certification personnel and military personnel procuring civil equipment.

Fee $2,595 Singapore $1,995 All other locations Includes instruction, four course notebooks, SAE ARP 4754–Certification Considerations for Highly-Integrated or Complex Aircraft Systems, SAE ARP 4761– Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment, reference materials, 1309 course and instructor was a didactic and helpful learning session and refreshments and four lunches. (Please note instructor was friendly and can really handle tough questions. Overall, all that the Singapore class is five days and KU staff are doing their job to the fullest to aid students to reach their goals. includes five lunches.) Keep up the good work. Myles Jalalian The course notebook is for participants only FAA and not for sale. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 23 Complex Electronic Hardware Development and DO-254 I nstructor: Leanna Rierson

Daye On How You May Benefit S an Diego, California • Introductions and background • Gain valuable insight into the September 22–24, 2010 • History and overview of DO-254 development and certification processes AA111150 for complex and programmable • FAA’s advisory material electronics. Wednesday–Friday 8 a.m.–4 p.m. • Complex electronic technology • Obtain practical keys for developing and Class time 21 hrs. • Framework of DO-254 assessing devices and systems to meet CEUs 2.1 the civil aviation standard: RTCA/DO-254. • Planning process • Obtain timely information about some • Development process Description of the more difficult topics related to This course provides the fundamentals complex electronic hardware, such of developing and assessing electronic Dayo Tw as “simple” hardware, microprocessor components to the standard RTCA/ assurance, firmware and hardware tools. • Validation and verification DO-254, Design Assurance Guidance • Learn the common pitfalls in applying for Airborne Electronic Hardware. It • Configuration management DO-254 and obtaining certification, is designed for developers, avionics • Process assurance (a.k.a. quality and ideas for how to address that issue engineers, systems integrators, aircraft assurance) proactively. designers and others involved in • Certification liaison process • Understand FAA’s policy and guidance. development or implementation of complex electronic hardware • Tools (e.g., Application-Specific Integrated Circuits, Field-Programmable Gate Day Three Arrays, etc.). The course also provides insight into the FAA’s review process • Firmware vs. software vs. hardware and guidance and provides practical • Microprocessor assurance keys for successful development and • Simple vs. complex certification. Practical exercises and in- class activities will be used to enhance • Structural coverage the learning process. • What to expect from certification authorities T arget Audience • Challenges in complex hardware Designed for developers, avionics development and certification engineers, systems integrators, aircraft • Summary designers and others involved in development or implementation of complex electronic hardware and programmable devices (e.g., Application-Specific Integrated Circuits, Field-Programmable Gate Arrays, etc.).

F ee $1,695 Includes instruction, a course notebook, the RTCA/DO-254 Design Assurance Guidance for Airborne Electronics Hardware Handbook, reference materials, refreshments and three lunches. Attendees should bring a pocket Enroll in this course and in Integrated Modular Avionics (IMA) and D0-297 calculator. (see page 34) and save money. The cost for the two courses combined is $2,295. The course notebook is for AA111160 participants only and not for sale. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 24 Orlando Conceptual Design of Unmanned Aircraft Systems I nstructors: Armand Chaput or Richard Colgren This class may be taught by one or both instructors.

O rlando, Florida Daye On How You May Benefit November 15–19, 2010 • Course introduction • Understand how to design and analyze AA111230 • Introduction to UAS overall unmanned aircraft systems. • UAS conceptual design issues • Understand how to estimate sensor size Monday–Thursday 8 a.m.–4 p.m. and performance and their impact on Friday 8 a.m.–11:30 a.m. • Fundamentals of system design overall system performance. Class time 31.5 hrs. • UAS operating environments • Understand basic elements of UAS CEUs 3.15 • Sortie rate estimates communications and know how to estimate overall communication system Description size and power requirements. Dayo Tw Conceptual approach to overall • Understand how to develop overall design of Unmanned Aircraft • Requirements analysis concepts of cooperation and assess Systems (UAS) includes concepts • Control station considerations and sizing impacts of sortie rate and supportability. of operations, communications, • Communication considerations/sizing • Understand key air vehicle configuration payloads, control stations, air vehicles drivers, how to estimate aero/propulsion/ • Payload (EO/IR and radar) considerations and support. Includes requirements weight/stability, overall air vehicle and sizing and architecture development, initial performance, size and trade-offs. sizing and conceptual level parametric • Reliability, maintainability and support and spreadsheet assessment of major • Understand how to bring all of the pieces system elements. • Life cycle cost together to optimize performance and • Decision making cost at the overall unmanned aircraft T arget Audience system level. Designed primarily for practicing Day Three conceptual-level design engineers, • Air vehicle parametric design systems engineers, technologists, researchers, educators and • Conceptual level aerodynamics engineering managers. Participants • Standard atmosphere models should have some knowledge of basic aerodynamics and conceptual design, • Parametric propulsion although it is not mandatory. Basic knowledge of spreadsheet analysis Dayr Fou methods is assumed. • Mass properties F ee $2,295 • Parametric geometry Includes instruction, a course • Air vehicle performance notebook, supplemental material, • Mission assessment refreshments and five lunches. • Methodology and correlation Attendees are encouraged to bring a laptop computer. Day Five The course notebook is for participants only and not for sale. • Air vehicle optimization • Overall system optimization • Class design presentation

An outstanding course for anyone in an aircraft systems design field. It gave me a foundation to evaluate or manage the design of systems. Well done. 1st Lt. Edward Pflugh U.S. Air Force Test Pilot School www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 25 Developing a Premier Aircraft Preventive Maintenance Program Based on the Principles of Reliability-Centered Maintenance (RCM) I nstructor: Neil Bloom

Daye On • Preventive maintenance—task S an Diego, California • Introduction to Reliability-Centered selection September 21-23, 2010 Maintenance (RCM) • Time-directed tasks AA111130 • Background of MSG Logic and RCM • Condition-directed tasks Tuesday–Thursday 8 a.m.–4 p.m. • Real-life disasters caused by inadequate • Failure-finding tasks preventive maintenance programs Class time 21 hrs. • Completing the PM task worksheet • Challenges of implementing an RCM- CEUs 2.1 Based PM Program • Predictive Maintenance (PdM) techniques Description • How to avoid the pitfalls • Probabilities as they relate to preventive This course explores in detail the background, • Explanation of the RCM concepts maintenance history, fundamentals and concepts of aircraft preventive maintenance. It also • The three phases of an RCM-Based PM • Sampling techniques Program includes learning how to avoid the pitfalls when attempting to develop a preventive • Understanding different failure modes Day Three maintenance program. Participants will learn the process and methodology for establishing, • Understanding the “canon law” for run- • RCM for instruments to-failure developing and implementing a premier • Instrument categories preventive maintenance program based • Understanding “hidden failures” on the principles of Reliability-Centered • Instrument design tolerance criteria • The “Missing Link” of RCM Maintenance (RCM). • The Instrument Logic Tree • What RCM is and what it is not Airline Maintenance Steering Group Logic • The RCM “Living Program” (MSG) and SAE Document JA1011 are • Understanding the differences thoroughly discussed. Participants will learn • Craft feedback evaluation element between redundant, standby and when a single-failure analysis is acceptable, backup functions • Corrective Maintenance (CM) when a multiple-failure analysis is required and evaluation element when a run-to-failure (RTF) strategy may be • Vendor manuals and bulletins invoked. Participants will be able to recognize Dayo Tw and appreciate the differences between • Preventive maintenance program • FAA Airworthiness Directives critical, potentially critical, commitment and implementation • Root cause analyses economic components as they relate to the “consequences” of equipment failures. • Databases • Preventive maintenance program • Informational resources audits T arget Audience • Information technology—software • A monitoring and trending strategy The target audience includes aircraft systems • RCM made simple: The implementation • How to measure reliability engineers, designers, quality assurance specialists, maintenance specialists, process defining an asset reliability • How to monitor reliability strategy production planners, pilots, airframe • How to trend reliability manufacturer representatives, airline • Minimum equipment list for aircraft maintenance and engineering personnel, departure eligibility • Aggregate metrics FAA personnel, and even senior-level • Understanding the Consequence of • Avoiding misleading KPI metrics management-selected aircraft mechanics and technicians. Failure Analysis (COFA) • RCM as an aerospace culture • Completing the COFA worksheet • Step-by-step review of the entire F ee: $1,695 process • The RCM decision logic process Includes instruction, a course notebook, Reliability Centered Maintenance— Implementation Made Simple, by Neil Bloom, refreshments and three lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 26 San Diego Digital Flight Control Systems: Analysis and Design I nstructor: David R. Downing

S an Diego, California Daye On Dayr Fou September 13–17, 2010 Introduction and Problem Definition, Flight Modern Design of Sampled Data MIMO AA111020 Dynamics: development of nonlinear Controllers: development and analysis of equations of motion, development of digital MIMO systems, development of Monday–Friday 8 a.m.–4 p.m. linear equations of motion, standard trim discrete and sampled data Linear Quadratic conditions, development of stability and Regulator, weighting matrix selection, Class time 35 hrs. control derivatives nonzero set point problem, proportional CEUs 3.5 Classical Design of Continuous Controllers integral structure, control rate weighting structure, PIF structure, design of typical Description Using SISO Tools: problem definition, Laplace Transforms, complex plane sampled data lateral and longitudinal This course presents a set of classical analysis of linear SISO systems, analysis of control modes for MIMO vehicles using and modern flight control analysis closed loop SISO systems, compensators, modern techniques. and design tools. These tools will be frequency response of linear first and combined to form a design process second order systems, Bode diagrams, Day Five that will enable the development system identification, design of SISO Output Feedback for Sampled Data of flight control systems that are closed-loop control systems. Controllers: development of output implementable in “real world” feedback design techniques, command vehicles. These techniques will be Dayo Tw generator tracker, output feedback-PIF- used to design typical aeronautical Classical Design of Continuous Controllers CGT MIMO-sampled data controllers, vehicles’ lateral and longitudinal design of typical sampled data lateral controllers. Using SISO Tools (cont.): Design of typical continuous lateral and longitudinal control and longitudinal control modes for MIMO vehicles using output feedback techniques. T arget Audience modes for continuous MIMO vehicles, implementation of perturbation controllers Designed for individuals from in nonlinear MIMO vehicles. government or industry who design, simulate, implement, test or operate Classical Design of Sampled Data digital flight control systems or who Controllers Using SISO Tools: problem need an introduction to classical and definition, develop models of sampler and modern flight control concepts. ZOH, complex plane analysis of linear SISO- sampled data systems, analysis of closed- loop SISO sampled data systems, z-plane F ee $2,295 compensators, design of typical sampled Includes instruction, a course data lateral and longitudinal control notebook, refreshments and five modes for continuous MIMO vehicles, lunches. implementation of perturbation controllers The course notebook is for in nonlinear MIMO vehicles. participants only and not for sale. Day Three Modern Design of Continuous MIMO Controllers: analysis of MIMO systems, development of continuous Linear Quadratic Regulator, weighting matrix selection, nonzero set point problem, proportional integral structure, control rate weighting structure, PIF structure, comparison of PIF and PID control structures, design of typical lateral and longitudinal control modes for continuous MIMO vehicles using modern techniques.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 27 FAA Certification Procedures and Airworthiness Requirements as Applied to Military Procurement of Commercial Derivative Aircraft/Systems I nstructors: Gilbert L. Thompson and Everett W. Pittman This course may be taught by one or both instructors.

Daye On • Utilizing FAA and Industry Guide to S an Diego, California • Review of course content and class Product Certification, specifically September 20–22, 2010 exercise Project-Specific Certification Plan (PSCP) principles in the Request for Proposal AA111090 • Overview of FAA Aircraft Certification (RFP) process (AIR) and Flight Standards (AFS) service Monday–Wednesday 8 a.m.–4 p.m. organizations as they relate to military • Impact of FAA Safety Management practices; FAA Form 337/Field Approval Class time 21 hrs. use of commercial derivative aircraft/ CEUs 2.1 systems process • Applicability of FAA Advisory Circulars, Description Day Three Notices and Orders Overview of FAA functions and • FAA “baseline” and “Project-Specific • Type Certification Data Sheets (TCDS) requirements applicable to Type Service Agreement” (PSSA) services • Impact of Part 36, Noise Standards; Design Approval, Production following Title 14, Code of Federal Airworthiness Directive (AD) process Approval, Airworthiness Approval, Regulations (CFR), Parts 1, 11, 21 applied to CDA and Continued Airworthiness associated with military-procured • Parts Manufacturer Approval (PMA) • Bilateral Aviation Safety Agreements commercial derivative aircraft and process (BASA) and European Aviation Safety products. Course will focus on the Agency (EASA) • Technical Standard Order Authorization unique military needs in procurement (TSOA) process • Impact of DoD acquisition policies as (customer versus contractor) of • Airworthiness Standards Parts 23, 25, 26, exemplified by USAF Policy Directives 62- products meeting civil airworthiness 27, 29, and 33 4, 62-5, 62-6, NAVAIR Instruction 13100.15, requirements which are aligned with and Army Regulation 70-62 military-specific mission/airworthiness • Part 183, Representatives of the goals. Administrator, including Subpart D, • Memorandum of Agreement/ Organization Designation Authorization Interagency Support Agreement (ODA) between DOT/FAA and Armed Services T arget Audience of the United States Designed, and focused in scope, • Comparison of DoD/FAA airworthiness specifically for U.S. Department Dayo Tw processes; application of MIL-HDBK- of Defense (DoD), Department of • Part 43, Maintenance, Preventive 516B, Airworthiness Certification Criteria; Homeland Security, U.S. Coast Guard, Maintenance, Rebuilding, and Alteration development of TACC/MACC and non-U.S. military procurement • Eligibility of Department of Defense and airworthiness personnel, and • Role of the FAA Military Certification associated military/supplier engineers, (DoD)/DoD contractor installations and Office (MCO) modification centers as FAA Part 145 consultants, project directors involved Repair Stations • FAA Order 8110.101, Type Certification in procurement of Commercial Procedures for Military Commercial Derivative Aircraft (CDA) or equipment • Part 39, Airworthiness Directives Derivative Aircraft developed for use on CDA. • Flight Standards Aircraft Evaluation • Certification options for CDA; use of FAA Group’s (AEG) role in aircraft certification Form 8130-31, Statement of Conformity– F ee $1,695 • Special conditions, equivalent level Military Aircraft Includes instruction, a course of safety and exemption process and notebook, supplemental material, issuance refreshments and three lunches. • Type Certification (TC) and Supplemental The course notebook is for Type Certification (STC) process (FAA participants only and not for sale. Handbook 8110.4)

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 28 Orlando FAA Conformity, Production and Airworthiness Certification Approval Requirements I nstructor: Donald Plouffe

O rlando, Florida Daye On How You May Benefit November 16–18, 2010 • Review course content and identification • Learn the FAA quality assurance system AA111270 of attendees’ key issues requirements for producing parts for the • Aircraft certification service versus flight civil aviation fleet. Tuesday–Thursday 8 a.m.–4 p.m. standards • Obtain a clear understanding of the FAA Class time 21 hrs. • Overview of 14 CFR Part 21 conformity inspection process. CEUs 2.1 • Designee and delegations • Understand the requirements and process leading up to an FAA production Description • Rules, policy and guidance approval. Presents the fundamental FAA • FAA conformity process • Gain an understanding of what the FAA requirements to produce products, considers the elements of a good-quality appliances and parts for installation Dayo Tw assurance system and how the FAA on FAA-type certificated products. audits the system. • Production approvals Includes FAA conformity process, • Learn the various FAA airworthiness quality assurance requirements, • Quality system requirements approvals and how they apply to your the FAA’s evaluation program, • Aircraft Certification Systems Evaluation product. airworthiness requirements and Program (ACSEP) certificate management. Also • Learn what it takes to export your includes a broad overview of • Certificate management products to other countries. the Organizational Delegation • Airworthiness approvals • Understand the FAA’s Compliance and Authorization (ODA) regulations, Enforcement Program. qualification, responsibilities, application, appointment, operation Day Three and management. • Airworthiness approvals • Compliance and enforcement T arget Audience • Organizational Delegation Authorization Designed for government and (ODA) industry (original equipment and suppliers) engineers, quality assurance personnel, Designated Airworthiness Representatives (DARs), and managers involved in the manufacture of products, appliances and parts installed on civil or military aircraft with FAA airworthiness certification.

F ee $1,695 Includes instruction, a course notebook, supplemental material, refreshments and three lunches. The course notebook is for participants only and not for sale.

This course was extremely informative and easy to grasp the basic principles without getting bogged down with too many detailed regulatory references. Highly recommended for individuals who seek a high-level view/description of the FAA certification process. Sidney “Butch” Sneade Navmar Applied Sciences Corp. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Seattle | San Diego 29 FAA Functions and Requirements Leading to Airworthiness Approval I nstructors: Gilbert L. Thompson and Everett W. Pittman The course may be taught by one or both instructors.

Daye On Day Three S eattle, Washington • Review of course content and • Continuation of typical TC and STC April 27–29, 2010 identification of attendees’ key issues projects AA101380 • Overview of FAA Aircraft Certification • Relation of Parts 23 and 25 to Civil (AIR) and Flight Standards (AFS) service Aviation Regulations (CAR), CARs 3 and Tuesday–Thursday 8 a.m.–4 p.m. organization and functions 4b Developing Type Certification Data Class time 21 hrs. • Advisory Circular, Notice and Order Sheets (TCDS) CEUs 2.1 process and issuance • Noise Certification Part 36; Airworthiness • Federal Aviation Regulations (FAR) Parts Directive (AD) process, Part 39 S an Diego, California 1 and 11 • AEG’s involvement in MMEL, September 15–17, 2010 • FAR Part 21 and the Technical Standard maintenance and flight manuals AA111070 Order Authorization (TSOA) process • Flight Standards Information Management System (FSIMS), notices Wednesday–Friday 8 a.m.–4 p.m. and orders related to airworthiness Dayo Tw Class time 21 hrs. • Bilateral Aviation Safety Agreements CEUs 2.1 • Parts 43 and 45 (BASA) • Part 36 Noise Requirements • U.S./European Union Executive Description • Part 39, Airworthiness Directives Agreement and the European Aviation Overview of the FAA organizational • Part 183, Representatives of the Safety Agency (EASA) structure and its function in aircraft certification, the rulemaking and Administrator, including Subpart D, • International Civil Aviation Organization advisory process, production rules Organization Designation Authorization (ICAO) (ODA); Flight Standards Aircraft applicable to aircraft and aircraft Evaluation Group’s (AEG) role in aircraft components, subsequent certification certification process and continued airworthiness. Course is specifically tailored toward • Parts 23, 25, 26, 27, 29, and 33 civil airworthiness certification. Course • Rulemaking and special conditions, is FAA-approved for IA renewal. process and issuance • Equivalent level of safety and exemption T arget Audience process Designed for industry (airframe and • Parts Manufacturer Approval (PMA) vendor) engineers, design engineers, civil airworthiness engineers, • Type Certification (TC) and Supplemental consultants, project directors, Type Certification (STC) process (FAA aircraft modifiers, FAA Designated Handbook 8110.4) Engineering Representatives (DER) • Certification Process Improvement (CPI), and coordinators, FAA organizational FAA and Industry Guide to Product designees/authorized representatives Certification, Partnership for Safety Plan (AR), industry and governmental (PSP)/Project Specific Certification Plan quality assurance inspectors and (PSCP) managers. • Safety Management concepts; documentation of typical TC and STC F ee $1,695 projects Includes instruction, a course notebook, supplemental material, • FAA Form 337/Field Approval refreshments and three lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 30 Orlando Flight Control and Hydraulic Systems I nstructor: Wayne Stout

O rlando, Florida Daye On Dayr Fou November 15–19, 2010 Introduction and background, system Mechanism fundamentals: mechanical AA111240 design methodology, design requirements advantage, gearing ratios, building (customer, business, regulatory, block mechanisms (linkages, bellcranks, Monday–Thursday 8 a.m.–4 p.m. engineering, environmental, competition), overcenter, dwell or lost motion, addition/ Friday 8 a.m.–11:30 a.m. design implications of requirements, amplification, yokes, cables, override and design requirement example, design disconnects, etc.), four bar linkages, gearing Class time 31.5 hrs. guides and manuals, testing, open and fundamentals, gearing systems including CEUs 3.15 closed-loop systems, system analysis standard/planetary gear trains, power (nonlinear simulations, linear analysis screws, nonlinearities, stiffness, examples of Description models and nonlinear analysis models) mechanical systems, examples Covers fundamental design issues, Hydraulic fundamentals: fluid properties Flight control system design: flight control system requirements, and analysis (density, viscosity, bulk modulus), fluid flow configurations (reversible, irreversible, design methodologies for aerospace (tubes, orifices, servo), pressure transients fly-by-wire), mechanization of flap/slats, hydraulic and flight control systems. in fluid flow, conservation of mass and flight control system design issues, impact Includes design requirements, momentum, basic hydraulic system of certification regulations, failure modes component description and modeling equations, computer-aided (jams, runaways, slow overs), safety analysis operation, component and system modeling of hydraulic systems, examples issues and redundancy, flight control math modeling, component sizing, system design methodology and examples system layout rationale, system sizing Dayo Tw and airframe integration. Emphasizes Day Five the fundamentals and necessary Hydraulic components: operation, engineering tools (both analytical and examples, fundamental equations for Flight control system airframe integration, otherwise) needed to understand and each component and component hydraulic system integration, fault design aerospace hydraulic and flight sizing, components include actuators, detection, fly-by-wire actuation control systems. Practical examples metering valves, relief valves, shuttle Extensions to current system design and actual systems are presented and valves, pumps, motors, check valves methods: hybrid system modeling, Design discussed throughout the class. and fuses, accumulators, reservoirs, of Experiments (DOE), comprehensive pressure regulation, and flow control, testing, sensitivity methods, probabilistic T arget Audience thermodynamics of hydraulic systems, methods, references and resources examples Designed for system and component How You May Benefit level engineers and managers, Day Three including airframe, vendor, industry, • Learn the fundamentals and enhance government and educators involved Servovalves (flapper, jet pipe and motor- overall knowledge of flight control and with aerospace mechanical systems. controlled) hydraulic system design. Hydraulic system design: basic system • Improve understanding of component F ee $2,295 configurations, power generation systems, operation, performance characteristics, Includes instruction, a course landing gear control, brake systems, flaps/ sizing and modeling. slats, spoilers, steering, thrust reversers, notebook, refreshments and five • Understand the governing physical lunches. primary flight control, actuation examples (mechanical and electrical) equations for the various components/ Attendees should bring a pocket systems and how they can be utilized to calculator. Hydraulic system design issues, impact of address fundamental design issues. certification regulations, hydraulic system The course notebook is for design methodology, failure modes, safety • Gain an appreciation for the issues and participants only and not for sale. analysis issues and redundancy, integration requirements associated with aircraft with mechanical systems mechanical systems. • Improve knowledge of sensitivity and robust design methods that are applicable to mechanical system design.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Seattle | San Diego 31 Flight Test Principles and Practices I nstructor: Donald T. Ward

Daye On Dayr Fou S eattle, Washington • Flight test overview and introduction; • Advanced performance methods: April 26–30, 2010 the atmosphere: properties, altimetry, nonstabilized performance methods, AA101350 pneumatic lag turning performance, ground effect Monday–Friday 8 a.m.–4 p.m. • Air data principles and measurements: measurement, getting more for less from airspeed, altitude, Mach number, alpha flight tests Class time 35 hrs. and beta • Static stability and control: longitudinal CEUs 3.5 and lateral-directional static stability • Mass, center of gravity, and moment of S an Diego, California inertia determination testing September 20–24, 2010 • Time/space position measurements • Dynamic stability and control: dynamic mode characteristics and measurement AA111110 • Handling qualities: Cooper-Harper Monday–Friday 8 a.m.–4 p.m. Dayo Tw scale, FAR and mil-spec requirements, Class time 35 hrs. • Air data calibration methods: position workload scale CEUs 3.5 error; temperature probe, angle of attack, • Parameter identification: regression and sideslip calibration analysis, maximum likelihood estimation Description • Instrumentation system principles: of derivatives design requirements, static and dynamic Introduction to flight test process, response, calibration principles and practices. Engineering Day Five principles and their application to • Data recording and processing methods: • Thrust drag accounting, isolation and the flight testing of aircraft will be analog, digital, filtering, and signal covered. conditioning; proper use of digital bus measurement of component drags data (MIL-1553, ARINC 429, 629) for flight • Structural flight tests: static loads, flutter T arget Audience testing • Flow visualization: tufts, flow cones, Designed for all levels of engineers • Propulsion system testing: piston, sublimating chemicals, liquid crystals, and managers in industry working turboprop, and turbofan engines dyes, smoke injection; test methods on flight test projects, military and • In-flight measurement of thrust and • Spin testing: test methods, safety issues civil project engineers, test pilots and flight test engineers, government power • Systems testing and evaluation: research laboratory personnel, and communication, navigation, SAS and FAA and other regulatory agency autopilots Day Three engineers. • Stall tests: stall speed determination, stall characteristics, stall protections systems F ee $2,295 • Flight test program planning: Includes instruction, a course organization, milestones, flight cards, notebook, Introduction to Flight Test documentation, procedures, safety issues Engineering, Volume I, by Donald T. • Takeoff and landings and cruise Ward, Thomas W. Strganac and Rob performance: speed, range, and Niewohner, refreshments and five endurance lunches. • Climb performance: test methods, The course notebook is for correction to standard conditions, participants only and not for sale. specific energy concepts

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 32 Singapore | Seattle | San Diego | Kansas City | Orlando Fundamental Avionics I nstructors: Albert Helfrick, Brian Butka, William Barott and Robert Chupka This course may be taught by one instructor or a combination of instructors, depending on availability.

S ingapore Daye On Dayr Fou March 1–5, 2010 • AA101320 • Early history of aviation and wireless • Inertial navigation Monday–Thursday 8:30 a.m.–4:30 p.m. • History of regulatory and advisory • Laser gyros Friday 8:30 a.m.–3:15 p.m. bodies • Random Navigation, RNAV Class time 33.75 hrs. • Establishment of the National • Required Navigation Performance, CEUs 3.375 Airspace System, NAS RNP Displays S eattle, Washington • Federal Aviation Regulations, FAR • Human factors April 26–30, 2010 • AA101360 • European regulatory and advisory • Electromagnetic compatibility agencies • High Intensity Radiated Fields, HIRF • Radio navigation San Diego, California • Lightning effects September 13–17, 2010 • AA111030 • Antennas and radio beams • Nondirectional beacon Day Five Kansas City, Missouri • VHF Omni range • Airborne environment, DO-160 October 18–22, 2010 • AA111200 • Distance measuring, DME • Failure analysis Orlando, Florida • Safety assessment Dayo Tw November 15–19, 2010 • AA111250 • Design assurance levels • Long-Range Navigation, LORAN • Reliability prediction, MIL-HDBK 217 All U.S. locations: • Landing Systems, ILS Monday–Thursday 8 a.m.–4 p.m. • Software considerations, DO-178 • Radar altimeter Friday 8 a.m.–2:45 p.m. • Hardware considerations, DO-254 • Ground proximity warning systems Class time 33.75 hrs. • Flight data recorder CEUs 3.375 • Terrain Awareness and Warning System, TAWS • Cockpit voice recorder Description • Satellite navigation This course is a comprehensive study of • Global Positioning System, GPS avionics from the simple stand-alone systems to the latest integrated systems. The theory of operation is covered as well as the environment Day Three and certification processes. • Secondary radar, Mode A/C, Mode S T arget Audience • Collision avoidance, TCAS Designed for avionics engineers, electronic • Automatic Dependent Surveillance, testing laboratory personnel, airframe systems Broadcast, ADSB and flight test engineers, government research • Weather radar laboratory personnel, FAA Designated • Lightning detection Engineering Representatives (DERs) and military personnel procuring civil equipment. • Airborne communication • Aeronautical telecommunications Fee network $2,595 Singapore • Data buses/networking $2,295 All other locations • Compass/gyros Includes instruction, course notebook, Principles of Avionics, by Albert Helfrick; supplemental • Air data systems materials, refreshments and five lunches. The course notebook is for participants only and not for sale. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Fort Worth | San Diego 33 Helicopter Performance, Stability and Control I nstructor: Ray Prouty

Daye On Dayr Fou F ort Worth, Texas • The hovering helicopter • Airfoils for rotor blades June 14–18, 2010 • Factors affecting hover • Anti-torque systems AA101420 • Vertical flight • Empennages and wings Monday–Thursday 8 a.m.–4 p.m. • Momentum theory of forward flight • Other configurations: tandems, coaxials, Friday 8 a.m.–11:30 a.m. synchropters, tilt-rotors, tilt-wings • Blade-element theory of forward flight Class time 31.5 hrs. • The preliminary design process CEUs 3.15 Dayo Tw S an Diego, California • Blade-element theory of forward flight Day Five (continued) • Noise September 13-17, 2010 • Forward flight computer program • Vibrations AA111040 • Estimating performance • Helicopter accidents Monday–Thursday 8 a.m.–4 p.m. • Calculating performance characteristics Friday 8 a.m.–11:30 a.m. • Maneuvering flight Class time 31.5 hrs. CEUs 3.15

Day Three Description • Rotor flapping characteristics What the working helicopter • Trim and static stability aerodynamicist needs to know • Dynamic stability to analyze an existing design or participate in the development of • Aerodynamic considerations of main a new one. Covers all aspects of rotor hover, vertical flight and forward flight. Emphasis on relating helicopter aerodynamics to airplane aerodynamics for those who are making the transition.

T arget Audience Designed for engineers, engineering managers and educators who are involved in helicopters.

F ee $2,295 Includes instruction, a course notebook, refreshments and five lunches. The course notebook is for participants only and not for sale.

Who needs Wikipedia when you have Ray Prouty as an instructor! Edward Brian Moeller Sikorsky Aircraft Company www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 34 San Diego Integrated Modular Avionics (IMA) and DO-297 (NEW) I nstructor: Leanna Rierson

S an Diego, California Daye On Dayo Tw September 20-21, 2010 • Introductions and background • DO-297 (continued) AA111080 • What is IMA? • Technical highlights of DO-297 • What are the benefits of IMA? • Design guidelines Monday–Tuesday 8 a.m.–4 p.m. • History of IMA and supporting • Partitioning analysis Class time 14 hrs. certification guidance CEUs 1.4 • Health management • Overview of the IMA guidance material • Integration Description • TSO-C153 (Integrated Modular Avionics • Configuration files and configuration This course provides the Hardware Elements) management fundamentals for developing and • Purpose of TSO-C153 integrating IMA systems, using • Certification approach of DO-297 TSO-C153 (Integrated Modular Avionics • Limitations of TSO-C153 • Six certification tasks Hardware Elements), FAA Advisory • Experiences to date with TSO-C153 • Life cycle processes Circular 20-145 (Guidance for Integrated • TSO-C153 contents Modular Avionics [IMA] that Implement • Life cycle data TSO-C153 Authorized Hardware • Developing a Minimum Performance • FAA’s plans for recognizing DO-297 Elements), and DO-297 Integrated Specification per TSO-C153 • ARINC 653 Usage in IMA Systems Modular Avionics (IMA) Development • Unique aspects of TSO-C153 Guidance and Certification • Using TSO-C153, AC 20-145, DO-297, and Considerations. Practical exercises • FAA Advisory Circular 20-145 (Guidance ARINC 653 together for Integrated Modular Avionics [IMA] that and in-class activities will be used to • Common challenges in IMA enhance the learning process. Implement TSO-C153 Authorized Hardware Elements) development and certification T arget Audience • Purpose of the Advisory Circular (AC) • Practical tips for IMA development and certification Designed for developers and • Technical highlights from the AC integrators of integrated modular • Roles and responsibilities avionics systems. The focus will be on How You May Benefit • Considering TSO-C153 and AC 20- identifying challenges with IMA and • Gain valuable insight into the IMA 145 from various user perspectives satisfying the regulatory guidance. development and certification (e.g., avionics developer and aircraft processes. manufacturer) F ee $1,295 • Understand the importance of IMA • DO-297 (Integrated Modular Avionics [IMA] Includes instruction, a course design assurance. Development Guidance and Certification notebook, RTCA DO-297 Integrated Considerations) • Obtain practical insight into how to Modular Avionics (IMA) Development address some of the common IMA • Overview of DO-297 Guidance and Certification challenges. Considerations, refreshments and two lunches. • Understand FAA’s IMA policy and guidance. The course notebook is for participants only and not for sale.

Enroll in this course and in Complex Electronic Hardware Development and D0-254 (see page 23) and save money. The cost for the two courses combined is $2,295. AA111160 www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Orlando 35 Operational Aircraft Performance and Flight Test Practices I nstructor: Mario Asselin

Daye On How You May Benefit O rlando, Florida Introduction; atmospheric models; • Review basic airplane performance November 15–19, 2010 airspeeds; position errors; drag polar and theory. AA111260 engine models; weight and balance • Determine what needs to be tested to build performance models. Monday–Friday 8 a.m.–4 p.m. Dayo Tw • Determine the required instrumentation Class time 35 hrs. Stall speeds and stall testing; stall to best measure airplane performance. CEUs 3.5 warning and stall identification; required • Understand the scatter normally instrumentation and data reduction; Description testing for low-speed drag, excess thrust expected during flight testing and how monitoring; check climbs; high-speed drag appropriate feedback from engineering Overview of airplane performance and basic flight envelope limits helps the flight crew minimize this theory and prediction, certification scatter. standards and basic flight test practices. Course will focus on • Develop performance models to match Day Three turbojet/turbofan-powered aircraft flight test results. Aircraft range; measuring SAR; data certified under JAR/CAR/14 CFR reduction; presenting the information to • Understand the safety level built-in Part 25. This standard will briefly aircrews; climbing performance; WAT limits; certification requirements and their be compared to military and Part turning performance impact on airplane performance. 23 standards to show different • Understand how to show compliance to approaches to safety, certification, Dayr Fou the certification authorities. operational and design differences. Take-off performance, basic models; flight • Learn how to present the airplane test; rejected takeoff; presenting the performance information to the flight T arget Audience information to the flight crew (AFM, flight crew. Designed for aeronautical manuals) engineers in the design or flight test • Understand how to set operational limits departments, educators, aircrews with to ensure continued operational safety. Day Five engineering background and military Landing performance; presenting the personnel involved in managing fleets information to the flight crew (AFM, flight of 14 CFR Part 25 (FAR 25)-certified manuals); consideration for contaminated aircraft. runways (CAR/JAR); obstacle clearance; accounting for high temperature deviation F ee $2,295 for minimum altitude flights Includes instruction, a course notebook, An Introduction to Aircraft Performance, by Mario Asselin, refreshments and five lunches. The instructor recommends bringing a laptop computer with Excel to work exercises. The course notebook is for participants only and not for sale.

Remarkable breadth and depth of aircraft performance coverage given the five- day course duration, skillfully presented within the integrated contexts of FAA certification requirements, airplane performance theory and pilot operations. Professor Asselin perfectly balances these elements to deliver a masterful treatment of aircraft performance from the analysis stage to flight test, backed by his vast industry experience and dedication to teaching. Pure delight! Alexandre Ly The Boeing Company www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 36 Seattle Principles of Aeroelasticity I nstructor: Thomas William Strganac

S eattle, Washington Daye On Dayr Fou April 26–30, 2010 • Overview and foundation • Flutter Identification AA101370 • Introduction and historical review • Review of flutter models • Fundamentals: definitions, similarity • The flutter boundary: civilian and military Monday–Thursday 8 a.m.–4 p.m. parameters and aeroelastic stability requirements, matched point flutter Friday 8 a.m.–2 p.m. boundaries analysis Class time 33 hrs. • Static aeroelasticity: divergence, lift • Case studies: examples of flutter analysis CEUs 3.3 effectiveness, control effectiveness, • Experiments: ground vibration tests, wind reversal and active suppression Description tunnel tests • Introduction to dynamic aeroelasticity: Provides an in-depth understanding gust response, flutter, buzz of aeroelastic behavior for aerospace Day Five systems. Explores aeroelastic • Practice phenomena, structural dynamics and Dayo Tw • Aeroservoelasticity for flutter suppression fluid-structure-control interaction; • Theory also examines practical issues such • Aeroelastic tailoring as ground and flight tests. Includes • Principles of mechanical vibrations • Wind tunnel tests solution methodologies, state-of- • Modal methods the-art computational methods for • Flight tests • Structural dynamics aeroelastic analysis, development • Nonlinear aeroelasticity: limit cycle of the operational boundary, • Steady and quasi-steady aerodynamics oscillations, store-induced instabilities aeroservoelasticity and contemporary issues such as limit cycle oscillations • Concluding remarks and related nonlinear pathologies in Day Three aeroelastic systems. • Theory (continued) • Unsteady aerodynamics: “Theodorsen” T arget Audience aerodynamics, numerical methods and Designed for engineers and technical approximations, strip theory, vortex and managers involved in aerospace doublet lattice methods vehicle design, analysis and testing. • Methods of analysis • Governing equations for the aeroelastic F ee $2,295 system Includes instruction, a course • Frequency domain methods: modal notebook, Aeroelasticity, by Raymond formulations, V-g diagrams, K-method Bisplinghoff, Holt Ashley and Robert (U.S. method), and P-k method (British Halfman; Introduction to Flight Test method) Engineering, Volume II, by Donald T. Ward, Thomas William Strganac and • Time domain methods Robert Niewohner; refreshments and five lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 37 Principles of Aerospace Engineering I nstructor: Wally Johnson

Daye On • Introduction to aeroelasticity: certification S an Diego, California • Atmospheric models and airspeed requirements, static aeroelasticity: September 20–24, 2010 divergence, control reversal; dynamic measurements: standard air, air properties AA111120 calculations, airspeed measurements aeroelasticity: flutter analysis and testing • Introduction to certification • Design airspeeds: design airspeeds Monday–Thursday 8 a.m.–4 p.m. requirements: certification agencies, requirements and derivations; flight Friday 8 a.m.–11:30 a.m. envelope derivation airworthiness standards, military Class time 31.5 hrs. specifications • Structural loads: external loads CEUs 3.15 • Aircraft components and their functions: classifications; structural loads process wing, flaps, stabilizer, fin, control surfaces, and requirements Description reference geometries • Symmetrical maneuvers: V-n diagram; The objective of this course is to • Introduction to aerodynamics: review balanced maneuver and pitch maneuvers provide an overview and integrated of basic aerodynamic concepts: airfoil • Asymmetric maneuvers—roll maneuver, exposure to airplane aerodynamics, fundamentals, finite wings, lift, drag, yaw maneuver, and engine out conditions performance, propulsion, flight high speed aerodynamics, overview mechanics, mass properties, structural of wind tunnel testing, overview of Dayr Fou dynamics, aeroelasticity, structural computational fluid dynamics methods, loads, structures, ground testing, flight • Gust conditions: gust formula, discrete flow visualization testing and certification. The material gust conditions and continuous presented in this course is in the • Weight and balance: calculation of mass turbulence conditions properties: weight, center of gravity form of lecture notes and showing • Ground conditions: landing , taxi and and moment of inertia; establishing the examples of the Basic Aerospace ground maneuvers weight-cg envelope Engineering software. This course • Airframe loads: wing loads, horizontal tail shows the relationship between aircraft certification requirements, Dayo Tw loads, vertical tail loads, fuselage loads, fatigue loads engineering analysis and testing. • Introduction to propulsion: types of propulsion systems, thrust calculations • Aircraft structures: introduction to stress T arget Audience and ratings, engine efficiency analysis, structural elements, wing and fuselage structure, materials selection, This course is intended as an overview • Airplane performance: thrust and static and fatigue design, introduction to for nonaerospace engineering- power curves, pull-up and steady turn finite element method. degreed professionals, managers, maneuvers, takeoff, landing and cruise military and government personnel performance; climb performance, range, • Ground testing: instrumentations, bird who are involved in aircraft design and endurance strike, landing gear drop test, ground and certification. vibration, ground loads calibration, static • Flight mechanics: aircraft axis systems, loads tests and fatigue loads tests aircraft equations of motion, static and F ee $2,295 • Flight testing: certification requirements, lateral-directional stability, longitudinal Includes instruction, a course instrumentations, flutter, flight loads and lateral-directional applied forces and notebook, a copy of Basic Aerospace validation, operational loads monitoring, moments; linearizing the equations of Engineering software, refreshments function and reliability tests, stall speeds and motion and five lunches. operational speeds, longitudinal stability and • Mechanics of materials: material behavior control, and directional stability and control The course notebook is for under loading, stress-strain relations, beam participants only and not for sale. bending and buckling, yield, compressive, tensile and fatigue strengths Day Five • Certification: certification agencies, Day Three certification process, how to show compliance • Introduction to mechanical vibrations and structural dynamics: certification • Airplane design: design requirements and requirements, equation of motion, free objectives, design optimization vibration, damped free vibration, mode • Airplane crashes: what went wrong, why, shapes, modal analysis structural failure, engine failure, landing failure, loss of control www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 38 San Diego Project Management for Aerospace Professionals I nstructor: Herb Tuttle

S an Diego, California Daye On Dayr Fou September 13–17, 2010 • Survey and benchmark, understanding • Project team, sources of people, AA111050 project management, leadership, compromise, control, support team, obstacles to successful projects, coordination, interaction, subcontractors, Monday–Friday 8 a.m.–4 p.m. definition of teams team dynamics, team success, • Project definition and distinguishing team development and traditional Class time 35 hrs. management role of internal project CEUs 3.5 characteristics, resources, project management process, typical problems, manager, theories of motivation, stimulating creativity, working through Description the triple constraint, obstacles, project outcomes, use of project teams group problems Designed to give aerospace • Strategic issues, proposals, starting professionals familiarity with Day Five current project management successful projects, contract negotiation, techniques. Includes identifying international projects and the true • Project cost reporting, computers, the functions of a project team and benefits of teamwork project changes, handling changes, team management team; the integration • Participant program or project plans building exercises of project management; work identified • Project or program plans presented by breakdown structures, interfaces, participants; projects evaluated and rated communications and transfers; • Current trends in project management estimating, planning, risk and Dayo Tw challenges of the project manager; • Internal project planning, issues, working alternative organizational structures; with the customer, use of software, team How You May Benefit decision making, planning hazards control and planning of time, money • Learn how to put together a program/ and technical resources. • Work breakdown structure, statement of project plan that fits management’s work, choosing team players needs. T arget Audience • Time estimating and scheduling, other • Understand program planning, project Designed for engineers and other planning methods, graphical tools, management and post-audit life cycle. technical professionals at all levels and time estimating, productive meetings, • Understand how systems engineering new project managers responsible meeting record keeping, goals of and project management fit within for small as well as large and long- meetings duration projects. program management. • Learn methods to manage “scope-creep” F ee $2,295 Day Three and manage change. Includes instruction, a course • Network diagrams, team improvement • Understand cost estimating, budgeting notebook, Project Management: activities, designate project teams and control. A Systems Approach to Planning, • Cost estimating, project cost system, • Learn how to develop and use teams to Scheduling, and Controlling, by Harold resources, time vs. cost trade-off complete successful projects. Kerzner, refreshments and five • Contingency, risk, cost/schedule lunches. • Understand how to establish project control, project organization, informal communication management. The course notebook is for organization, organizational forms, participants only and not for sale. team strategies, team development and • Understand project risk, analysis, traditional management monitoring and control. • Understand project procurement, subcontracting and contract management. • Learn how to retain knowledge of the team for future projects. • Learn about current topics in project management.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Online Instruction 39 Reliability and 1309 Design Analysis for Aircraft Systems (Computer-based course) I nstructor: David L. Stanislaw

Course Outline by Section O nline Instruction Available anytime 1. National Transportation Safety Board Accident Statistics AA101490 2. Learning from an Analysis of Power Industry Accidents Class time 28 hrs. 3. AOPA Nall Report and Boeing Statistical Summary CEUs 2.8 4. Pilot Causes of Accidents—Dr. Milton Survey Description 5. Safety in Aviation—Dr. Ir. H. Wittenberg Covers requirements of FARs 23.1309, 6. Historical 1309 Rules 25.1309, 27.1309, and 29.1309 from fundamental analysis techniques 7. Understanding FAR 25.1309 to system integration; includes 8. Built-in—Test and Probability Perspective construction of failure mode and Fault Tree Handbook effects analysis, criticality analysis and fault trees. Includes detailed review of 9. RTCA DO-167 Airborne Electronics Reliability SAE ARP 4754 and ARP 4761. Principles 10. MIL—HDBK—217 Reliability Prediction of Electronic Equipment AFSC 7 Part Derating apply to all critical and essential Guidelines aircraft systems. 11. RAC Electronic Parts Reliability Data T arget Audience 12. RAC Nonelectric Parts Reliability Data Designed for Parts 23, 25, 27 and 29 system certification engineers, 13. RAC Failure Mode/Mechanism Distributions airframe system designers, 14. DOD—HDBK—763 Human Engineering Procedures Guide FAA-Designated Engineering Representatives (DERs), aircraft 15. DOT/FAA/RD—93/5 Human Factors for Flight Deck Certification certification personnel and military personnel procuring civil equipment. 16. JAR—VLA—1309, FAR 23.1309 and FAR 25.1309 Review 17. FAA Advisory Circulars F ee $1,295 plus 18. SAE ARP4761 Safety Assessment Guidelines $35 (USD) shipping within the U.S. SAE ARP4754 Guidelines $95 (USD) shipping to Canada and international destinations 19. MIL—STD—1629 Procedures for Performing a Failure Mode, Effects and Criticality Analysis Fee includes instruction, a course notebook, Fault Tree Handbook, by 20. RTCA DO—178B Software Considerations in Airborne Systems D.F. Haasl, SAE ARP 4754—Certification 21. RTCA DO—254 Design Assurance Guidance for Airborne Electronic Hardware Considerations for Highly-Integrated or Complex Aircraft Systems, and SAE 22. FAA Order N8110.37 Delegated Functions and Authorized Areas ARP 4761—Guidelines and Methods 23. FAA AC 23.1309 Equipment, Systems and Installations for Conducting the Safety Assessment Process on Civil Airborne Systems and 24. AC 25.1309 System Design and Analysis Equipment. 25. AMJ 25.1309 Advisory Material Joint Participants are guided through the 28 course sections and have the 26. AC 25—19 Certification Maintenance Requirements flexibility to complete the sections 27. Databus Architectures and Interference and readings on their own time. Interaction with the instructor and 28. Electric Lavatory Heater Exercise classmates takes place via threaded discussion and e-mail. The course notebook is for participants only and not for sale. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 40 Orlando Software Safety, Certification and DO-178B I nstructor: Leanna Rierson

O rlando, Florida Daye On Dayr Fou November 16–19, 2010 • Introductions and background • Assessing compliance to DO-178B—the AA111280 • Overview of existing standards related to Software Job-Aid software safety • Common pitfalls in applying DO-178B Tuesday–Friday 8 a.m.–4 p.m. • Tie between the system, safety and • Software challenges facing the aviation Class time 28 hrs. software processes industry: object-oriented technology, CEUs 2.8 • History, purpose, framework and layout of off-shore development, model- DO-178B based development, increased use of Description verification and development tools, use • Reading the DO-178B Annex A Tables Provides the fundamentals of of real-time operating systems and other developing and assessing software • DO-178B planning process commercially available components, software reuse to the standard RTCA/DO-178B • DO-178B development and integration/ Software Considerations in Airborne test processes—development objectives, • Summary Systems and Equipment Certification. high-level requirements, traceability, Also provides insight into the FAA’s design (low-level requirements How You May Benefit software review process, the FAA’s and architecture), code/integration, software policy, practical keys for integration/test objectives, normal and • Gain valuable insight into the software successful software development robustness testing development and certification processes. and certification, common pitfalls of • Obtain practical keys for developing software development, and software and assessing software to meet the civil challenges facing the aviation Dayo Tw aviation standard: RTCA/DO-178B. community. Practical exercises and • DO-178B verification processes— in-class activities will be used to overview of verification, verification of • Understand the importance of software enhance the learning process. requirements, design, code and testing assurance and its tie to the system safety assessment and the system development • DO-178B configuration management, processes. T arget Audience quality assurance, and certification liaison Designed for software developers, processes—configuration management • Learn the common pitfalls in applying avionics engineers, systems objectives and terminology, control DO-178B and obtaining certification and integrators, aircraft designers and categories, quality assurance (QA) ideas for how to proactively address others involved in development or objectives, DO-178B QA philosophy, those issues. implementation of safety-critical SQA approaches, certification liaison • Understand the FAA’s software-related software. The focus is on civil aviation, objectives, DO-178B life cycle data policy and guidance. certification, and use of RTCA/DO- • Special topics related to DO-178B— • Learn about the software challenges 178B; however, the concepts may be partitioning and protection, structural facing the aviation industry. applicable for other safety domains, coverage, dead and deactivated code, such as military, medical, nuclear and service history, Commercial-Off-The-Shelf automotive. (COTS) software F ee $1,995 Day Three Includes instruction, a course notebook, the RTCA/DO-178B Software • FAA software-related policy and Considerations in Airborne Systems and guidance—software review process, Equipment Certification handbook, user-modifiable and field-loadable refreshments and four lunches. software, change impact analysis, tool qualification, previously developed The course notebook is for software, software reuse, integrated participants only and not for sale. modular avionics, databases (DO-200A), complex hardware (DO-254)

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 San Diego 41 Structural Composites I nstructor: Max Kismarton, Richard Hale and Mark Ewing This course may be taught by one or a combination of instructors.

Daye On Dayr Fou S an Diego, California • Introduction/historical review • Global design considerations September 13–17, 2010 • Materials behavior and selection • Hygrothermal effects AA111060 • Fibers, matrix materials, other composite • Interlaminar and free-edge effects Monday–Friday 8 a.m.–4 p.m. materials • Laminate failure theories Class time 35 hrs. • Manufacturing introduction • Design problems, stress analysis, multi- CEUs 3.5 ply failure Dayo Tw • Family optimization Description • Manufacturing for varied products: flat The course provides an and curved parts, longitudinals, sandwich Day Five understanding of available fiber panels and cylinders and matrix materials, manufacturing • Joints • Tooling design methods and the mechanical • Ply definition in 3-D space behavior of composite materials for • Cost the design of airframe structures. • Modern software tools The course topics include: material Day Three • Manufacturability and quality assurance behavior, selection and cost; general • Fatigue damage mechanisms anisotropic theory, elastic behavior • Lamina micromechanics, failure modes and stiffness matrix formulation; • Short fiber composites • Damage tolerance, environmental effects computer-aided analysis; strength and reparability • Lamina macromechanics, failure theories and theory of failure; fatigue and • Nondestructive evaluation damage tolerance assessment; and • Laminate macromechanics repairability. • Summary and wrap-up • Analysis examples • Anisotropic elasticity T arget Audience Designed for practicing design and • Classical lamination theory structural engineers, educators and engineering managers whose responsibilities include aircraft structures.

F ee $2,295 Includes instruction, a course notebook, Composite Airframe Structures, by Michael Niu, refreshments and five lunches. The course notebook is for participants only and not for sale.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 42 Instructor Bios Instructor Biographies Instructors whose biographies appear on the following pages are scheduled to teach public courses in 2010. For a complete listing of all our outstanding instructors, please go to www.ContinuingEd.ku.edu/aero/instructors.php.

Mario Asselin Brian Butka Mario Asselin is currently chairman of Asselin, Inc., Brian Butka is an associate professor of electrical and systems a company that provides engineering services in engineering at the Embry-Riddle Aeronautical University performance, stability and control. He is also senior manager in Daytona, Florida. He has more than 12 years of analog/ aerodynamics with Honda Aircraft Corporation where mixed signal and VLSI circuit design experience at Integrated he supervises flight sciences, flight testing, simulator and Device Technology, where he was a principal engineer. interiors activities. He is an FAA Flight Analyst DER. Prior to that, he was an assistant professor for six years at Asselin previously held positions as vice president engineering the United States Naval Academy, where he was honored with Sino Swearingen Aircraft Corporation, Learjet’s chief as the Best Teacher in Electrical Engineering in 1994. He has of stability and control at the Bombardier Flight Test Center also served as an adjunct professor at Georgia Institute of in Wichita, chief technical for the aerodynamic design and Technology. Earlier, he was a process design engineer at certification of Bombardier’s CRJ-900 and Transport Canada Westinghouse Electric Corporation and a product engineer DAD. He has taught courses for the Royal Military College of at Texas Instruments. His research areas include electrostatic Canada, McGill University and Concordia University in Montreal. discharge protection circuits for GHz I/Os, characterization He is the author of An Introduction to Aircraft Performance. and test of parts with GHz I/Os using embedded systems, and self-characterizing/testing circuits, multi-GHz serial Asselin holds a B.E. degree in mechanical engineering from communication systems, and power integrity optimization. the Royal Military College of Canada and an M.Sc.A. degree in aerothermodynamics from École Polytechnique of Montreal. Butka has a B.S. in electrical engineering from Syracuse University and an M.S. and Ph.D. in electrical engineering, both from Georgia Institute of Technology. N eil Bloom Neil Bloom is the author of Reliability Centered Maintenance A rmand Chaput (RCM) — Implementation Made Simple. Bloom has more than 35 years of both hands-on and senior-level Armand Chaput is an adjunct professor in aerospace managerial engineering and maintenance experience engineering and engineering mechanics at the University in the commercial aviation and commercial nuclear of Texas–Austin where he teaches unmanned aircraft power industries, with close association with the FAA system design and serves as director of the Aircraft and the Nuclear Regulatory Commission (NRC). System Design and Integration Laboratory. He is retired from Lockheed Martin Aeronautics Company, where His career in the airline industry included positions in he was a Senior Technical Fellow and member of the engineering and preventive maintenance programs, as Air System Design and Integration technical staff. superintendent of aircraft maintenance, and assistant to the vice president of maintenance. He was a member of While at Lockheed Martin Aeronautics he supported a the maintenance review board for the Lockheed L1011 and range of advanced technology programs, most recently as worked with MSG Logic, which was the forerunner to RCM. Weight Czar and Chief Weight Control Engineer for the F-35 Joint Strike Fighter Program. He has served as member of Bloom’s career within nuclear power included engineering and the USAF Scientific Advisory Board, the Naval Studies Board maintenance management. He held management positions of the National Academy and the board of trustees for the in maintenance engineering, maintenance procedures and Association for Unmanned Vehicle Systems International. regulatory policies, and for 14 years, he was the program manager for RCM and preventive maintenance programs. He is the 2003 recipient of the SAE Clarence L. “Kelly” Johnson Aerospace Vehicle Design and Development Award. He is a Bloom has written articles for Maintenance Technology, Uptime Fellow of the AIAA, an instrument rated commercial pilot and and Reliability magazines. He has been a guest speaker on flight instructor. the topic of RCM at some of the most prestigious national and international conferences such as the Electric Power Chaput holds a B.S., M.S. and Ph.D. from Texas A&M University, Research Institute (EPRI), the American Society of Mechanical all in aerospace engineering. Engineers (ASME), the American Nuclear Society (ANS) and the International Atomic Energy Agency (IAEA) in Vienna, Austria. Bloom received a B.S. in mechanical engineering from the University of Miami. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 43

David R. Downing has 45 years of experience in various areas of engineering, including communications, navigation, precision testing and David Downing is a professor emeritus of aerospace measurement, radar and security systems. He performed engineering at the University of Kansas. He teaches courses radiation hardening on military avionics, designed test and does research in advanced flight control, instrumentation equipment for the emerging cable television industry, general systems and flight testing. Downing was formerly an aerospace aviation avionics for Cessna Aircraft, and precision parameter engineer at NASA Langley Research Center, a systems engineer measuring and magnetics systems for Dowty Industries. at the NASA Electronics Research Center, and an assistant professor of systems engineering at Boston University. He Helfrick is the author of 12 books, numerous contributions received a B.S.E. degree in aerospace engineering and an M.S.E. to encyclopedias, handbooks and other collections. He degree in instrumentation engineering from the University of has more than 100 technical papers and presentations, Michigan. He also earned an S.C.D. degree in instrumentation served as an expert witness in a number of civil cases and engineering from the Massachusetts Institute of Technology. has testified before Congress. He holds four U.S. patents, is a registered professional engineer in New Jersey, a senior member of the IEEE and an Associate Fellow of the AIAA. Mark S. Ewing He holds a B.S. in physics from Upsala College, an M.S. in Mark Ewing is chairman of the Aerospace Engineering mathematics from New Jersey Institute of Technology Department and director of the flight research laboratory and a Ph.D. in applied science from Clayton University. at the University of Kansas. Previously, he served as a senior research engineer in the structures division at Wright Laboratory, Wright-Patterson Air Force Base, and as an associate Wally Johnson professor of engineering mechanics at the U.S. Air Force Wally Johnson is a senior loads engineer at Boeing IDS in Academy. His research interests include structural vibrations Wichita. His responsibilities include design, fatigue, static and structural acoustics, especially carbon fiber-reinforced and dynamic loads analysis. Johnson has 20 years of loads composites. Ewing is a past recipient of the University of experience. Previously, he served as a technical specialist Kansas School of Engineering Outstanding Educator Award. and an FAA DER at Raytheon Aircraft Company. He was the He holds a B.S. degree in engineering mechanics lead static engineer on the Hawker 4000 business jet. He has from the U.S. Air Force Academy, an M.S. degree in served as a member of the Aviation Rulemaking Advisory mechanical engineering and a Ph.D. in engineering Committee group working to harmonize the FARs and JARs mechanics, both from Ohio State University. in the area of loads and dynamics. Johnson also has worked as a senior loads engineer at Learjet. Johnson is a FAR 23/25 consultant Loads DER. He holds B.S. and M.S. degrees in Bill Goodwine aerospace engineering from Wichita State University. Bill Goodwine is an associate professor in the Department of Aerospace and Mechanical Engineering at the University of Marge Jones Notre Dame. His research and teaching focus is on nonlinear control and dynamical systems, with particular emphasis Marge Jones is a system safety consultant specializing in on geometric methods and hybrid systems. He received commercial aircraft certification and has been involved in a his M.S. and Ph.D. degrees from the California Institute of variety of STC and TC projects. She has been a federal aviation Technology. He was the recipient of a National Science administration designated engineering representative for Foundation CAREER award and numerous departmental, structures, power plant, and systems and equipment for the past college, university and ASEE teaching awards. 18 years. She is also a certified safety professional in system safety from the Board of Certified Safety Professionals and has several years of safety engineering experience with defense systems A lbert Helfrick and NASA payloads. Jones provides safety consultant/product safety services to aircraft and defense industries. Her area of Albert Helfrick is currently the chair of the Electrical and safety consultation includes performing safety analyses, defining Systems Engineering Department at Embry-Riddle Aeronautical system architecture and safety requirements, developing University. design solutions to safety-related issues, and evaluating and/ Previously, he was director of engineering for Tel-Instrument or preparing certification documentation for regulations Electronics, a manufacturer of avionics test equipment. compliance. Before entering academia, he was a self-employed consulting She holds a B.S. degree in safety engineering from Texas A&M engineer for four years where he and his company designed University and an M.S. degree in systems management from fire and security systems, consumer items and avionics. He Florida Institute of Technology.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 44 Instructor Bios

Max Kismarton S teven L. Morris Max Kismarton is an aircraft designer and a Technical Fellow at Steven L. Morris is a senior consultant for Engineering Systems, The Boeing Company, with extensive hands-on experience in Inc., Colorado Springs, Colorado. Morris served as an officer engineering (design, loads, stress, weights, testing, advanced and engineer in the U.S. Air Force for more than 24 years. His metals and composites), manufacturing (tooling, processes, experience includes teaching, research and consulting in the machinery, shop management) and management (cost areas of airplane design, stability and control, aerodynamics, engineering and estimating, lean manufacturing, project/ flight simulation, aircraft icing and accident reconstruction. program management). He is a co-author of Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical He is currently working in the materials and processes group, Feedback Control. He is an Associate Fellow of AIAA. He is also heading up multiple research and development projects on a member of the SAE Aircraft Icing Technology Committee. micromechanical behavior and hybrid laminates and high He received a B.S. in engineering sciences from the U. S. performance wing box structures for present and future Air Force Academy, an M.S. in aeronautical engineering commercial aircrafts. from the Air Force Institute of Technology, and a Ph.D. in Over the last 25 years, he has designed and built composite aerospace engineering from Texas A&M University. airframe primary structure for small and large composite aircrafts such as Amber, Gnat, High Speed Civil Transport, F-16XL-2, Shadow, ERAST, Hummingbird, UCAV X-45 and the 787 Mike Phillips Dreamliner. Mike Phillips is the CMMI Program Manager at the Software Kismarton holds a B.S. in aerospace engineering from the Engineering Institute, a federally funded research and University of Kansas. development center sponsored by the U.S. Department of Defense and operated by Carnegie Mellon University. He led a team that created the CMMI Product Suite which Michael Mohaghegh successfully demonstrates key practices for both systems and software engineering. He is the co-author of an Michael Mohaghegh is a Boeing Technical Fellow in advanced Addison-Wesley book, CMMI-ACQ: Guidelines for Improving structures and materials, with 40 years of experience in the Acquisition of Products and Services. As an Air Force designing and analyzing aircraft (707, 737, 747, B1, 767, 777, 787, senior officer, Phillips led an Air Force program office’s 747-8) and developing technology and design standards. He development and acquisition of the software-intensive B-2 is the developer and instructor for courses on static strength, Spirit stealth bomber using integrated product teams. design and analysis, finite element, and fatigue, fracture and composites at The Boeing Company. Mohaghegh is He holds a B.S. degree in astronautical engineering from also an affiliate professor of aeronautics and astronautics the U.S. Air Force Academy, an M.S. degree in nuclear and is the director of the Modern Aircraft Structures engineering from Georgia Tech, an M.S. degree in Certificate Program at the University of Washington. systems management from the University of Southern California, an M.A. degree in international affairs from Salve He also has taught classes for airlines, suppliers and universities Regina College and an M.A. degree in national security in the U.S. and abroad. Previously, he held the positions and strategic studies from the Naval War College. of principal lead engineer and FAA DER for the Boeing Commercial Airplane Group. Mohaghegh has published in the Journal of Applied Mechanics, Journal of Aircraft, International Journal of Technical Sciences, International Journal of Mechanical E verett W. Pittman Engineering Education, and the Boeing AERO magazine. Everett Pittman is a private consultant in aircraft certification. He received his B.S. and M.S. degrees in structural engineering He retired from the FAA with more than 35 years of domestic from the University of California, Berkeley, and his Ph.D. in and international aircraft certification experience, most recently engineering mechanics from the University of Washington. as manager of the Wichita Aircraft Certification Office. He also has served as a flight test engineer, airframe engineer, project manager, manager of the Regulatory Review Branch in Washington, D.C., the International Aircraft Certification Specialist in Washington, D.C., and manager of the Europe, Africa, and Middle East Aircraft Certification Office in Brussels, Belgium. He helped develop new bilateral airworthiness agreements with Canada, Argentina, South Africa, and Indonesia, and helped develop the FAA Part 21 training course. Pittman received a B.S. degree in aerospace engineering from Parks College of St. Louis University.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 45

Donald Plouffe Jan Roskam Donald Plouffe is an independent consultant operating as Jan Roskam is the Emeritus Ackers Distinguished Professor J and J Aero LLC, providing manufacturing, airworthiness, of Aerospace Engineering at the University of Kansas. conformity and consulting services to the aviation industry. His university honors include the 2003 Chancellors Club He is a Designated Airworthiness Representative. Career Teaching Award and five-time winner of Aerospace Engineering Educator of the Year, selected by graduating Formerly, Plouffe was an FAA Manufacturing Inspection Office seniors. In October 2007, Dr. Roskam received the prestigious Manager for the Aircraft Certification Service, New England AIAA Aircraft Design Award, and in 2008 the Lifetime Engine and Propeller Directorate in Burlington, Massachusetts. Achievement Award, also from AIAA. The author of 15 Plouffe has 30 years of experience in the aviation industry in textbooks, Roskam has had industrial experience with three type certification, production certification and airworthiness major aircraft companies and has been actively involved in the certification, first article, in process, and final assembly design and development of more than 50 aircraft programs. He inspections; quality assurance provisions of special processes is a Fellow of AIAA and the Society of Automotive Engineers. (heat treating, brazing, welding, carbonizing, plating); Roskam received an M.S. degree in aeronautical engineering destructive and nondestructive inspections, manufacturing from the Delft University of Technology, The Netherlands, and processes, airworthiness assurance, developing and a Ph.D. in aeronautics and astronautics from the University of implementing quality control systems and procedures, Washington. testing procedures, and use of FAA-approved design data. He holds a B.S. degree in management from University of Rhode Island. Wayne R. Sand Wayne R. Sand is an aviation weather consultant with R ay Prouty expertise in aircraft icing tests, analysis of icing accidents and development of icing instrumentation. He also has Ray Prouty is a private consultant for the helicopter industry extensive expertise in convective weather, winter weather and with more than 50 years of experience. He began his career mountain weather. As former deputy director of the Research at Hughes Tool Company and later at Sikorsky Aircraft as Applications Program at the National Center for Atmospheric a helicopter aerodynamicist. Other positions he has held Research, he developed aviation weather technology for include: stability and control specialist, Bell Helicopters; group the FAA. Previously, Sand was a member of the Atmospheric engineer-helicopter aerodynamics, Lockheed Aircraft; and Science Department at the University of Wyoming. He also chief, stability and control, Hughes Helicopters/McDonnell conducted research on thunderstorms and convective icing Douglas Helicopters. The author of the Aerodynamics column while at the South Dakota School of Mines and Technology. of Rotor and Wing magazine for more than 20 years, Prouty Sand is co-holder of a patent on a technique for the remote also wrote Helicopter Performance, Stability, and Control, a detection of aircraft icing conditions. He holds a B.S. degree college textbook. He is an Honorary Fellow of the American in mathematics and physical science from Montana State Helicopter Society. Prouty holds B.S. and M.S. degrees in University, an M.S. degree in meteorology from the South aeronautical engineering from the University of Washington. Dakota School of Mines and Technology, and a Ph.D. in atmospheric science from the University of Wyoming.

Leanna Rierson David L. Stanislaw Leanna Rierson is an independent consultant in software and complex electronic hardware development for safety-critical David Stanislaw is an independent consultant in avionics systems, with emphasis on civil aviation. She has more than with emphasis on civil aviation. He held engineering 20 years of experience in the software and aviation industry. assignments in airborne systems design and later assumed Rierson spent nine years as a software and avionics specialist responsibility for avionics and electrical engineering at at the Federal Aviation Administration; five of those years the airframe level. Stanislaw was an FAA DER for more were as Chief Scientific and Technical Advisor for Aircraft than 15 years, and has conducted seminars on all phases Computer Software. Rierson has also held engineering of aircraft electronics. The holder of several radar patents, positions at NCR and Cessna Aircraft Company. She served Stanislaw was a member of RTCA and has participated in on all of the teams that developed the following IMA-related international symposiums. He held a commercial pilot rating. material: TSO-C153, AC 20-145, and RTCA/DO-297. Leanna is also an FAA Designated Engineering Representative (DER) Stanislaw received a B.S. degree in electron physics from LaSalle with authority in both software and complex electronic College. hardware and has worked on several IMA projects. She has a master’s degree in software engineering from Rochester Institute of Technology and a bachelor’s degree in electrical engineering from Wichita State University. www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 46 Instructor Bios

Wayne Stout Herb Tuttle Wayne Stout is an independent consultant with a technical Herb Tuttle has been an assistant professor and the director specialization in design, analysis, simulation and certification of the engineering management graduate program at the of aircraft mechanical systems. Stout has more than 20 years University of Kansas Edwards Campus for the past 15 years. of experience in aircraft mechanical systems at Bombardier In his previous 20 years of professional practice, he was a Aerospace–Learjet, The Boeing Company and Honeywell. He management consultant, project manager, project engineer has held positions of engineering specialist, systems integrator and manufacturing manager with various Fortune 500 and chief engineer. His experience covers all design phases companies. He received undergraduate degrees in electrical from concept to final product across commercial, military and industrial engineering from the State University of New and space products. In addition, Stout has been an adjunct York at Alfred and Buffalo, an M.B.A. from the University professor at Wichita State University and is a FAA DER in flight of Kansas, an M.S. degree in engineering management controls, hydraulics, ECS, pressurization and door mechanisms. from the University of Tennessee, and an M.S. degree in industrial engineering from Illinois State University. He Stout received a B.S. degree in mechanical engineering from is currently working on his dissertation, The Relationship the South Dakota School of Mines and Technology, an M.S. between Team Success and Team Virtuality of Technical Teams, degree in aeronautical engineering and a Ph.D. in engineering, in the industrial and systems engineering/engineering both from Wichita State University. program at the University of Alabama in Huntsville.

T homas William Strganac C.P. (Case) van Dam Thomas W. Strganac is a professor of aerospace engineering at Texas A&M University. His research and engineering activities C.P. (Case) van Dam is a professor of aeronautical engineering focus on aeroelastic phenomena, structural dynamics, fluid- at the University of California Davis, where he teaches in the structure interaction, limit cycle oscillations, and related Department of Mechanical and Aeronautical Engineering and nonlinear mechanics. From 1975 to 1989, Strganac was a heads the California Wind Energy Collaborative—a partnership research engineer at NASA’s Langley Research Center and an between the University of California and the California Energy aerospace engineer at NASA’s Goddard Flight Space Center. He Commission. is an Associate Fellow of the AIAA and a registered professional Previously, he was a National Research Council postdoctoral engineer. researcher at the NASA Langley Research Center and a research Strganac received a B.S. degree from North Carolina State engineer at Vigyan Research Associates, Inc. Van Dam’s current University and an M.S. degree from Texas A&M University, research includes wind energy engineering, aerodynamic both in aerospace engineering, and a Ph.D. in engineering drag prediction and reduction, high-lift aerodynamics mechanics from Virginia Tech. and active control of aerodynamic loads. He has extensive experience in computational aerodynamics, wind-tunnel experimentation and flight testing; has consulted for aircraft, Gilbert L. Thompson wind energy, and sailing yacht manufacturers; and has served on review committees for government agencies and research Gilbert L. Thompson is a private consultant in aircraft organizations. He is a past recipient of the AIAA Lawrence certification. He has more than 32 years of experience in Sperry Award, a U.S. Department of Energy Award and several domestic and international aircraft certification with the FAA. NASA awards. He also has served as a systems engineer; project manager; Van Dam received B.S. and M.S. degrees from the Delft manager for the systems and equipment branch, Los Angeles University of Technology, The Netherlands, and M.S. and Aircraft Certification Office; and assistant manager, Transport D.E. degrees from the University of Kansas, all in aerospace Airplane Directorate. Certification experience includes the engineering. Robinson R22/R44 Rotorcraft, Lockheed L1011, McDonnell Douglas DC-8, DC-9, DC-10, MD-80, MD-90, KC-10A, MD- 11, MDHI 369/500NOTAR, MDHI 600, MDHI 900, the first concurrent and cooperative joint FAA/Joint Aviation Authorities certification of the Boeing 717-200 and development of the criteria for civil certification of the military Globemaster C-17. In 1999, he was the recipient of the Aviation Week and Space Technology Laurels Award for outstanding achievement in the field of aeronautics/propulsion. Thompson holds a B.S. degree in aerospace engineering from the University of Michigan and a B.A. degree in mathematics from Bellarmine University, Louisville, Kentucky.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Instructor Bios 47

Paul Vijgen Mark K. Wilson Paul s Vijgen i an Associate Technical Fellow in aerodynamics Mark K. Wilson, an internationally recognized authority engineering at Boeing Commercial Airplanes in Seattle. He in systems engineering and president of Mark Wilson currently supports the development of commercial aircraft, Consulting, is a systems engineering and aerospace including implementation of aerodynamic fuel-burn reduction consultant with more than 40 years of systems engineering technologies. While at Boeing and at NASA Langley, he has acquisition experience. He is a director and chief been involved over the past 25 years with application studies operating officer of Aerospace Technologies Associates, and flight tests of laminar-flow control over wings, fuselages and LLC, and an associate with Dayton Aerospace, Inc. nacelles. Other flight research includes transport high-lift flows, Wilson, a member of the senior executive service, completed wake-vortex development and supersonic turbulent flows. his Air Force career as director of the Air Force Center for Vijgen received an M.S. degree from the Delft University of Systems Engineering, Air Force Institute of Technology Technology, The Netherlands, and a D.E. degree from the (AFIT), Wright Patterson Air Force Base, Ohio. He served University of Kansas, both in aerospace engineering. as the technical advisor for systems engineering at the Aeronautical Systems Center and as technical director in the headquarters of Air Force Material Command (AFMC), Ken Vranish Directorate of Engineering and Technical Management. He was director of engineering in the C-17 System Program Ken Vranish is an independent consultant and president of KVA Office at the Aeronautical Systems Center, where he directed Engineering, Inc. He has 30 years of experience in the hardware all aspects of systems engineering necessary to develop, and software design and certification of avionics equipment produce and sustain the C-17 Weapon System. He also and other safety critical systems used on commercial and worked on numerous weapon systems, including the B-2 military aircraft. Vranish worked 10 years at Boeing in the bomber and the F-15 fighter. His first assignment was as development of autopilot systems. In 1987, he started his own a structural engineer in the F-15 A/B Program Office. consulting company and in the years since has worked on many aircraft systems, participated in aircraft incident reviews, Wilson is a Sloan Fellow. He earned his B.S. in aerospace and conducted research with various industry groups on engineering from Purdue University and holds an M.S. specialized topics pertaining to aircraft operation, including the in management from Stanford University and an M.S. in Effects of Atmospheric Radiation on Electronic Components. management science from the University of Dayton. Vranish is considered an industry expert on how radiation impacts the aircraft operational environment. Vranish holds a B.S. degree in electrical engineering from Montana State University-Bozeman.

Donald T. Ward Donald T. Ward is a professor emeritus of aerospace engineering at Texas A&M University and a former director of its flight mechanics laboratory. Previously, he served 23 years as an officer in the United States Air Force, retiring as a colonel. His last military assignment was as wing commander of the 4950th 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. degree in aeronautical engineering from the University of Texas, an M.S. degree in astronautics from the Air Force Institute of Technology, and a Ph.D. in aerospace engineering from Mississippi State University.

www.ContinuingEd.ku.edu/aero Tel. 785-864-5823, or toll-free 877-404-5823 Mailroom: Please reroute to replacement or Training Director

KU Continuing Education Aerospace Short Course Program 1515 Saint Andrews Drive Lawrence, KS 66047-1619 USA

Please leave mailing panel attached.

www.ContinuingEd.ku.edu/aero Toll-free in the U.S.: 877-404-5823 or 785-864-5823 2010 University of Kansas reg istration form 1 If your mailing address requires a different format than indicated here, please use that format and ignore the printed guidelines. First name, middle initial Last name or surname Telephone number

Position o Male o Female Fax number

Company or organization E-mail address

o I cannot attend this year, but please add me to your mailing list. Mail stop, building or room number (if needed) Preregistration is required. Street address or post office box o home o work o Special Accommodation City, state or province Zip+four or postal code If you will need special accommodation, please mark the box above, and a member of the Continuing Education staff will contact you. 100037 Country

My priority code (located above your name on the mailing panel above): ______2 Please register me for the following course(s):

Course Name Course # Dates Location

Course Name Course # Dates Location Payment Preferred means of communication Please continue to send information by (check all that apply): 3 o Check enclosed, payable in U.S. dollars to The University of Kansas. o Mail o E-mail o Fax o Please remove my name from the mailing list. o Bill company: If purchase order number is required on invoice, please provide it. Please bring a copy of purchase order or letter of authorization to check-in on the first day of How did you first hear about our short courses? the course. PO#______o Referral o KU brochure o Magazine ad o Web site o Article or listing o E-mail Billing address if different from above: ______

______Easy Ways to Register Mail Complete the registration form and mail with payment to: o Charge to: credit card company______KU Continuing Education Aerospace Short Courses 1515 Saint Andrews Drive Amount______Lawrence, Kansas 66047-1619 USA Card #______Exp.______Phone Toll-free 877-404-5823 or 785-864-5823 Name on card (print)______Fax 785-864-4871 E-mail [email protected] • Web www.ContinuingEd.ku.edu/aero Cardholder’s phone number______