The Wright Brothers' Adventure
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Modeling an Airframe Tutorial
EAA SOLIDWORKS University p 1/11 Modeling an Airframe Tutorial Difficulty: Intermediate | Time: 1 hour As an Intermediate Tutorial, it is assumed that you have completed the Quick Start Tutorial and know how to sketch in 2D and 3D. If you struggle to recall how to do basic functions, please review the Tips Sheet. The Modeling an Airframe Tutorial guides you through the creation of a tubular airframe in SOLIDWORKS. The objective of the lesson is to teach you how to use the tools to design an aircraft frame. Time limits prevent us from completing this airframe, but you should learn the skills to model an airframe. You will create this part and drawing: This lesson includes: Creating a 3D Sketches Using the Weldment feature to add structural members Trimming structural members Creating a drawing and adding a ‘cut list’ Bill of Materials (BoM) EAA SOLIDWORKS University p 2/11 Modeling an Airframe Tutorial Creating a 3D Sketch for the Airframe In this lesson we will use the weldment feature to create an airframe. Weldments are structural members defined by a cross section picked from a library and a sketch line to define its length. This sketch line can be from multiple 2D sketches, or a single 3D sketch. By using two layout sketches (side and plan elevations), you can control the 3D sketch easily and any future changes will be reflected in your airframe. The layout sketches capture the design intent and the dimensions of the finished frame. 1. Open a New Part, verify Units are inches, and Save As “Airframe” (Top Menu / File / Save As). -
Foo Fighters ‘All My Life’
Tracks Foo Fighters ‘All My Life’ Foo Fighters SONG TITLE: ALL MY LIFE ALBUM: ONE BY ONE RELEASED: 2002 LABEL: RCA GENRE: ROCK PERSONNEL: DAVE GROHL (GTR + VOX) CHRIS SHIFLET (GTR) NATE MENDEL (BASS) TAYLOR HAWKINS (DRUMS) UK CHART PEAK: 1 US CHART PEAK: 43 BACKGROUND INFO NOTES ‘All My Life’ is the last single off the Grammy Texan Taylor Hawkins started his career as a Award winning Foo Fighters’ album One by One. drummer-for-hire and before landing the Foo This driving rock performance comes courtesy of Fighters’ gig was, amongst other things, the touring drummer Taylor Hawkins. The track starts with 30 drummer for Alanis Morissette in her Jagged Little seconds of Dave Grohl singing and playing solo guitar Pill period. Grohl originally contacted Hawkins before the rest of the band comes in at breakneck for advice on the best person to fill the drum slot in speed. The drum groove features displaced snare 1997 and was surprised to hear that he was willing hits and other syncopations that give the verses a see- to do the job himself. Hawkins professes himself to saw sense of motion. By contrast, the choruses are be a big fan of Queen’s Roger Taylor and played with straight-ahead rock. him at Live Earth in 2007 along with Chad Smith of the Red Hot Chili Peppers. He also toured as Brian May’s drummer. At one point when the Foo Fighters THE BIGGER PICTURE supported May, he played both the support and headline slots! This album heralds the start of a period of rejuvenation for the Foo Fighters. -
Unit-1 Notes Faculty Name
SCHOOL OF AERONAUTICS (NEEMRANA) UNIT-1 NOTES FACULTY NAME: D.SUKUMAR CLASS: B.Tech AERONAUTICAL SUBJECT CODE: 7AN6.3 SEMESTER: VII SUBJECT NAME: MAINTENANCE OF AIRFRAME AND SYSTEMS DESIGN AIRFRAME CONSTRUCTION: Various types of structures in airframe construction, tubular, braced monocoque, semimoncoque, etc. longerons, stringers, formers, bulkhead, spars and ribs, honeycomb construction. Introduction: An aircraft is a device that is used for, or is intended to be used for, flight in the air. Major categories of aircraft are airplane, rotorcraft, glider, and lighter-than-air vehicles. Each of these may be divided further by major distinguishing features of the aircraft, such as airships and balloons. Both are lighter-than-air aircraft but have differentiating features and are operated differently. The concentration of this handbook is on the airframe of aircraft; specifically, the fuselage, booms, nacelles, cowlings, fairings, airfoil surfaces, and landing gear. Also included are the various accessories and controls that accompany these structures. Note that the rotors of a helicopter are considered part of the airframe since they are actually rotating wings. By contrast, propellers and rotating airfoils of an engine on an airplane are not considered part of the airframe. The most common aircraft is the fixed-wing aircraft. As the name implies, the wings on this type of flying machine are attached to the fuselage and are not intended to move independently in a fashion that results in the creation of lift. One, two, or three sets of wings have all been successfully utilized. Rotary-wing aircraft such as helicopters are also widespread. This handbook discusses features and maintenance aspects common to both fixed wing and rotary-wing categories of aircraft. -
Evaluation and Flight Assessment of a Scale Glider
Dissertations and Theses 8-2014 Evaluation and Flight Assessment of a Scale Glider Alvydas Anthony Civinskas Embry-Riddle Aeronautical University - Daytona Beach Follow this and additional works at: https://commons.erau.edu/edt Part of the Aerospace Engineering Commons Scholarly Commons Citation Civinskas, Alvydas Anthony, "Evaluation and Flight Assessment of a Scale Glider" (2014). Dissertations and Theses. 41. https://commons.erau.edu/edt/41 This Thesis - Open Access is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Dissertations and Theses by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Evaluation and Flight Assessment of a Scale Glider by Alvydas Anthony Civinskas A Thesis Submitted to the College of Engineering Department of Aerospace Engineering in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering Embry-Riddle Aeronautical University Daytona Beach, Florida August 2014 Acknowledgements The first person I would like to thank is my committee chair Dr. William Engblom for all the help, guidance, energy, and time he put into helping me. I would also like to thank Dr. Hever Moncayo for giving up his time, patience, and knowledge about flight dynamics and testing. Without them, this project would not have materialized nor survived the many bumps in the road. Secondly, I would like to thank the RC pilot Daniel Harrison for his time and effort in taking up the risky and stressful work of piloting. Individuals like Jordan Beckwith and Travis Billette cannot be forgotten for their numerous contributions in getting the motor test stand made and helping in creating the air data boom pod so that test data. -
Ai2019-2 Aircraft Serious Incident Investigation Report
AI2019-2 AIRCRAFT SERIOUS INCIDENT INVESTIGATION REPORT ACADEMIC CORPORATE BODY JAPAN AVIATION ACADEMY J A 2 4 5 1 March 28, 2019 The objective of the investigation conducted by the Japan Transport Safety Board in accordance with the Act for Establishment of the Japan Transport Safety Board and with Annex 13 to the Convention on International Civil Aviation is to prevent future accidents and incidents. It is not the purpose of the investigation to apportion blame or liability. Kazuhiro Nakahashi Chairman Japan Transport Safety Board Note: This report is a translation of the Japanese original investigation report. The text in Japanese shall prevail in the interpretation of the report. AIRCRAFT SERIOUS INCIDENT INVESTIGATION REPORT INABILITY TO OPERATE DUE TO DAMAGE TO LANDING GEAR DURING FORCED LANDING ON A GRASSY FIELD ABOUT 3 KM SOUTHWEST OF NOTO AIRPORT, JAPAN AT ABOUT 15:00 JST, SEPTEMBER 26, 2018 ACADEMIC CORPORATE BODY JAPAN AVIATION ACADEMY VALENTIN TAIFUN 17EII (MOTOR GLIDER: TWO SEATER), JA2451 February 22, 2019 Adopted by the Japan Transport Safety Board Chairman Kazuhiro Nakahashi Member Toru Miyashita Member Toshiyuki Ishikawa Member Yuichi Marui Member Keiji Tanaka Member Miwa Nakanishi 1. PROCESS AND PROGRESS OF THE INVESTIGATION 1.1 Summary of On Wednesday, September 26, 2018, a Valentin Taifun 17EII (motor the Serious glider), registered JA2451, owned by Japan Aviation Academy, took off from Incident Noto Airport in order to make a test flight before the airworthiness inspection. During the flight, as causing trouble in its electric system, the aircraft tried to return to Noto Airport by gliding, but made a forced landing on a grassy field about 3 km short of Noto Airport, and sustained damage to the landing gear, therefore, the operation of the aircraft could not be continued. -
AMA FPG-9 Glider OBJECTIVES – Students Will Learn About the Basics of How Flight Works by Creating a Simple Foam Glider
AEX MARC_Layout 1 1/10/13 3:03 PM Page 18 activity two AMA FPG-9 Glider OBJECTIVES – Students will learn about the basics of how flight works by creating a simple foam glider. – Students will be introduced to concepts about air pressure, drag and how aircraft use control surfaces to climb, turn, and maintain stable flight. Activity Credit: Credit and permission to reprint – The Academy of Model Aeronautics (AMA) and Mr. Jack Reynolds, a volunteer at the National Model Aviation Museum, has graciously given the Civil Air Patrol permission to reprint the FPG-9 model plan and instructions here. More activities and suggestions for classroom use of model aircraft can be found by contacting the Academy of Model Aeronautics Education Committee at their website, buildandfly.com. MATERIALS • FPG-9 pattern • 9” foam plate • Scissors • Clear tape • Ink pen • Penny 18 AEX MARC_Layout 1 1/10/13 3:03 PM Page 19 BACKGROUND Control surfaces on an airplane help determine the movement of the airplane. The FPG-9 glider demonstrates how the elevons and the rudder work. Elevons are aircraft control surfaces that combine the functions of the elevator (used for pitch control) and the aileron (used for roll control). Thus, elevons at the wing trailing edge are used for pitch and roll control. They are frequently used on tailless aircraft such as flying wings. The rudder is the small moving section at the rear of the vertical stabilizer that is attached to the fixed sections by hinges. Because the rudder moves, it varies the amount of force generated by the tail surface and is used to generate and control the yawing (left and right) motion of the aircraft. -
Federal Aviation Administration, DOT § 61.45
Federal Aviation Administration, DOT Pt. 61 Vmcl Minimum Control Speed—Landing. 61.35 Knowledge test: Prerequisites and Vmu The speed at which the last main passing grades. landing gear leaves the ground. 61.37 Knowledge tests: Cheating or other VR Rotate Speed. unauthorized conduct. VS Stall Speed or minimum speed in the 61.39 Prerequisites for practical tests. stall. 61.41 Flight training received from flight WAT Weight, Altitude, Temperature. instructors not certificated by the FAA. 61.43 Practical tests: General procedures. END QPS REQUIREMENTS 61.45 Practical tests: Required aircraft and equipment. [Doc. No. FAA–2002–12461, 73 FR 26490, May 9, 61.47 Status of an examiner who is author- 2008] ized by the Administrator to conduct practical tests. PART 61—CERTIFICATION: PILOTS, 61.49 Retesting after failure. FLIGHT INSTRUCTORS, AND 61.51 Pilot logbooks. 61.52 Use of aeronautical experience ob- GROUND INSTRUCTORS tained in ultralight vehicles. 61.53 Prohibition on operations during med- SPECIAL FEDERAL AVIATION REGULATION NO. ical deficiency. 73 61.55 Second-in-command qualifications. SPECIAL FEDERAL AVIATION REGULATION NO. 61.56 Flight review. 100–2 61.57 Recent flight experience: Pilot in com- SPECIAL FEDERAL AVIATION REGULATION NO. mand. 118–2 61.58 Pilot-in-command proficiency check: Operation of an aircraft that requires Subpart A—General more than one pilot flight crewmember or is turbojet-powered. Sec. 61.59 Falsification, reproduction, or alter- 61.1 Applicability and definitions. ation of applications, certificates, 61.2 Exercise of Privilege. logbooks, reports, or records. 61.3 Requirement for certificates, ratings, 61.60 Change of address. -
Hangar 9 Ultimate Manual
TM® WE GET PEOPLE FLYING 46% TOC Ultimate 10-300 ASSEMBLY MANUAL Specifications Wingspan ..........................................................................................100 in (2540 mm) Length ................................................................................................110 in (2794 mm) Wing Area.........................................................................................3310 sq in (213.5 sq dm) Weight ...............................................................................................40–44 lb (18–20 kg) Engine.................................................................................................150–200cc gas engine Radio ..................................................................................................6-channel w/15 servos Introduction Thank you for purchasing the Hangar 9® 46% TOC Ultimate. Because size and weight of this model creates a higher degree for potential danger, an added measure of care and responsibility is needed for both building and flying this or any giant-scale model. It’s important that you carefully follow these instructions, especially those regarding hinging and the section on flying. Like all giant-scale aerobatic aircraft, the Hangar 9® TOC Ultimate requires powerful, heavy-duty servos. Servos greatly affect the flight performance, feel and response of the model. To get the most out of your Ultimate, it’s important to use accurate, powerful servos on all control surfaces. In the prototype models, we used JR 8411 digital servos with excellent -
Glider Handbook, Chapter 2: Components and Systems
Chapter 2 Components and Systems Introduction Although gliders come in an array of shapes and sizes, the basic design features of most gliders are fundamentally the same. All gliders conform to the aerodynamic principles that make flight possible. When air flows over the wings of a glider, the wings produce a force called lift that allows the aircraft to stay aloft. Glider wings are designed to produce maximum lift with minimum drag. 2-1 Glider Design With each generation of new materials and development and improvements in aerodynamics, the performance of gliders The earlier gliders were made mainly of wood with metal has increased. One measure of performance is glide ratio. A fastenings, stays, and control cables. Subsequent designs glide ratio of 30:1 means that in smooth air a glider can travel led to a fuselage made of fabric-covered steel tubing forward 30 feet while only losing 1 foot of altitude. Glide glued to wood and fabric wings for lightness and strength. ratio is discussed further in Chapter 5, Glider Performance. New materials, such as carbon fiber, fiberglass, glass reinforced plastic (GRP), and Kevlar® are now being used Due to the critical role that aerodynamic efficiency plays in to developed stronger and lighter gliders. Modern gliders the performance of a glider, gliders often have aerodynamic are usually designed by computer-aided software to increase features seldom found in other aircraft. The wings of a modern performance. The first glider to use fiberglass extensively racing glider have a specially designed low-drag laminar flow was the Akaflieg Stuttgart FS-24 Phönix, which first flew airfoil. -
To Download the Love Ride 32 Brochure (Pdf Format)
HISTORY A caravan of thousands of motorcycles from Harley-Davidson of Glendale, California to a Concert and Festival at Castaic Lake to benet Wounded Warrior Project® (WWP). The mission of Wounded Warrior Project is to honor and empower Wounded Warriors. Grand Marshal Honorary Grand Marshal Honorary Grand Marshal Honorary Chairman Founder and Chairman Jay Leno Peter Fonda Robert Patrick Willie G. Davidson Oliver Shokouh $45 MINIMUM DONATION IN ADVANCE $60 AT THE DOOR LOVERIDE HISTORY In 1984, Oliver Shokouh, the owner of Harley-Davidson of Glendale, decided to embark on a new fundraising endeavor. To succeed, it would have to be a labor of love, and with help from some friends, the LOVE RIDE was born. Peter Fonda agreed to do the rst LOVE RIDE public service announcement. Robbie Kreiger, of the Doors, jumped in and performed at the event. Even Willie G. Davidson himself came out for the ride. On November 11, 1984, over 500 outstanding people showed up, starting a tradition that has grown beyond anyone’s expectation. Over the ensuing 30 years, LOVE RIDE participants have accomplished a lot together, raising over $24 million for important causes. People from all over the world have come together as a community to make a dierence. And that is something to be proud of. Make a dierence. Join us for our “Grand Finale” and be a part of the LOVE RIDE’s rich history. Love Ride concerts have featured ZZ Top, BB King, Foo Fighters, Jackson Browne, Bruce Springsteen, Sheryl Crow, Sammy Hagar, Dwight Yoakum, the Doobie Brothers, Mick Fleetwood, Steve Miller Band, Black Crows, Lynyrd Skynrd, Little Feat, Crosby , Stills & Nash, Robbie Krieger & The Doors, George Thorogood, Billy Idol, Los Lobos, Eric Burdon and other ne artists that have performed. -
Experience Early Aviation with Fully
REVIEW Maxford’s vintage- themed models look extremely authentic when they are in the air, although pilots EXPERIENCE EARLY will probably want to spring for the available optional pilot figures to more AVIATION WITH capably create a convincing scalelike profile. FULLY FUNCTIONING WATCH A VIDEO! WING WARPING Access additional Maxford USA 1/9 Rumpler Taube EP 64-Inch ARF content by visiting By Jon Barnes | [email protected] www.ModelAviation. Photos by the author com/bonuscontent. THERE IS NO DENYING the surfaces, which would in the the Etrich Taube. Why the logic behind man’s eager efforts future become the standard for seeming disparity? It is primarily to take to the sky in a flying almost all aircraft, was the yaw because, with no licensing fees, machine. Engineers of the early axis. at least 14 companies built vari- 20th century understandably Designed by Igo Etrich in 1909, ations of the initial design. The attempted to mimic the methods the Taube first flew in 1910. It two-seat Rumpler Taube ulti- used by birds to change direction would become the first mass-pro- mately proved to be the most and altitude. At least one early duced aircraft in Germany, and common type and thus most effort to imitate the eminently go on to be used for military pur- appropriately the subject of flexible tail and wing feathers of poses by several of the nations Maxford’s attention. a bird can be seen in a mono- embroiled that were in World Maxford USA’s propensity to plane known as the Taube. War I. -
The Bleriot Xi: a Study in Aerodynamics by Robert G
THE BLERIOT XI: A STUDY IN AERODYNAMICS BY ROBERT G. WALDVOGEL If you wished to study aerodynamics, you would only need to look at the very early aircraft designs, such as the Bleriot XI. There are no high bypass ratio turbofans, nor upper deck lounges, nor global positioning systems. Instead, the aircraft is a sheer expression of the design solutions needed to overcome the four forces of flight: lift, weight, thrust, and drag. One of these “studies” can be made at Cole Palen’s Old Rhinebeck Aerodrome in Rhinebeck, New York. The culmination of ten previous configurations built by Louis Bleriot, who had reinvested 60,000 French francs amassed during an automobile lamp manufacturing venture to develop a technologically successful airplane in a race with such names as the Wright Brothers, Henri Farman, Santos Dumont, and Glenn Curtiss, the Bleriot XI itself had become the world’s first practical monoplane. The Bleriot VII, providing its initial foundation, had appeared with a partially enclosed fuselage to house its single pilot; wings braced to a tubular cabane framework over the cockpit; a four-bladed, 50-hp Antoinette engine; a large, dual-elevon horizontal tail; a small rudder; and swivelable, independently-sprung wheels. Although it crashed on December 18, 1907, it had nevertheless provided the foundation for a later, definitive design. The Bleriot VIII, rapidly following, had retained the low-wing configuration, but had featured pivoting, wing tip ailerons and a tricycle undercarriage, each comprised of single wheels. Although the Bleriot IX had been a larger variant of the VIII, and the Bleriot X had introduced a pusher-propeller arrangement with triple canard rudders, these intermediate steps had offered little to the ultimate design and therefore had been quickly discarded.