Sportplane Construction Techniques
Sportplane Construction Techniques

Author: Tony Bingelis

Publisher:

Published: 2021

Total Pages:

ISBN-13: 9781734133059

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This book is a great technical resource for homebuilt aircraft builders that includes sections on getting ready to build, construction practices, fiberglass components, control systems, aircraft interiors, canopies and windshields, landing gear, instrumentation, electrical systems, and finishing.All of Tony's books are must haves for anyone building or thinking about building their own airplane. Each is a collection of his columns from the Experimental Aircraft Association's flagship monthly magazine, EAA Sport Aviation. Tony's work covers the topics in exceptional detail, and the reader benefits not only from Tony's extensive firsthand experience as a homebuilder, but also from his time in the U.S. Air Force, and his volunteer service to EAA as a Technical Counselor.

Aircraft Structures
Aircraft Structures

Author: David J. Peery

Publisher: Courier Corporation

Published: 2013-04-29

Total Pages: 578

ISBN-13: 048626730X

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This legendary, still-relevant reference text on aircraft stress analysis discusses basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition.

Introduction to Aircraft Flight Mechanics
Introduction to Aircraft Flight Mechanics

Author: Thomas R. Yechout

Publisher: AIAA

Published: 2003

Total Pages: 666

ISBN-13: 9781600860782

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Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Flight Testing Homebuilt Aircraft
Flight Testing Homebuilt Aircraft

Author: Vaughan Askue

Publisher: Iowa State Press

Published: 1992-01-01

Total Pages: 177

ISBN-13: 9780813813080

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Now that it's built, how well will it fly? Flight Testing Homebuilt Aircraft tells how to test such aircraft systematically and safely, with professional results. It defines flight testing as a four-phase step-by-step process of learning the limitations of an aircraft; defining and eliminating aircraft problems; and determining aircraft capability and optimum flying techniques - all with minimum risk to pilot and machine. With straightforward description and more than 80 illustrations, the book teaches builders to use this process to design thorough, safe flight tests customized to specific aircraft in specific testing environments.

Bonded Repair of Aircraft Structures
Bonded Repair of Aircraft Structures

Author: A. Baker

Publisher: Springer Science & Business Media

Published: 1988-05-31

Total Pages: 236

ISBN-13: 9789024736065

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The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability.