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|a 1273206175
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|a 9780768099430
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|a 10.4271/9780768099430
|2 doi
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|a UAMI
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|a Schmidt, R. Kyle,
|e author.
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|a The design of aircraft landing gear /
|c R. Kyle Schmidt.
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|a Warrendale, Pennsylvania, USA :
|b SAE International,
|c [2020]
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|a 1 online resource (2 volumes (xxiii, 1049, 16 pages)) :
|b illustrations (some color)
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|a Includes bibliographical references and index.
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|a The Design of Aircraft Landing Gear is designed to guide the reader through the key principles of landing system design and to provide additional references when available. Many problems which must be confronted have already been addressed by others in the past, but the information is not known or shared, leading to the observation that there are few new problems, but many new people. It is intended to share much of the existing information and provide avenues for further exploration. The design of an aircraft and its associated systems, including the landing system, involves iterative loops as the impact of each modification to a system or component is evaluated against the whole. It is rare to find that the lightest possible landing gear represents the best solution for the aircraft: the lightest landing gear may require attachment structures which don't exist and which would require significant weight and compromise on the part of the airframe structure design.
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|a Print version record.
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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|a eBooks on EBSCOhost
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|a Airplanes
|x Landing gear
|x Design and construction.
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|a Airplanes
|x Landing gear
|x Design and construction
|2 fast
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|i Print version:
|a Schmidt, R. Kyle.
|t Design of aircraft landing gear.
|d Warrendale, Pennsylvania, USA : SAE International, [2020]
|z 0768099420
|w (OCoLC)1253292096
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