Illustrated description of number of service failures of landing gear parts; these failures are believed to be due to low-cycle fatigue; static, impact, and fatigue tests are described, with description of test apparatus and methods; evidence presented is believed to warrant consideration of fatigue in design.
Airplane landing-gear fatigue problems
Aeronautical Eng Rev
Aeronautical Engineering Review ; 4 , n 11
1945
10 pages
Article (Journal)
English
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