Simple cumulative fatigue damage law used to estimate endurance of typical components when subjected to alternating wing loads encountered by aircraft in flight; study of damage in terms of infinitesimally small intervals of alternating load and corresponding fatigue strength; life of structure is governed almost entirely by gust velocity; results compared with criteria suggested by P.B.WALKER, and K. WALKER.
Estimation of fatigue damage in aircraft wing structures
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 58 , n 522
1954
7 pages
Aufsatz (Zeitschrift)
Englisch
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