Simulated flight history tests conducted as part of fatigue research program on C-46 wings; data obtained on crack initiation, location, rate and manner of fatigue crack propagation and final failure of wings are compared with results from constant amplitude tests on similar wings. See also NACA -- Tech 3190 indexed in Engineering Index 1954 p 52, under Aircraft Wings -- Stresses.
Fatigue investigation of full-scale transport-airplane wings -- Variable-amplitude tests with gust-loads spectrum
NACA -- Tech Note
1957
43 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1960
|Engineering Index Backfile | 1954
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