Six fatigue tests were conducted on C-46 aircraft wings; 2 at high constant-amplitude load, 2 with loading schedules based on gust-frequency statistics, and 2 with loading schedules developed from maneuver-loads statistics; results presented, discussed, and compared with previously published data from other tests in this series.
Fatigue investigation of full-scale transport-airplane wings -- Tests with constant-amplitude and variable-amplitude loading schedules
NASA -- Tech Note
1960
37 pages
Article (Journal)
English
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Engineering Index Backfile | 1957
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