Purpose of P3A program was to demonstrate fatigue characteristics of wing and main landing gears under simulated flight-by-flight loading spectrum that represented planned service life of model; flight-by-flight test loading spectrum comprising 7500 flight hours was constructed with emphasis on air-ground-air transitions that are provided during flight-by-flight simulation and that adversely affect fatigue life; test methods devised provided automated loading system that faithfully duplicated service conditions on specimen in relatively short test-time span with small operating crew; applicability of methods to supersonic aircraft testing.
Full-scale structural fatigue test program
J Aircraft
Journal of Aircraft ; 2 , n 5
1965
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
A full-scale structural fatigue test program
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