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.


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    Titel :

    Full-scale structural fatigue test program


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Ketola, R.N. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 2 , n 5 ; p 407-410


    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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