Of two approaches for providing safety against catastrophic aircraft structural fatigue, "safe life" and "fail safe" methods, author concludes that safe life method is generally inadequate while fail safe method is practical and sound; fail safe attributes of certain materials, stress levels and details of design, summarized from Lockheed tests; from fail safe standpoint 2024 is superior to 7075 aluminum alloy. (see also Flight v 69 n 2463 Apr 6 1956 p 394-7)


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    Titel :

    Fatigue and fail safe airframe design


    Weitere Titelangaben:

    Soc Automotive Engrs -- Trans


    Beteiligte:


    Erscheinungsdatum :

    1956


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Fatigue and Fail-Safe Airframe Design

    McBrearty, J. F. | SAE Technical Papers | 1956


    Fatigue and fail safe airframe design

    McBrearty, J.F. | Engineering Index Backfile | 1956


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    Freier Zugriff