Douglas Aircraft's development program in production of DC-8 commercial aircraft includes increased amount of structural fatigue studies ranging from tests of large portions of fuselage and panel tests to detail fatigue tests of joints and fittings; types of loads included: pressure cabin cycling, flight gust loads, and acoustic pressure loads; testing DC-8 a-c electric system; testing of sound suppressors and thrust reversers.


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    Title :

    Pre-flight development of modern aircraft


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Adams, H.W. (author)

    Conference:

    Society of Automotive Engineers -- Meeting ; 1957 Testing



    Publication date :

    1957


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    PRE-FLIGHT DEVELOPMENT OF MODERN AIRCRAFT

    ADAMS, H. W. | SAE Technical Papers | 1957


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