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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    Titel :

    Pre-flight development of modern aircraft


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Adams, H.W. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1957 Testing



    Erscheinungsdatum :

    1957


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    PRE-FLIGHT DEVELOPMENT OF MODERN AIRCRAFT

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


    Modern Aircraft Flight Control

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    Modern aircraft flight control

    Vukobratović, Miomir / Stojić, Radoslav | TIBKAT | 1988


    Modern aircraft flight control

    Vukobratović, Miomir ;Stojić, Radoslav | SLUB | 1988