Development program for acoustically loaded structure for DC-8 jet transport at Douglas Aircraft Co, using high-intensity-siren test facility and 24-in. sq panels; acoustic loads on structure determined by extrapolation of near field noise data of engines comparable in thrust to those of DC-8; relationships among load, response, and fatigue for both jet and sinusoidal loading investigated theoretically.


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    Title :

    Development of aircraft structure to withstand acoustic loads


    Additional title:

    Aero/Space Eng


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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