A response analysis is carried out to determine the predictability of sidewall accelerations in aircraft, to investigate whether it is necessary to model the exterior pressure as a traveling wave as opposed to a standing wave, and to determine the importance of parameters describing the exterior pressure and sidewall panel. Prediction of the acceleration response is found to be improved by including traveling wave and spatial variation effects of the exterior pressure in the model. Variations with propeller rpm are found to be important for the longer panel.


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    Titel :

    Acceleration response of fuselage sidewall panels on a twin-engine, light aircraft


    Beteiligte:
    Roussos, L. A. (Autor:in) / Mixson, J. S. (Autor:in)

    Kongress:

    In: Noise-Con 81 ; 1981 ; Raleigh, NC


    Erscheinungsdatum :

    01.01.1981


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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