Results for the vibration measured at five locations on the fuselage structure during static operations are presented. The analysis was concerned with the magnitude of the vibration and the relative phase between different locations, the frequency response (inertance) functions between the exterior pressure field and the vibration, and the coherent output power functions at interior microphone locations based on sidewall vibration. Fuselage skin panels near the plane of rotation of the propeller accept propeller noise excitation more efficiently than they do exhaust noise.


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    Title :

    Evaluation of Aero Commander sidewall vibration and interior acoustic data: Static operations


    Contributors:

    Publication date :

    1980-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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