Theoretical methods developed by G.B.WHITMAN and F.WALKDEN are used to study possibilities of using aerodynamic interference to reduce or suppress shock wave noise due to lift by conventional aircraft; wind tunnel experiments with wing body configurations are conducted and are analyzed in light of theoretical indications.


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    Title :

    Shock wave noise of supersonic aircraft


    Additional title:

    SAE -- Paper


    Contributors:
    Ryhming, I.L. (author) / Yoler, Y.A. (author) / Aoki, Y. (author)

    Conference:

    SAE Meeting ; 1960 Noise



    Publication date :

    1960


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT

    RYHMENG, I. L. / AOKI, Y. / YOLER, Y. A. | SAE Technical Papers | 1960


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    Engineering Index Backfile | 1959


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    Shock-wave noise problem of supersonic aircraft in steady flight

    Maglieri, D.J. / Carlson, H.W. | Engineering Index Backfile | 1959


    The shock-wave noise problem of supersonic aircraft in steady flight

    Maglieri, Domenic J. / Carlson, Harry W. | TIBKAT | 1959