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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    Titel :

    Shock wave noise of supersonic aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Ryhming, I.L. (Autor:in) / Yoler, Y.A. (Autor:in) / Aoki, Y. (Autor:in)

    Kongress:

    SAE Meeting ; 1960 Noise



    Erscheinungsdatum :

    1960


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT

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


    Shock wave noise problem of supersonic aircraft

    Engineering Index Backfile | 1959


    THE SHOCK WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT

    Hubbard, H. H. / Maglieri, D. J. | NTRS | 1959


    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