Noise associated with aircraft flying at supersonic speeds is shown to depend primarily on shock wave pattern formed by aircraft; study of such patterns around aircraft in accelerated and retarded flight leads to explanation of booms, of short duration, heard by ground observers after aircraft has dived at supersonic speeds. (See also Roy Aeronautical Soc -- J v 57 n 510 June 1953 p 396-414; Engineering v 175 n 4549 Apr 3 1953 p 439-40)


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    Title :

    Some aspects of noise from supersonic aircraft


    Additional title:

    Nature (Lond)


    Contributors:
    Lilley, G.M. (author) / Westley, R. (author) / Yates, A.H. (author) / Busing, Y.R. (author)

    Published in:

    Nature ; 171 , n 4362


    Publication date :

    1953


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Some aspects of noise from supersonic aircraft

    Lilley, G.M. / Westley, R. / Yates, A.H. et al. | Engineering Index Backfile | 1953


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    Gabbay, E.J. | Engineering Index Backfile | 1958


    Some design aspects of slender aircraft for supersonic flight

    Küchemann, D. / Weber, J. | TIBKAT | 1974


    SUPERSONIC CONVERTIBLE LOW-NOISE AIRCRAFT

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    Free access