Perturbations of N-shaped acoustic wave packet produced by aircraft motion are analyzed for case when N approaches caustic curve; equation is derived for maximum boom intensity in focalization zone.


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    Title :

    Geometrical acoustics, sonic boom of supersonic aircraft, and focalization


    Additional title:

    Acoustique geometrique, bruit balistique des avions supersoniques et focalisation


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    53 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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