Object of paper is to obtain lower bounds for resulting sonic boom, in track of aircraft, by appropriate design of aircraft geometry; aircraft, flying straight and level at supersonic speeds, is subject to various constraints on its total lift, volume, area distribution and center-of-pressure position.


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    Title :

    Lower bounds for sonic bangs in far field


    Additional title:

    Aeronautical Quarterly


    Contributors:
    Jones, L.B. (author)

    Published in:

    Publication date :

    1967


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Sonic bangs

    Warren, C.H.E. | Engineering Index Backfile | 1953


    Bibliography on sonic bangs

    Wadsworth, Jill | TIBKAT | 1968


    Methods for estimating distributions and intensities of sonic bangs

    Randall, D. G. / Aeronautical Research Council | TIBKAT | 1959