Whitham's theory for predicting boom intensity is combined with lifting effects to assess shock noise of aircraft flying at supersonic speeds; investigation limited to steady level flight conditions; boom intensity evaluated at ground points along aircraft's track.


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    Title :

    Investigation of lifting effects on intensity of sonic booms


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Morris, J. (author)

    Published in:

    Publication date :

    1960


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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