Attempt is made to find most favorable speed-altitude schedule for transport or bomber, with minimum shock-wave noise as prime consideration; propagation of shock waves for case of homogeneous atmosphere and also for normal atmosphere exhibiting temperature and wind gradients, recent experimental results and available theory concerning "sonic boom" given.


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    Title :

    Sonic boom -- Limitations on supersonic aircraft operations


    Additional title:

    Aero/Space Eng


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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