Attenuation in shock tube due to unsteady-boundary-layer action.


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    Title :

    Attenuation in shock tube due to unsteady-boundary-layer action


    Additional title:

    NACA -- Tech Note


    Contributors:
    Mirels, M. (author)


    Publication date :

    1956


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :