Iteration method suggested; with this method both supersonic and subsonic flows behind curved shock can be investigated and analytic expressions obtained so that general conclusions may be drawn.


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    Title :

    On flow behind attached curved shock


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Pai, S.I. (author)

    Published in:

    Publication date :

    1952


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :