Determination of pressure distribution over thin, finite wing in supersonic flow due to prescribed incidence that varies slowly in time (so that square of reduced frequency may be regarded as negligible) is reduced to pair of steady flow problems.


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    Title :

    First-order formulation of unsteady supersonic flow problem for finite wings


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Miles, J.W. (author)


    Publication date :

    1956


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English