Study is made of L.Lee's rule for hypersonic laminar boundary layer; it is shown that this rule is exact under assumptions invoked in inviscid theory of hypersonic flow; modified local flat plate similarity scheme derived, involving separate rules for velocity and enthalpy profiles, is compared with exact solutions and theory of hypersonic leading edge interaction.


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    Title :

    On local flat-plate similarity in hypersonic boundary layer


    Additional title:

    J Aerospace Sciences


    Contributors:
    Moore, F.K. (author)

    Published in:

    Publication date :

    1961


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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