Theoretical study of laminar boundary layer on airfoil immersed in hypersonic stream is made under given assumption; numerical applications illustrate use of theory for flow along flat plate and for flow along curved wall for which shape is specified by certain governing profile parameters. Translation from Aerotecnica (Italy) Apr 1956 p 68-94.


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    Title :

    Laminar boundary layer at hypersonic speeds


    Additional title:

    NASA -- Tech Translation


    Contributors:
    Ferrari, C. (author)


    Publication date :

    1961


    Size :

    56 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :