Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack.


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    Title :

    Laminar boundary layer on cone in supersonic flow at large angle of attack


    Additional title:

    NACA -- Tech Note


    Contributors:
    Moore, F.K. (author)


    Publication date :

    1952


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :