Investigation of Laminar Aerodynamic Heat-Transfer Characteristics of Hemisphere-Cylinder in Langley 11-Inch Hypersonic Tunnel at Mach Number of 6.8.


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    Title :

    Investigation of laminar aerodynamic heat-transfer characteristics of hemisphere-cylinder in Langley 11-inch hypersonic tunnel at mach number of 6.8


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1956


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :