Paper presents flat plate friction and heat transfer data for many of hypersonic flight conditions of interest; parameters are calculated for flat plate at angle of attack from 0 to 50 ° with equilibrium dissociation of air behind shock wave and within laminar boundary layer and tabulated for wall temperatures between 1000 and 3000 R with free stream velocities of 10,000 to 28,000 ft.


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    Title :

    Laminar Skin-Friction and Heat-Transfer Parameters for Flat Plate at Hypersonic Speeds in Terms of Free-Stream Flow Properties


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    57 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :