Momentum-integral method for calculating subject boundary-layer growth for zero-angle-of-attack case; available flat-plate boundary-layer results permit calculations for cones for wide ranges of hypersonic Mach number and surface temperature; numerical results presented for slender cone show that slight blunting greatly affects conditions at outer edge of boundary layer; Mach number is markedly decreased at long distances from tip; local skin friction and heat transfer are significantly reduced by slight blunting.


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    Title :

    Laminar boundary-layer growth on slightly blunted cones at hypersonic speeds


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :