Report describes mostly computational study of hypersonic flow about sharp cone. Part of continuing effort to understand and predict complicated aerodynamic and heat-transfer phenomena in flows over forebodies of such hypersonic vehicles as Space Shuttle and proposed National Aerospace Plane. Focuses on transition from laminar to turbulent flow, with particular reference to heat-transfer predictions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Computed Hypersonic Flow About A Sharp Cone


    Contributors:

    Published in:

    Publication date :

    1991-10-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Sharp cone drag measurements in a rarefied hypersonic flow.

    JONES, M. H. / MILLER, J. T. | AIAA | 1969


    Nonequilibrium Calculation of Shock Shapes Over Sharp-Cone in Intermediate Hypersonic Air Flow

    Furudate, M. / Nonaka, S. / Sawada, K. et al. | British Library Conference Proceedings | 1999


    Rarefied Hypersonic Flow over a Sharp Cone : DSMC, Navier Stokes and Experimental Results

    Lengrand, J. C. / Chpoun, A. / Allegre, J. et al. | British Library Conference Proceedings | 1994


    An experimental study of hypersonic turbulence on a sharp cone

    HARVEY, J. / BERGMAN, R. / HOLDEN, M. | AIAA | 1989


    Hypersonic parabolized Navier-Stokes code validation on a sharp nose cone

    Huebner, Lawrence D. / Pittman, James L. / Dilley, Arthur D. | NTRS | 1989