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    Title :

    A study of a supersonic axisymmetric spiked inlet at angle of attackusing the Navier-Stokes equations


    Contributors:
    HOWLETT, D. (author) / HUNTER, L. (author)

    Conference:

    24th Aerospace Sciences Meeting ; 1986 ; Reno , NV , U.S.A.



    Publication date :

    1986-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Supersonic inlet study using the Navier-Stokes equations

    HUNTER, L. G. / TRIPP, J. M. / HOWLETT, D. G. | AIAA | 1986


    A Mach 2.0 plus supersonic inlet study using the Navier-Stokes equations

    HUNTER, L. / TRIPP, J. / HOWLETT, D. | AIAA | 1985