Section presents data on aerodynamic characteristics of revolution for angle of attack range of zero to almost 90° throughout supersonic and hypersonic flight regimes; basic theories governing pressure distributions on bodies of revolution and in their surrounding flow fields are evaluated. (Available, Superintendent of Documents, U S Government Printing Office, Washington, D.C.)


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    Title :

    Handbook of supersonic aerodynamics -- Section 8, bodies of revolution


    Additional title:

    U S Bur Naval Weapons NAVWEPS Report



    Publication date :

    1961


    Size :

    335 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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