Newtonian closed-form expressions for aerodynamic coefficients are developed for complete and partial conic and spheric bodies at combined angles of attack and sideslip; calculations from expressions presented in tabulated form; comparisons of theory with hypersonic experimental data for many shapes.


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    Title :

    Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data


    Additional title:

    NASA -- Tech Report


    Contributors:


    Publication date :

    1962


    Size :

    306 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :