Report presents supersonic trim-drag calculations in such form that wing-plus-tail, wing-plus-canard and wing-alone configurations may be easily compared, and in such form that static margin is immediately available; general equations for lift, moment, and drag coefficient due to lift.


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    Title :

    Trim drag at supersonic speeds of various delta-planform configurations


    Additional title:

    NASA -- Tech Note


    Contributors:
    Graham, M.E. (author) / Ryan, B.M. (author)


    Publication date :

    1960


    Size :

    98 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :