Lift, drag, and pitching moments of models modified according to moment-of-area rule were measured and compared with those of unmodified configuration at Mach number from 0.6 to 1.4 and at angles of attack from -- 2° to +12°.


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    Title :

    Effect of moment-of-area-rule modifications of drag, lift, and pitching-moment characteristics of unswept aspect-ratio-6 wing and body combination


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :