Tests made to determine effect of conical wing camber on aerodynamic characteristics of wing body combination having 3% thick wing, at Mach 0.80 to 1.05 and angles of attack from -- 4 to 14°; appendix on influence of leading edge suction and span load efficiency on drag due to lift factors of plane and cambered wings included.


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    Title :

    Transonic aerodynamic characteristics of wing-body combination having 52.5° sweptback wing of aspect ratio 3 with conical camber and designed for Mach number of 2 root


    Additional title:

    NASA -- Tech Note


    Contributors:
    Igoe, W.B. (author) / Re, R.J. (author) / Cassetti, M.D. (author)


    Publication date :

    1961


    Size :

    51 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :