Lift and drag measurements made on models in Langley Unitary Plan wind tunnel; values of maximum lift-drag ratio were about 1.4 at Mach 2.65 and about 1.2 at Mach 4.65; angles of attack of tests were limited by unsteady behavior of models.


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    Title :

    Wind-tunnel investigation of paraglider models at supersonic speeds


    Additional title:

    NASA -- Tech Notes


    Contributors:


    Publication date :

    1961


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :