Use of jet spanning lower surface of wing as method of improving lift-drag ratio of supersonic aircraft by generating favorable interference effects investigated; results indicate some improvement which, however, does not appear to be large enough to be of practical use.


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    Title :

    Effects of lower surface jet on lift-drag ratio of 45° sweptback wing at mach number of 2.01


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :