Lift-drag ratio attainable by slender flat-top body at supersonic speeds, considering Newtonian pressure distribution and constant skin friction


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    Title :

    Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body.


    Contributors:
    Brown, S. L. (author) / Hull, D. G. (author) / Miele, A. (author)

    Published in:

    Publication date :

    1967-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English