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    Title :

    Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by Reynolds numbers up to 8.00 x 10(exp 6) and Mach numbers up to 0.29


    Contributors:

    Publication date :

    1955-10-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English