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    Title :

    Some Effects of Aeroelasticity at Mach Numbers from 0.7 to 1.6 on the Rolling Effectiveness of Thin Flat-plate Delta Wings Having 45 Degree Swept Leading Edges and Full-span Constant-chord Ailerons


    Contributors:

    Publication date :

    1952-02-19


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English