Investigation made for thin flat plate wings for steady vertical and longitudinal motions, steady rolling and pitching and motions in which wing is accelerating uniformly in vertical direction.


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    Title :

    Theoretical relations between stability derivatives of wing in direct and in reverse supersonic flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    47 pages


    Remarks:

    Diagrs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :