Mathematical analysis and interpretation of forces affecting stability and controllability of airplane; most effective means against spinning; numerical examples show how dependent on certain conditions are entry and recovery, particularly on accidental coincidence of certain angles of attack and angles of yaw.


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    Title :

    Combined pitching and yawing motion of airplanes


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memo


    Contributors:
    Von Baranoff, A. (author) / Hopf, L. (author)


    Publication date :

    1931


    Size :

    29 pages


    Remarks:

    38 Figs., Supp. on plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Combined pitching and yawing motion of airplanes

    Baranoff, A V / Hopf, L | NTRS | 1931


    Combined pitching and yawing motion of airplanes

    Baranoff, A. / Hopf, L. | TIBKAT | 1931



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