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    Title :

    The effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel


    Contributors:

    Published in:

    Publication date :

    1944


    Size :

    12 S.


    Remarks:

    Ill., graph. Darst.
    Originally issued June 1944 as Advance restricted report L4F02


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik