Equations of motion for airplane penetrating gust derived using few simplifying assumptions; calculations of loads for different static longitudinal stability on two German airplane models, HC 45 and HS 122, compared with flight tests. English translation from (ZWB) Forschungsbericht n 1422 Dec 31 1940.


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    Title :

    Influence of static longitudinal stability on behavior of airplanes in gusts


    Additional title:

    NACA -- Tech Memo


    Contributors:
    Hoene, H. (author)


    Publication date :

    1951


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :