Dynamic yawing loads considered on basis of restricted theory; comparison shown between computed loads and load measured in flight on fighter airplane; in order to take into account dynamic effects in design, specifications of yawing maneuverability or control movement are needed.


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    Title :

    Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Boshar, J. (author) / Davis, P. (author)


    Publication date :

    1946


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Consideration of dynamic loads on vertical tail by theory of flat yawing maneuvers

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