Significant errors are pointed out in accepted practice of writing aerodynamic forces and moments that act on body of revolution; more correct formulation presented shows that, even with linear aerodynamic coefficients, differential equations governing motion are fundamentally nonlinear.


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    Title :

    Study of aerodynamic forces and moments on bodies of revolution in combined pitching and yawing motions


    Additional title:

    NASA -- Tech Note


    Contributors:
    Tobak, M. (author) / Lessing, H.C. (author)


    Publication date :

    1960


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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