It is shown that strip theory, that is, treating each chord-wise strip aerodynamically as portion of infinite unswept wing, is exact in determining contribution of any flexible or rigid body mode to generalized aerodynamic force on any rigid body mode; this result is approximation to correct result when second mode involved is flexible mode.


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    Title :

    Generalized aerodynamic forces on Delta wing with supersonic leading edges


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Walsh, J. (author) / Zartarian, G. (author) / Voss, H.M. (author)

    Published in:

    Publication date :

    1954


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :