Within limitations of linearized potential theory for supersonic flow, solutions have been obtained for damping in roll of triangular, trapezoidal, rectangular, and two sweptback plan forms.


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    Title :

    Damping due to roll of triangular, trapezoidal, and related plan forms in supersonic flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Jones, A.L. (author) / Alksne, A. (author)


    Publication date :

    1948


    Size :

    18 pages


    Remarks:

    6 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :