Expressions derived for representative group of wing plan forms; analysis based on edge suction theory as well as linearized potential theory and applied to triangular, trapezoidal, rectangular, and sweptback plan forms without dihedral.


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    Title :

    Yawing moment due to sideslip 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 :

    1949


    Size :

    65 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :