Wings are treated on assumption that flow potentials in planes at right angles to long axis of airfoils are similar to corresponding 2-dimensional potentials; pressure distributions caused by downward acceleration, pitching, rolling, sideslipping, and yawing are obtained for wings with and without dihedral; stability derivatives calculated from these distributions are expected to apply at both subsonic and supersonic speeds.


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    Title :

    Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :