Calculations based on linearized supersonic flow theory and on additional assumption that Mach cones yaw with wing.


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    Title :

    Effect of thickness on lateral force and yawing moment of sideslipping Delta wing at supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English