General velocity potential for slender pointed body of revolution oscillating periodically in supersonic uniform stream, presented; two types of bodies of revolution are examined to demonstrate how aerodynamic stability derivates may be varied by changing contour of body; "flaring" aft end of body is shown to increase lift, as well to increase aerodynamic damping moment of finless body.


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    Title :

    Nonsteady supersonic flow about pointed bodies of revolution


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1951


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :