The load distribution, forces, and moments are calculated theoretically for inclined slender wing-body combinations consisting of a slender body of revolution and either a plane or cruciform arrangement of low-aspect-ratio pointed wings. The results are applicable at subsonic and transonic speeds, and at supersonic speeds, provided the entire wing-body combination lies near the center of the Mach cone.


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    Title :

    The Aerodynamic Forces on Slender Plane- and Cruciform-Wing and Body Combinations


    Contributors:

    Publication date :

    1950-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English