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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    01.01.1950


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch