Subject is studied with reference to missile configurations utilizing cruciform arrangements of wings and relatively large bodies of revolution; two methods of handling problem are presented.


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    Title :

    Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    32 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :