Theoretical Lift and Damping in Roll at Supersonic Speeds of Thin Sweptback Tapered Wings with Streamwise Tips, Subsonic Leading Edges, and Supersonic Trailing Edges.


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    Title :

    Theoretical lift and damping in roll at supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges


    Additional title:

    Nat Advisory Committee Aeronautics -- Reports


    Contributors:


    Publication date :

    1950


    Size :

    16 pages


    Remarks:

    Diagrams, Graphs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :