Theoretical analysis, based on linearized equation for supersonic flow; by restriction to case for which Mach lines from wing apex lie behind leading edge, simplified treatment was possible.


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    Title :

    Characteristics of thin triangular wings with triangular-tip control surfaces at supersonic speeds with Mach lines behind leading edge


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    33 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :