Theoretical analysis based on linearized theory for supersonic flow; two cases treated: in one, flap extended outboard from center of wing and in other, flap extended inboard from wing tip.


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    Title :

    Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Tucker, W.A. (author) / Nelson, R.L. (author)


    Publication date :

    1948


    Size :

    43 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :