Results of sweptback wing tests compared with triangular wing results for Mach number of 1.43 show same trends of lift and drag as sweep angle is changed.


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    Title :

    Preliminary investigation at supersonic speeds of triangular and sweptback wings


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    37 pages


    Remarks:

    Illus, Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Preliminary Tests at Supersonic Speeds of Triangular and Swept-back Wings

    Ellis, Macon C , Jr / Hase , Lowell E | NTRS | 1947


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, Herbert S. / Malvestuto, Frank S. | TIBKAT | 1948


    Stability derivatives of triangular wings at supersonic speeds

    Ribner, H.S. / Malvestuto, Jr., F.S. | Engineering Index Backfile | 1948