Experimental studies were conducted to determine the longitudinal force and moment aerodynamic coefficients for a 1/48 scale model of an F-106 aircraft and a 0.01 scale model of an XB-70-1 aircraft. The two airplanes and one 60 degree delta wing model were designed and fabricated to satisfy the specific test conditions of the Kansas University wind tunnel with a 3 by 4.3 test section. Results of the tests are given


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    Title :

    Experimental Investigation of Dynamic Ground Effect. Semiannual Report, September 19, 1985-March 15, 1986


    Contributors:
    P. H. Lee (author) / C. E. Lan (author) / V. U. Muirhead (author)

    Publication date :

    1986


    Size :

    61 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English