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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    Titel :

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


    Beteiligte:
    P. H. Lee (Autor:in) / C. E. Lan (Autor:in) / V. U. Muirhead (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    61 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch