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


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An experimental investigation of dynamic ground effect


    Beteiligte:

    Erscheinungsdatum :

    1986-04-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Experimental investigation of dynamic ground effect

    LEE, PAI-HUNG / LAN, C. EDWARD / MUIRHEAD, VINCENT U. | AIAA | 1989


    Experimental investigation of dynamic ground effect

    Lee, Pai-Hung / Lan, C. Edward / Muirhead, Vincent U. | NTRS | 1989


    Investigation of dynamic ground effect

    Chang, Ray Chung / Muirhead, Vincent U. | NTRS | 1987


    Experimental and Analytic Investigation of Ground Effect

    Traub, Lance W | Online Contents | 2015