The Lift of a Delta Wing at Supersonic Speeds*
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An Experimental Investigation of the Flowfield over a Low Aspect Ratio Wing
A wind tunnel investigation was performed to study the flow field over a 70° swept sharped edge delta wing model at high angles of attack. The experiments were conducted in the subsonic wind tunnel at the Department of Mechanical Engineering, Sharif University of Technology. Velocity profiles have been measured using a special pitot tube and hot wire anemometer at angles of attacks of 10 to 35 ...
متن کاملAn Experimental Investigation of the Flowfield over a Low Aspect Ratio Wing
A wind tunnel investigation was performed to study the flow field over a 70° swept sharped edge delta wing model at high angles of attack. The experiments were conducted in the subsonic wind tunnel at the Department of Mechanical Engineering, Sharif University of Technology. Velocity profiles have been measured using a special pitot tube and hot wire anemometer at angles of attacks of 10 to 35 ...
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An extensive experimental investigation is conducted to study the effect of canard position relative to the fuselage reference line on the aerodynamic forces of a fighter type configuration model. Aerodynamic forces at different flight conditions are measured in a subsonic wind tunnel. The wing and the canard have triquetrous shapes. Experiments are conducted at Reynolds number of 342209 and at...
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[1] E. T. Whittaker and G. N. Watson, Modern Analysis, Cambridge Univ. Press, London, 1927, ch. 22. [2] R. Fricke, Die elliptische Funktionen, vol. 2, Leipzig, 1922, p. 293. [3] G. Holzmiiller, Einfiihrung in die Theorie der isogonalen Verwandtschaften und der conformen Abbildung, Teubner, Leipzig, 1882, pp. 256-258. [4] H. J. Stewart, The lift of a delta wing at supersonic speeds, Quart. Appl....
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