Abstract
The profiles of conical bodies for which the position of the center of pressure in a supersonic flow with symmetry plane does not depend on the flow parameters are considered. The theoretical investigation of the aerodynamic characteristics of circular cones [1] has shown that their center of pressure does not depend on the angle of attack α when the shock wave is attached to the apex of the cone. It was established experimentally in [2, 3] for star-shaped bodies that the position of the center of pressure for such bodies hardly changes in a wide range of Mach numbers and angles of attack.
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Yu. N. D'yakonov, L. V. Pchelkina, and I. D. Sandomirskaya, Supersonic Flow over Blunt Bodies [in Russian], Izd. Mosk. Unt., Moscow (1971).
A. L. Gonor, M. N. Kazakov, A. I. Shvets, and V. I. Shein, “Aerodynamic characteristics of star-shaped bodies at supersonic velocities,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1 (1971).
A. L. Gonor, M. A. Zubin, and N. A. Ostapenko, “Experimental investigation of the aerodynamic characteristics of star-shaped bodies at supersonic velocities,” Proceedings of the Institute of Mechanics at the Moscow State University: Nonequilibrium Gas Flows and the Optimal Profiles of Bodies in a Supersonic flow [in Russian], Izd. Mosk. Unt., Moscow (1978).
A. L. Gonor, “Newton's law of resistance for bodies formed by intersecting surfaces,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1 (1967).
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 99–104, January–February, 1980.
I thank G. G. Chernyi for discussing the results.
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Ostapenko, N.A. On the center of pressure of conical bodies. Fluid Dyn 15, 80–84 (1980). https://doi.org/10.1007/BF01089817
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DOI: https://doi.org/10.1007/BF01089817