Abstract
We have experimentally studied the effect of asymmetric heating of gas-permeable porous inserts situated in front of a cylinder on the aerodynamics of this system in supersonic airflow with a Mach number of M∞ = 4.85. The inserts were heated by electric glow discharge. It is established that side forces perpendicular to the airflow axis arise and their quantitative characteristics are determined.
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A. V. Fedorov, V. F. Kozlov, A. N. Shiplyuk, A. A. Maslov, and N. D. Malmuth, AIAA J. 44(8), 1866 (2006).
V. M. Fomin, S. G. Mironov, and K. M. Serdyuk, Tech. Phys. Lett. 35, 117 (2009).
V. M. Fomin, A. A. Maslov, N. D. Malmuth, et al., AIAA J. 40(6), 1170 (2002).
I. A. Bedarev, S. G. Mironov, K. M. Serdyuk, A. V. Fedorov, and V. M. Fomin, J. Appl. Mech. Tech. Phys. 52(1), 9 (2011).
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Original Russian Text © S.G. Mironov, A.A. Maslov, I.S. Tsyryulnikov, 2014, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2014, Vol. 40, No. 19, pp. 83–88.
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Mironov, S.G., Maslov, A.A. & Tsyryulnikov, I.S. Controlling aerodynamic forces with the aid of gas-permeable porous materials. Tech. Phys. Lett. 40, 868–870 (2014). https://doi.org/10.1134/S1063785014100113
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DOI: https://doi.org/10.1134/S1063785014100113