The plasma of the discharge, initiated along a surface of wing or the fuselage, is promising aircraft control facility. Strong shock wave formation at air gap disruption by the sliding discharge (SD) changes a flow over aircraft surface and creates an impulse for changing a trajectory of flight (see Figure 1). Critical existence conditions measurements of the sliding discharge in an air flow are important for its application in supersonic aircraft. These conditions at supersonic flows were investigated earlier [1], [2]. The purpose of this work is to direct measure of efficiency SD to create impulse obtained by wing in the subsonic and supersonic air flow.
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V.S. Aksenov, V.V. Golub, S.A. Gubin, V.P. Efremov, I.V. Maklashova, A.I. Kharitonov, Yu.L. Sharov Sliding Electric Arc Discharge as a Means of Aircraft Trajectory Control Tech. Phys. Letters, vol. 30, No. 10, pp. 871-873, 2004
V.S. Aksenov, S.A. Gubin, D.V. Blagodatskih, M.V. Bragin, V.V. Golub, V.V. Volodin, I.N. Laskin Active Flow Control by the Sliding Electric Arc Discharge, European conference for aerospace sciences, July 4-7th 2005
V.V. Golub, V.S. Aksenov, D.I. Baklanov, V.V. Volodin, S.V. Golovastov, S.A. Gubin, V.P. Efremov, A.S. Savel’ev, V.E. Fortov, Yu.L. Sharov Issledovanie vliyaniya magnitnogo polya na initsiirovanie detonatsii iskrovym razryadom v vodorodo-vozdushnoi smesi, Dokladi Akademii Nauk vol. 404, N 3, pp. 321-326, 2005
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Aksenov, V., Gubin, S., Efremov, K., Golub, V. (2009). Experimental investigation of the sliding electric frequency mode arc discharge in the subsonic and supersonic flow. In: Hannemann, K., Seiler, F. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_73
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DOI: https://doi.org/10.1007/978-3-540-85181-3_73
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