Abstract
The effect of a strong shock wave on a weakly ionized collisional plasma was studied. The structure of the ion-acoustic perturbation caused by the shock wave was numerically investigated. The effect of the nonlinearity, dispersion, and dissipation on the formation of an oscillating wave profile was shown. It is found that in some modes, an increase in the shock wave velocity leads to a sharp increase in the concentration of charged particles and a reduction in the number of perturbation maxima. This change of the flow structure can be preceded by the formation of localized regions with an increased degree of plasma ionization. It is shown that the presence of plasmoids can lead to a strong influence of charges on the neutral component.
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R. F. Avramenko, A. I. Klimov, Yu. L. Serov, I. P. Yavor, and R. F. Bedin, “Anomalous Plasma Flow around Bodies,” Inventor’s Certificate No. 007, Priority September 17, 1980, Registered December 25, 1986 in the State Register of Discoveries of the USSR.
Yu. L. Serov, “Experimental Investigation of a Supersonic Sphere Motion in a Plasma on Ballistic Apparatus,” in Proc. of the 2nd Weakly Ionized Gases Workshop, Norfolk (USA), April 24–25, 1998 (S. l., 1998), pp. 32–45.
G. I. Mishin, “Experimental Investigation of the Flight of a Sphere in Weakly Ionized Air,” in Proc. of the 15th Aerodynamics Conf., Atlanta, June 23–25, 1997 (S. l., 1997).
V. E. Semenov, V. G. Bondarenko, V. B. Gildenburg, et al., “Weakly Ionized Plasmas in Aerospace Applications,” Plasma Phys. Control. Fusion. 44, B293–B305 (2002).
L. N. Myrabo, Yu. P. Raizer, M. N. Shneider, and R. Bracken, “Reduction of Drag and Energy Consumption During Energy Release Preceding a Blunt Body in Supersonic Flow,” Teplofiz. Vysok. Temp. 42, 890–899 (2004).
P. Bletzinger, B. N. Ganguly, D. van Wie, and A. Garscadden, “Plasmas in High Speed Aerodynamics,” J. Phys., D: Appl. Phys. 38, R33–R57 (2005).
V. Yu. Kolosov, V. S. Sukhomlinov, V. Yu. Sepman, et al., “Acoustic Dispersion Effect on the Propagation of a Shock Wave in a Glow Discharge Plasma,” in Proc. of the 9th Int. Space Planes and Hypersonic Systems and Technologies Conf., Norfolk (USA), 1999 (AIAA, 1999), Paper No. 99–4882.
D. A. Koroteyev, “On the Impact of Plasma Formations on Shock Waves,” Polet, No. 2, 36–42 (2008).
G. I. Mishin, A. P. Bedin, N. I. Yushchenkova, et al., “Abnormal Relaxation and Instability of Shock Waves in Gases,” Zh. Tekh. Fiz. 51 (11), 2315–2324 (1981).
V. A. Pavlov, “On the Structure of the Ion-Acoustic Shock Wave in a Weakly Ionized Plasma,” Fiz. Plasmy 22 (2), 182–187 (1996).
V. A. Pavlov, “Ion-Sound Effect of the Houston Horse,” Fiz. Plasmy 26 (6), 543–547 (2000).
V. A. Pavlov, “Weakly Ionized Plasma in Supersonic Flow,” Fiz. Plasmy 28 (2), 522–526 (2002).
V. A. Pavlov, “Influence of Supersonic Ion Clusters on the Plasma Neutral Component,” Int. J. Geomagnetism Aeronomy 7 (1), 1–7 (2007).
U. M. Ascher and L. R. Petzold, Computer Methods for Ordinary Differential Equations and Differential-Algebraic Equations (SIAM, Philadelphia, 1998).
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Original Russian Text © V.A. Pavlov, Ya.V. Tryaskin.
Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 56, No. 3, pp. 21–29, May–June, 2015.
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Pavlov, V.A., Tryaskin, Y.V. Plasma effect of the Houston horse. J Appl Mech Tech Phy 56, 361–368 (2015). https://doi.org/10.1134/S0021894415030037
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DOI: https://doi.org/10.1134/S0021894415030037