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Formation and structure of a shock wave around a body under the condition of direct heat addition. / Kuchinsky, V. V.; Soukhomlinov, S.; Sheverev, V. A.; Otugen, M. V.

Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1: Forums. ed. / T.J. O Hern; T.J. O Hern. Vol. 1 2003. p. 809-814.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Kuchinsky, VV, Soukhomlinov, S, Sheverev, VA & Otugen, MV 2003, Formation and structure of a shock wave around a body under the condition of direct heat addition. in TJ O Hern & TJ O Hern (eds), Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1: Forums. vol. 1, pp. 809-814, 2001 ASME Fluids Engineering Division Summer Meeting, New Orleans, LA, United States, 29/05/01.

APA

Kuchinsky, V. V., Soukhomlinov, S., Sheverev, V. A., & Otugen, M. V. (2003). Formation and structure of a shock wave around a body under the condition of direct heat addition. In T. J. O Hern, & T. J. O Hern (Eds.), Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1: Forums (Vol. 1, pp. 809-814)

Vancouver

Kuchinsky VV, Soukhomlinov S, Sheverev VA, Otugen MV. Formation and structure of a shock wave around a body under the condition of direct heat addition. In O Hern TJ, O Hern TJ, editors, Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1: Forums. Vol. 1. 2003. p. 809-814

Author

Kuchinsky, V. V. ; Soukhomlinov, S. ; Sheverev, V. A. ; Otugen, M. V. / Formation and structure of a shock wave around a body under the condition of direct heat addition. Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1: Forums. editor / T.J. O Hern ; T.J. O Hern. Vol. 1 2003. pp. 809-814

BibTeX

@inproceedings{3b8530e7a3d54416a2443cf05bdfbbf9,
title = "Formation and structure of a shock wave around a body under the condition of direct heat addition",
abstract = "A physical model for the supersonic flight of a body in low temperature plasma is developed in this paper. It is shown that, at supersonic speeds, the effect of low temperature plasma is equivalent to that of heat deposition into the shock wave. An analytical solution for the shock wave structure is obtained. Effects of shock wave dissipation and increase in shock standoff distance are predicted. Results of ballistic experiments in plasma are satisfactorily explained on the basis of the proposed model. In addition, the efficiency of drag force reduction by low-temperature plasma at supersonic speeds is evaluated.",
author = "Kuchinsky, {V. V.} and S. Soukhomlinov and Sheverev, {V. A.} and Otugen, {M. V.}",
year = "2003",
language = "English",
isbn = "0791835324",
volume = "1",
pages = "809--814",
editor = "{O Hern}, T.J. and {O Hern}, T.J.",
booktitle = "Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1",
note = "2001 ASME Fluids Engineering Division Summer Meeting ; Conference date: 29-05-2001 Through 01-06-2001",

}

RIS

TY - GEN

T1 - Formation and structure of a shock wave around a body under the condition of direct heat addition

AU - Kuchinsky, V. V.

AU - Soukhomlinov, S.

AU - Sheverev, V. A.

AU - Otugen, M. V.

PY - 2003

Y1 - 2003

N2 - A physical model for the supersonic flight of a body in low temperature plasma is developed in this paper. It is shown that, at supersonic speeds, the effect of low temperature plasma is equivalent to that of heat deposition into the shock wave. An analytical solution for the shock wave structure is obtained. Effects of shock wave dissipation and increase in shock standoff distance are predicted. Results of ballistic experiments in plasma are satisfactorily explained on the basis of the proposed model. In addition, the efficiency of drag force reduction by low-temperature plasma at supersonic speeds is evaluated.

AB - A physical model for the supersonic flight of a body in low temperature plasma is developed in this paper. It is shown that, at supersonic speeds, the effect of low temperature plasma is equivalent to that of heat deposition into the shock wave. An analytical solution for the shock wave structure is obtained. Effects of shock wave dissipation and increase in shock standoff distance are predicted. Results of ballistic experiments in plasma are satisfactorily explained on the basis of the proposed model. In addition, the efficiency of drag force reduction by low-temperature plasma at supersonic speeds is evaluated.

UR - http://www.scopus.com/inward/record.url?scp=0346955743&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0346955743

SN - 0791835324

VL - 1

SP - 809

EP - 814

BT - Proceedings of the 2001 ASME Fluids Engineering Division Summer Meeting. Volume 1

A2 - O Hern, T.J.

A2 - O Hern, T.J.

T2 - 2001 ASME Fluids Engineering Division Summer Meeting

Y2 - 29 May 2001 through 1 June 2001

ER -

ID: 9653354