Standard

Plasma control of shock waves in aerodynamics and sonic boom mitigation. / Miles, Richard B.; Macheret, Sersey O.; Martinelli, Luigi; Murray, Robert; Shneider, Mikhail; Ionikh, Yu Z.; Kline, John; Fox, Jon.

2001. Работа представлена на 32nd AIAA Plasmadynamics and Lasers Conference 2001, Anaheim, CA, Соединенные Штаты Америки.

Результаты исследований: Материалы конференций › материалы › Рецензирование

Harvard

Miles, RB, Macheret, SO, Martinelli, L, Murray, R, Shneider, M, Ionikh, YZ, Kline, J & Fox, J 2001, 'Plasma control of shock waves in aerodynamics and sonic boom mitigation', Работа представлена на 32nd AIAA Plasmadynamics and Lasers Conference 2001, Anaheim, CA, Соединенные Штаты Америки, 11/06/01 - 14/06/01. https://doi.org/10.2514/6.2001-3062

APA

Miles, R. B., Macheret, S. O., Martinelli, L., Murray, R., Shneider, M., Ionikh, Y. Z., Kline, J., & Fox, J. (2001). Plasma control of shock waves in aerodynamics and sonic boom mitigation. Работа представлена на 32nd AIAA Plasmadynamics and Lasers Conference 2001, Anaheim, CA, Соединенные Штаты Америки. https://doi.org/10.2514/6.2001-3062

Vancouver

Miles RB, Macheret SO, Martinelli L, Murray R, Shneider M, Ionikh YZ и пр.. Plasma control of shock waves in aerodynamics and sonic boom mitigation. 2001. Работа представлена на 32nd AIAA Plasmadynamics and Lasers Conference 2001, Anaheim, CA, Соединенные Штаты Америки. https://doi.org/10.2514/6.2001-3062

Author

Miles, Richard B. ; Macheret, Sersey O. ; Martinelli, Luigi ; Murray, Robert ; Shneider, Mikhail ; Ionikh, Yu Z. ; Kline, John ; Fox, Jon. / Plasma control of shock waves in aerodynamics and sonic boom mitigation. Работа представлена на 32nd AIAA Plasmadynamics and Lasers Conference 2001, Anaheim, CA, Соединенные Штаты Америки.

BibTeX

@conference{66a2f80fd3004d3381b8da84b9e582c6,
title = "Plasma control of shock waves in aerodynamics and sonic boom mitigation",
abstract = "There is a great deal of interest in the possibility of using plasmas for various aerospace applications ranging from drag reduction to power extraction. This paper outlines a series of experimental and modeling efforts that are directed toward determining the viability of these concepts. The first issue addressed is the question regarding anomalously high shock propagation speeds and shock splitting in weakly ionized gases that have been reported in the literature. Careful modeling and experiments of both steady-state and pulsed plasmas suggest that these observations are due to predictable effects from temperature gradients. The utilization of thermal plasmas for drag reduction, vehicle steering, and sonic boom mitigation, and cold, nonequilibrium plasmas for MHD flow control and power extraction are then discussed.",
author = "Miles, {Richard B.} and Macheret, {Sersey O.} and Luigi Martinelli and Robert Murray and Mikhail Shneider and Ionikh, {Yu Z.} and John Kline and Jon Fox",
year = "2001",
month = jan,
day = "1",
doi = "10.2514/6.2001-3062",
language = "English",
note = "32nd AIAA Plasmadynamics and Lasers Conference 2001 ; Conference date: 11-06-2001 Through 14-06-2001",

}

RIS

TY - CONF

T1 - Plasma control of shock waves in aerodynamics and sonic boom mitigation

AU - Miles, Richard B.

AU - Macheret, Sersey O.

AU - Martinelli, Luigi

AU - Murray, Robert

AU - Shneider, Mikhail

AU - Ionikh, Yu Z.

AU - Kline, John

AU - Fox, Jon

PY - 2001/1/1

Y1 - 2001/1/1

N2 - There is a great deal of interest in the possibility of using plasmas for various aerospace applications ranging from drag reduction to power extraction. This paper outlines a series of experimental and modeling efforts that are directed toward determining the viability of these concepts. The first issue addressed is the question regarding anomalously high shock propagation speeds and shock splitting in weakly ionized gases that have been reported in the literature. Careful modeling and experiments of both steady-state and pulsed plasmas suggest that these observations are due to predictable effects from temperature gradients. The utilization of thermal plasmas for drag reduction, vehicle steering, and sonic boom mitigation, and cold, nonequilibrium plasmas for MHD flow control and power extraction are then discussed.

AB - There is a great deal of interest in the possibility of using plasmas for various aerospace applications ranging from drag reduction to power extraction. This paper outlines a series of experimental and modeling efforts that are directed toward determining the viability of these concepts. The first issue addressed is the question regarding anomalously high shock propagation speeds and shock splitting in weakly ionized gases that have been reported in the literature. Careful modeling and experiments of both steady-state and pulsed plasmas suggest that these observations are due to predictable effects from temperature gradients. The utilization of thermal plasmas for drag reduction, vehicle steering, and sonic boom mitigation, and cold, nonequilibrium plasmas for MHD flow control and power extraction are then discussed.

UR - http://www.scopus.com/inward/record.url?scp=85087602424&partnerID=8YFLogxK

U2 - 10.2514/6.2001-3062

DO - 10.2514/6.2001-3062

M3 - Paper

AN - SCOPUS:85087602424

T2 - 32nd AIAA Plasmadynamics and Lasers Conference 2001

Y2 - 11 June 2001 through 14 June 2001

ER -

ID: 62197635