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Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1. / Knight, Doyle; Brovkin, Vadim; Khmara, Dmitri; Kolesnichenko, Yuri; Lashkov, Valeriy; Mashek, Igor.

Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles. 2009. (European Space Agency, (Special Publication) ESA SP; Том 659 SP).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование

Harvard

Knight, D, Brovkin, V, Khmara, D, Kolesnichenko, Y, Lashkov, V & Mashek, I 2009, Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1. в Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles. European Space Agency, (Special Publication) ESA SP, Том. 659 SP, 6th European Symposium Aerothermodynamics for Space Vehicles, Versailles, Франция, 3/11/08.

APA

Knight, D., Brovkin, V., Khmara, D., Kolesnichenko, Y., Lashkov, V., & Mashek, I. (2009). Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1. в Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles (European Space Agency, (Special Publication) ESA SP; Том 659 SP).

Vancouver

Knight D, Brovkin V, Khmara D, Kolesnichenko Y, Lashkov V, Mashek I. Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1. в Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles. 2009. (European Space Agency, (Special Publication) ESA SP).

Author

Knight, Doyle ; Brovkin, Vadim ; Khmara, Dmitri ; Kolesnichenko, Yuri ; Lashkov, Valeriy ; Mashek, Igor. / Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1. Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles. 2009. (European Space Agency, (Special Publication) ESA SP).

BibTeX

@inproceedings{d2d8002d89cf40f4a2db89894ffbaf00,
title = "Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1",
abstract = "The interaction of a microwave-generated plasma with a hemisphere cylinder at Mach 2.1 is simulated. The theoretical model is the unsteady threedimensional Euler equations for a multi- species reacting gas. The thermochemistry model for air incorporates 23 species and 238 reactions. The initial condition for the simulation is the steady flow past the hemisphere cylinder.A 9 GHz microwave pulse of 1.2 μs duration is focused upstream of the blunt body shock on the hemisphere cylinder centerline. The high temperature plasma region generated by the microwave pulse is convected to the hemisphere cylinder and interacts with the blunt body shock resulting in the momentary formation of a recirculation region and reduction in surface pressure on the hemisphere cylinder centerline. The computed surface pressure shows good agreement with experiment.",
keywords = "CFD., Energy deposition, Microwave",
author = "Doyle Knight and Vadim Brovkin and Dmitri Khmara and Yuri Kolesnichenko and Valeriy Lashkov and Igor Mashek",
year = "2009",
month = jun,
day = "17",
language = "English",
isbn = "9789292212230",
series = "European Space Agency, (Special Publication) ESA SP",
booktitle = "Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles",
note = "6th European Symposium Aerothermodynamics for Space Vehicles ; Conference date: 03-11-2008 Through 06-11-2008",

}

RIS

TY - GEN

T1 - Interaction of a microwave-generated plasma with flow past a hemisphere cylinder at mach 2.1

AU - Knight, Doyle

AU - Brovkin, Vadim

AU - Khmara, Dmitri

AU - Kolesnichenko, Yuri

AU - Lashkov, Valeriy

AU - Mashek, Igor

PY - 2009/6/17

Y1 - 2009/6/17

N2 - The interaction of a microwave-generated plasma with a hemisphere cylinder at Mach 2.1 is simulated. The theoretical model is the unsteady threedimensional Euler equations for a multi- species reacting gas. The thermochemistry model for air incorporates 23 species and 238 reactions. The initial condition for the simulation is the steady flow past the hemisphere cylinder.A 9 GHz microwave pulse of 1.2 μs duration is focused upstream of the blunt body shock on the hemisphere cylinder centerline. The high temperature plasma region generated by the microwave pulse is convected to the hemisphere cylinder and interacts with the blunt body shock resulting in the momentary formation of a recirculation region and reduction in surface pressure on the hemisphere cylinder centerline. The computed surface pressure shows good agreement with experiment.

AB - The interaction of a microwave-generated plasma with a hemisphere cylinder at Mach 2.1 is simulated. The theoretical model is the unsteady threedimensional Euler equations for a multi- species reacting gas. The thermochemistry model for air incorporates 23 species and 238 reactions. The initial condition for the simulation is the steady flow past the hemisphere cylinder.A 9 GHz microwave pulse of 1.2 μs duration is focused upstream of the blunt body shock on the hemisphere cylinder centerline. The high temperature plasma region generated by the microwave pulse is convected to the hemisphere cylinder and interacts with the blunt body shock resulting in the momentary formation of a recirculation region and reduction in surface pressure on the hemisphere cylinder centerline. The computed surface pressure shows good agreement with experiment.

KW - CFD.

KW - Energy deposition

KW - Microwave

UR - http://www.scopus.com/inward/record.url?scp=66949133147&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:66949133147

SN - 9789292212230

T3 - European Space Agency, (Special Publication) ESA SP

BT - Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles

T2 - 6th European Symposium Aerothermodynamics for Space Vehicles

Y2 - 3 November 2008 through 6 November 2008

ER -

ID: 47780436