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

в: AIAA Journal, Том 47, № 12, 01.12.2009, стр. 2996-3010.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Knight, D, Kolesnichenko, YF, Brovkin, V, Khmara, D, Lashkov, V & Mashek, I 2009, 'Interaction of microwave-generated plasma with a hemisphere cylinder at mach 2.1', AIAA Journal, Том. 47, № 12, стр. 2996-3010. https://doi.org/10.2514/1.43657

APA

Knight, D., Kolesnichenko, Y. F., Brovkin, V., Khmara, D., Lashkov, V., & Mashek, I. (2009). Interaction of microwave-generated plasma with a hemisphere cylinder at mach 2.1. AIAA Journal, 47(12), 2996-3010. https://doi.org/10.2514/1.43657

Vancouver

Knight D, Kolesnichenko YF, Brovkin V, Khmara D, Lashkov V, Mashek I. Interaction of microwave-generated plasma with a hemisphere cylinder at mach 2.1. AIAA Journal. 2009 Дек. 1;47(12):2996-3010. https://doi.org/10.2514/1.43657

Author

Knight, Doyle ; Kolesnichenko, Yuri F. ; Brovkin, Vadim ; Khmara, Dmitri ; Lashkov, Valery ; Mashek, Igor. / Interaction of microwave-generated plasma with a hemisphere cylinder at mach 2.1. в: AIAA Journal. 2009 ; Том 47, № 12. стр. 2996-3010.

BibTeX

@article{c50ac6cf495b42f8b0a41bddc3f021d2,
title = "Interaction of microwave-generated plasma with a hemisphere cylinder at mach 2.1",
abstract = "Microwave energy deposition is a novel method for flow control in high-speed flows. Experiments have demonstrated its capability for beneficial flowfield modification in supersonic flow including, for example, drag reduction for blunt bodies. A fully three-dimensional, time-accurate gas dynamic code has been developed for simulating microwave energy deposition in air and the interaction of the microwave-generated plasma with the supersonic flow past a blunt body. The thermochemistry model includes 23 species and 238 reactions. The code is applied to the simulation of microwave energy deposition in supersonic flow past a hemisphere cylinder. The computed centerline surface pressure is compared with the experiment. The interaction of the microwave-generated plasma with the flowfield structure is examined.",
author = "Doyle Knight and Kolesnichenko, {Yuri F.} and Vadim Brovkin and Dmitri Khmara and Valery Lashkov and Igor Mashek",
year = "2009",
month = dec,
day = "1",
doi = "10.2514/1.43657",
language = "English",
volume = "47",
pages = "2996--3010",
journal = "AIAA Journal",
issn = "0001-1452",
publisher = "The American Institute of Aeronautics and Astronautics",
number = "12",

}

RIS

TY - JOUR

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

AU - Knight, Doyle

AU - Kolesnichenko, Yuri F.

AU - Brovkin, Vadim

AU - Khmara, Dmitri

AU - Lashkov, Valery

AU - Mashek, Igor

PY - 2009/12/1

Y1 - 2009/12/1

N2 - Microwave energy deposition is a novel method for flow control in high-speed flows. Experiments have demonstrated its capability for beneficial flowfield modification in supersonic flow including, for example, drag reduction for blunt bodies. A fully three-dimensional, time-accurate gas dynamic code has been developed for simulating microwave energy deposition in air and the interaction of the microwave-generated plasma with the supersonic flow past a blunt body. The thermochemistry model includes 23 species and 238 reactions. The code is applied to the simulation of microwave energy deposition in supersonic flow past a hemisphere cylinder. The computed centerline surface pressure is compared with the experiment. The interaction of the microwave-generated plasma with the flowfield structure is examined.

AB - Microwave energy deposition is a novel method for flow control in high-speed flows. Experiments have demonstrated its capability for beneficial flowfield modification in supersonic flow including, for example, drag reduction for blunt bodies. A fully three-dimensional, time-accurate gas dynamic code has been developed for simulating microwave energy deposition in air and the interaction of the microwave-generated plasma with the supersonic flow past a blunt body. The thermochemistry model includes 23 species and 238 reactions. The code is applied to the simulation of microwave energy deposition in supersonic flow past a hemisphere cylinder. The computed centerline surface pressure is compared with the experiment. The interaction of the microwave-generated plasma with the flowfield structure is examined.

UR - http://www.scopus.com/inward/record.url?scp=73549092478&partnerID=8YFLogxK

U2 - 10.2514/1.43657

DO - 10.2514/1.43657

M3 - Article

AN - SCOPUS:73549092478

VL - 47

SP - 2996

EP - 3010

JO - AIAA Journal

JF - AIAA Journal

SN - 0001-1452

IS - 12

ER -

ID: 47780284