Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › Рецензирование
Interaction of microwave-generated plasma with a blunt body at Mach 2.1. / Knight, Doyle; Kolesnichenko, Yuri F.; Brovkin, Vadim; Khmara, Dmitri; Lashkov, Valery; Mashek, Igor.
47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2009. 2009-0846 (47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition).Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › Рецензирование
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TY - GEN
T1 - Interaction of microwave-generated plasma with a blunt body 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 su- personic 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 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 su- personic 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 experiment. The interaction of the microwave-generated plasma with the flowfield structure is examined.
UR - http://www.scopus.com/inward/record.url?scp=78549233746&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:78549233746
SN - 9781563479694
T3 - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
BT - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
T2 - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Y2 - 5 January 2009 through 8 January 2009
ER -
ID: 47780161