Numerical Investigation of Autoignition Regionin a Supersonic Combustor

The present paper deals with the numerical investigation of autoignition region between a backward-facing step and perpendicular wall injectors in a supersonic combustor. A series of simulation changing the dynamic pressure ratio of the injectant to the main stream is carried out. Wall pressure prof...

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Veröffentlicht in:	JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2002, Vol.50(580), pp.181-181
Hauptverfasser:	Takase, Kazuo, Matsuo, Akiko, Tomioka, Sadatake, Mitani, Tohru
Format:	Artikel
Sprache:	eng ; jpn
Schlagworte:	Autoignition Region Compressible Flows Internal Flows Numerical Simulation Supersonic Combustor
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