Suppression of Instabilities in Gaseous Fuel High- Pressure Combustor Using Non- Coherent Oscillatory Fuel Injection.

Suppression of Instabilities in Gaseous Fuel High- Pressure Combustor Using Non- Coherent Oscillatory Fuel Injection.

著者名:

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : GT

シリーズ巻号:

2003

発行年:

2003

通号:

GT2003-38103

ペーパー番号:

GT2003-38103

総ページ数:

10

出版情報:

New York, NY: American Society of Mechanical Engineers

言語:

英語

請求記号:

A11800

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001749
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2003
回次:	2003
会議開催地:	Atlanta, Georgia, USA
会議開催年:	2003.06.16-2003.06.19
論文注記:	ASME Turbo Expo 2003, Atlanta, Georgia, USA, 16-19 June 2003

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2 テクニカルペーパー Active Control of Instabilities in High-Pressure Combustor by Non-Coherent Oscillatory Fuel Injection Lubarsky, E., Scherbik, D., Zinn, B.T. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Suppression of Combustion Instabilities in a Liquid Fuel Combustor Using a Fast Adaptive Control Algorithm Johnson, C.E., Neumeier, Y., Lubarsky, E., Lee, J.Y., Neumaier, M., Zinn, B.T. American Institute of Aeronautics and Astronautics
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