Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine

Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine

著者名:

Zhou, Jin ( National University of Defense Technology, P.R. China )
Hu, Xiaoping
Huang, Yuhui
Wang, Zhenguo

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

1996

発行年:

1996

通号:

96-3135

ペーパー番号:

96-3135

開始ページ:

1

終了ページ:

7

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050840
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	32nd
会議開催地:	Lake Buena Vista, FL
会議開催年:	1996.07.01-1996.07.03
論文注記:	32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 1-3, 1996/Lake Buena Vista, FL

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1 テクニカルペーパー Acoustic model for the self-oscillation of coaxial swirl injector Yuhui, Huang, Jin, Zhou, Xiaoping, Hu, Zhenguo, Wang American Institute of Aeronautics and Astronautics	7 テクニカルペーパー The characteristics of acoustic waves and acoustic cavities to combustion instability Jin, Zhou, Yuhui, Huang, Zhenguo, Wang American Institute of Aeronautics and Astronautics
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3 テクニカルペーパー Nonlinear Thermodynamic Analyses of Combustion Instability in Rocket Engine Yuhui, HUANG, Zhenguo, WANG, Jin, ZHOU American Institute of Aeronautics and Astronautics	9 テクニカルペーパー The optimization of boundary layer trip in advanced chambers Zhenguo, Wang, Yuhui, Huang, Jin, Zhou, Zhongguang, Zhang American Institute of Aeronautics and Astronautics
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5 テクニカルペーパー A Nonlinear Analytical Model of High-Frequency Combustion Instability in Rocket Engine Zhenguo, WANG, Yuhui, HUANG, Jin, ZHOU American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics. Yuhui, H., Wentao, Z., Zhenguo, W., Jin, Z. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental studies on atomization and flux distributions of gas-liquid coaxial injectors Hu, Xiaoping, Zhou, Jin, Wang, Zhenguo, Zhong, Liangsheng American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Experimental investigation on characteristics of tripropellant injectors Chibing, Shen, Chunlin, Jiang, Hui, Chen, Jin, Zhou, Zhenguo, Wang American Institute of Aeronautics and Astronautics

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