Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm
- 著者名:
- Weidong, Liu ( National University of Defence Technology, P.R. China )
- Zhenguo, Wang
- Jin, Zhou
- Fengchen, Zhuang
- 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:
- 96-3124
- ペーパー番号:
- 96-3124
- 開始ページ:
- 1
- 終了ページ:
- 11
- 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
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
テクニカルペーパー
Experiment and Numerical Simulation of Unsteady Temperature Fields in Automotive Catalytic Converters
Society of Automotive Engineering, Inc. |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Experiment and Numerical Simulation of Unsteady Temperature Fields in Automotive Catalytic Converters
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Global Model of Liquid Rocket Engine Combustion Instability Based on Chemistry Dynamics.
American Institute of Aeronautics and Astronautics |