Acoustic model for the self-oscillation of coaxial swirl injector
- Author(s):
- Yuhui, Huang ( National University of Defense Technology, P.R. China )
- Jin, Zhou
- Xiaoping, Hu
- Zhenguo, Wang
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 1997
- Pub. Year:
- 1997
- No.:
- 97-3328
- Paper no.:
- 97-3328
- Page(from):
- 1
- Page(to):
- 7
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Experimental studies on atomization and flux distributions of gas-liquid coaxial injectors
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
The characteristics of acoustic waves and acoustic cavities to combustion instability
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
The Characteristics of Acoustic Waves and Acoustic Cavities to Combustion Instability
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
A Nonlinear Analytical Model of High-Frequency Combustion Instability in Rocket Engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |