Computational analysis of LOX/GH2 rocket engine
- Author(s):
- Zhenguo, Wang ( National University of Defence Technology, P.R. China )
- Weidong, Liu
- Xiaoqing, Yan
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-3132
- Paper no.:
- 96-3132
- Page(from):
- 1
- Page(to):
- 10
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm
American Institute of Aeronautics and Astronautics |
7
Technical Paper
A Nonlinear Analytical Model of High-Frequency Combustion Instability in Rocket Engine
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Numerical analysis model for radial combustion instability in liquid propellant engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Three-Dimension Numerical Simulation of Combustion Processes in LH2/LOX Rocket Engines
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Three-dimension numerical simulation of combustion processes in LH2/LOX rocket engines
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Research on Temperature and Strain Rate Dependent Viscoelastic Response of Polyvinyl Butaral Film
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Cracking Failure Analysis and Optimization on Exhaust Manifold of Engine with CFD-FEA Coupling
Society of Automotive Engineers |