Experimental Blade Surface Pressures of a Supersonic Turbine for Rocket Engine Applications
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2003
- Pub. Year:
- 2003
- No.:
- 2003-4916
- Paper no.:
- 2003-4916
- Pages:
- 15
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Blade Surface Pressure Distributions in a Rocket Engine Turbine: Experimental Work with On-Blade Pressure Transducers
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Effects of Endwall Geometry and Stacking on Two-Stage Supersonic Turbine Performance.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Experimental Performance Evaluation of a Supersonic Turbine for Rocket Engine Applications
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 |
11
Technical Paper
Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Shape Optimization of Supersonic Turbines Using Response Surface and Neural Network Methods
American Institute of Aeronautics and Astronautics |