Improvement of Inlet Flow Characteristics of LE-7A Liquid Hydrogen Pump.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-4161
- Paper no.:
- 2002-4161
- Pages:
- 9
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Improvements of Inducer Inlet Backflow Characteristics Using 3-D Inverse Design Method.
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Numerical Analysis of Flow-Induced Structural Vibration in the LE-7A Liquid Hydrogen Pump
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Firing Tests of a Liquid-Hydrogen-Cooling Scramjet Engine in the Ramjet Engine Test Facility 2nd
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Engine Performance and Exhaust Characteristics of Direct-Injection Diesel Engine Operated with DME
Society of Automotive Engineers |
4
Technical Paper
Elastodynamic Analysis of Fluid-Induced Vibration in the LE-7A Liquid Hydrogen Pump
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 |
American Institute of Aeronautics and Astronautics |