Analysis of a Highly Loaded, Transonic, Inlet Compressor Stage: Isolated and Multi-stage Performance
- Author(s):
- Car, D. ( Air Force Research Laboratory WPAFB )
- Puterbaugh, S. L.
- Chriss, R. M.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-3206
- Paper no.:
- 00-3206
- Page(from):
- 1
- Page(to):
- 9
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
The Influence of Compressor Blade Row Interaction Modeling on Performance Estimates from Time-Accurate, Multi-Stage, Navier-Stokes Simulations.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Control of shock structure and secondary flow field inside transonic compressor rotors through aerodynamic sweep
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
3
Technical Paper
Effect of a mismatch between the buttons of variable stator vanes and the flowpath in a highly loaded transonic compressor stage
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
An Investigation of Wake-Shock Interactions in a Transonic Compressor with DPIV and Time-Accurate CFD.
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |