The Influence of Variable Rotor-Stator Interaction on Boundary-Layer Development in an Axial Compressor.
類似資料:
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
3
テクニカルペーパー
Design of a Low Solidity-Flow-Controlled Stator with Coanda Surface in a High Speed Compressor.
American Society of Mechanical Engineers |
9
テクニカルペーパー
Tip Clearance Vortex Development and Shock-Vortex-Interaction in a Transonic Axial Compressor Rotor.
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
11
テクニカルペーパー
Stator averaged, rotor blade-to-blade near wall flow in a multistage axial compressor with tip clearance variation
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |