The Self-Induced Unsteadiness of Tip Leakage Vortex and Its Effect on Compressor Stall Inception.
類似資料:
1
国際会議録
The Self-Induced Unsteadiness of Tip Leakage Vortex and Its Effect on Compressor Stall Inception
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
2
テクニカルペーパー
A Study on the Mechanism of Tip Leakage Flow Unsteadiness in an Isolated Compressor Rotor.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
9
テクニカルペーパー
The Flow Mechanism of How Distorted Flows Deteriorate Stability of an Axial Flow Compressor.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
5
テクニカルペーパー
Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
12
テクニカルペーパー
Effects of Steady tip Clearance Asymmetry and Rotor Whirl on Stall Inception in an Axial Compressor.
American Society of Mechanical Engineers |