Turbine Blade Tip Leakage Flow Control: Thick/Thin Blade Effects and Separation Line Studies.
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Conference Proceedings
Turbine Blade Tip Leakage Flow Control: Thick/Thin Blade Effects and Separation Line Studies
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Turbine Blade Tip Leakage Flow Control by Partial Squealer Tip and Plasma Actuators
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Effects of Steady tip Clearance Asymmetry and Rotor Whirl on Stall Inception in an Axial Compressor.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Tip Clearance Flow Visualization of a Turbine Blade Cascade with Active and Passive Flow Control.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A Transonic Axial Compressor Facility for Fundamental Research and Flow Control Development
American Institute of Aeronautics and Astronautics |