Loss Reduction in Compressor Cascades by Means of Passive Flow Control.
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American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Control of Secondary Flow in a High Loaded Compressor Stage by Means of a Groove Structure on the Sidewalls
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
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Reduction of secondary flow losses in turbine cascades by leading edge modifications at the endwall
American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
American Society of Mechanical Engineers |
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Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor.
American Society of Mechanical Engineers |