On the Impact of Blade Count Reduction on Aerodynamic Performance and Loss Generation in a Three-Stage LP Turbine.
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American Society of Mechanical Engineers |
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Performance analysis of a turbine stage having cooled nozzle blades with trailing edge ejection
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
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Performance Improvement and Noise Reduction through Vane and Blade Indexing of a Two-Stage Turbine
American Institute of Aeronautics and Astronautics |
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Aerodynamic Measurements in a Liner Turbine Blade Passage with Three-Dimensional Endwall Contouring.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |