The Effect of Coolant Injection on the Endwall Flow of a High Pressure Turbine.
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American Society of Mechanical Engineers |
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American Institute of Aeronautics and Astronautics |
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Effect of the Hub Endwall Cavity Flow on the Flow-Field of a Transonic High-Pressure Turbine.
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Effect of the Leakage Flows and the Upstream Platform Geometry of the Endwall Flows of a Turbine Cascade.
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Effect of Tip and Pressure Side Coolant Injection on Heat Transfer Distributions for a Plane and Recessed Tip.
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