Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge.
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American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge.
American Society of Mechanical Engineers |
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Effect of coolant injection on heat transfer for a simulated turbine airfoil leading edge
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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The Effects of Obstructions on Film Cooling Effectiveness on the Suction Side of a Gas Turbine Vane.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Turbine Airfoil Net Heat Flux Reduction with Cylindrical Holes Embedded in a Transverse Trench.
American Society of Mechanical Engineers |
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CFD Predictions of the Frequency Dependence of Pulsed Film Cooling Heat Flux on a Turbine Blade Leading Edge
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |