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Study on the Internal Heat Transfer Characteristic in a Rotating 2-Pass Channel (AR=1) at Engine-Similar Conditions

두산에너빌리티
Improvement of Film Cooling Effectiveness Using Keyhole Slot on Crossflow-fed Film Cooling Hole

두산에너빌리티
Study on the Heat Transfer Characteristic of Gas Turbine Blades through the Interaction of Internal Cooling Channels and Film Cooling Holes

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Study on the Improving Aerothermal Performance by Optimizing a Shape of Honeycomb labyrinth seal of a Gas Turbine

한화에어로스페이스
Experimental Study on the Optimization of Fan-Shaped Hole and the Superposition Effect of Film Cooling Effectiveness

한화에어로스페이스
Study on the Film Cooling Effectiveness of a Butterfly Shaped Hole Configuration of a Gas Turbine

페리지에어로스페이스
A Study on Film Cooling Performance for Various Hole Shapes Applied to Vane under High Speed Condition

한국항공우주연구원
An Experimental Study on Aerodynamic Loss of a Gas Turbine Trailing Edge and Film Cooling of Shroud and Vane

삼성전자
A Study on the Effect of Expansion Length Ratio and Arrangement on FIlm Cooling Performance of Fan-Shaped Hole

국방기술품질원
A Study on the Exit Shape of Fan-shaped Holes on the Film Cooling Effectiveness