
-
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

성균관대학교 박사과정
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

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