강영준박사(2024)

박사 후 연구원

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

김혁제석사(2024)

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

조예림석사(2024)

한화에어로스페이스

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

정진영박사(2023)

한화에어로스페이스

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

강민석석사(2023)

페리지에어로스페이스

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

김기문박사(2022)

한국항공우주연구원

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

김영서석사(2022)

삼성전자

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

송유진석사(2022)

국방기술품질원

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

이수인석사(2021)

현대자동차

Parametric Study on the Sealing Performance of Solid and Honeycomb Labyrinth Seals

박상현석사(2020)

삼성전자 DS

A Study on the Effect of Fan-Shaped Film Cooling Hole Shape and Manufacturing Tolerance on Film Coolimg Effectiveness