A Study on Film Cooling Performance for Various Hole Shapes Applied to Vane under High Speed Condition
한국항공대학교 항공우주및기계공학부 연구교수
An Experimental Study on Aerodynamic Loss of a Gas Turbine Trailing Edge and Film Cooling of Shroud and Vane
삼성전자 DS
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
현대자동차
Parametric Study on the Sealing Performance of Solid and Honeycomb Labyrinth Seals
삼성전자 DS
A Study on the Effect of Fan-Shaped Film Cooling Hole Shape and Manufacturing Tolerance on Film Coolimg Effectiveness
한화에어로스페이스
Numerical Study on the Optimization of Laidback Fan-Shaped Film Cooling Hole
두산중공업
Numerical Study on the Film Cooling Effectiveness of a Gas Turbine Using Protrusions
현대모비스
Study on the Heat Transfer Characteristics of Turbine Blade Internal Passage through the Configuration and Arrangement of Protrusions
두산중공업
Improvement of Film Cooling Effectiveness Using Various Film Cooling Holes and Dielectric Barrier Discharge Plasma