GE Korea
Heat Transfer Measurement on the Internal Coolant Passage of Gas Turbine Blade
두산에너빌리티
Measurement of the Heat Transfer Coefficient in the Rotating Dimpled Channel
Stackpole Powertrain International
Heat Transfer Measurement on the Internal Coolant Passage of Gas Turbine Blade
한화에어로스페이스
Effect of Turbine Blade Tip Shape on Aerodynamics Loss and Tip Heat Transfer of a Linear Turbine Cascade
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Measurement of the Film Cooling Effectiveness on Flat Plate and Heat Transfer Coefficient in the Rotating rectangular channel with Dimple
한전기술
Effect of Various Blade Tip on the Aerodynamic Loss of a Turbine Cascade
국방과학연구소
Measurement of Heat Transfer Coefficients in Gas Turbine Blade Using Improved Transient Liquid Crystal Technique