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    박상현석사(2020)

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

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    서현재석사(2019)

    한화에어로스페이스

    Numerical Study on the Optimization of Laidback Fan-Shaped Film Cooling Hole

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    최정욱석사(2018)

    두산중공업

    Numerical Study on the Film Cooling Effectiveness of a Gas Turbine Using Protrusions

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    장한나석사(2018)

    한화에어로스페이스

    Study on the Heat Transfer Characteristics of Turbine Blade Internal Passage through the Configuration and Arrangement of Protrusions

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    김예지석사(2017)

    두산중공업

    Improvement of Film Cooling Effectiveness Using Various Film Cooling Holes and Dielectric Barrier Discharge Plasma

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    박정신박사(2017)

    두산중공업

    Effect of Gas Turbine Blade Tip Shape on Secondary Flow and Tip Heat Transfer

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    문영기석사(2015)

    두산중공업

    Effect of the Angle and the Location of Auxiliary Holes on the Performance of the Anti-vortex Film Cooling Hole

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    박순상석사(2015)

    한화에어로스페이스

    Experimental investigation on the effect of turbulence intensity on the film cooling effectiveness of anti-wortex holes

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    이상훈석사(2014)

    젠틀몬스터

    Effect of Double Cavity Gas Turbine Blade Tip on Secondary Flow and Tip Heat Transfer

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    이용진박사(2012)

    국방기술품질원

    Turbine Cascade 3-D Flow Measurement (5-Hole Probe) Blade Heat Transfer measurement (TLC Technique)