서현재석사(2019)

한화에어로스페이스

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

최정욱석사(2018)

한화에어로스페이스

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

장한나석사(2018)

현대모비스

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

김예지석사(2017)

두산에너빌리티

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

박정신박사(2017)

한화에어로스페이스

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

문영기석사(2015)

두산에너빌리티

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

박순상석사(2015)

두산에너빌리티

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

이상훈석사(2014)

젠틀몬스터

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

이용진박사(2012)

국방기술진흥연구소

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

최은영석사(2011)

국방과학연구소

Rotating Turbine Blade Internal Heat Transfer Measurement CFD for Internal Heat Transfer of Rotating Turbine Blade