Effect of the Mainstream Temperature History on the Heat Transfer Coefficient of a Gas Turbine Blade Tip by Transient IR Technique Jung Shin Park and Jae Su Kwak Asian-Pacific Conference on Aerospace Technology and Science May 20-23, 2015 Jeju, Korea

Effect of angle between the primary and auxiliary holes of an anti-vortex film cooling hole Younggi Moon, Soon Sang Park, Jung Shin Park, Jae Su Kwak 2014 Asia-Pacific International Symposium on Aerospace Technology September 24-26 Shanghai, China

Effect of Turbulence Intensity on the Film Cooling Effectiveness on a Flat Plate with Anti-vortex Holes Soon Sang Park, Jung Shin Park, Jae Su Kwak Asian Congress on Gas Turbines 2014 August 18-20 Seoul, Korea

Experimental Study on the Film Cooling Effectiveness on a Flat Plate with Anti-Vortex Holes Soon Sang Park, Jung Shin Park, Song-Gye Sung, Jae Su Kwak 2014 the Third International Conference on Fluid Dynamics and Thermodynamics Technologies April 21-23 Antalya, Turkey

Measurement of Blade Tip Heat Transfer and Leakage Flow in a Turbine Cascade with Multi-Cavity Squealer Tip Jung Shin Park, Sang Hoon Lee, Won Suk Lee, Jin Taek Chung, Jae Su Kwak ASME 2013 Turbine Blade Tip Symposium and Course September 30 - October 3 Hamburg, Germany

Effect of Inlet Velocity Profile and Rotating Number on Flow Structure in the Rotating Channel with Rib Structure Dae-Hyun Kim, Ahmad Fikri Bin Mustaffa, Jin-Taek Chung, and Jung Shin Park, and Jae Su Kwak 21st International Society of Air Breathing Engine Conference September 9-13, 2013 Busan, Korea

Measurement of Blade Tip Heat Transfer and Secondary Flow in a Linear Cascade with Multi-Cavity Tip Sang Hoon Lee, Jung Shin Park, and Jae Su Kwak 21st International Society of Air Breathing Engine Conference September 9-13, 2013 Busan, Korea

Effect of the rib configuration in the squealer tip cavity of a gas turbine blade on the secondary flow in a linear cascade Sang Hoon Lee, Jung Shin Park, and Jae Su Kwak The Fifth International Symposium on Fluid Machinery and Fluids Engineering Octorber 24-27, 2012 Jeju, Korea

Effect of blade tip cavity geometry on aerodynamic efficiency and heat transfer performance of gas turbine Jung Shin Park, Won Suk Lee, Jin Taek Chung, and Jae Su Kwak The Eighth KSME-JSME Thermal and Fluids Engineering Conference March 18-21, 2012 Incheon, Korea

Effect of squealer tip geometry with multi-cavity on the heat transfer and flow near the blade tip region of the gas turbine Won Suk Lee, Dae Hyeon Kim, Jung Shin Park, Jae Su Kwak, and Jin Taek Chung Asian Joint Conference on Propulsion and Power March 1-4, 2012 Xi’an, China