Application of DBD Plasma to the Film Cooling on a Flat Plate with a Rectangular Slot Ye Jee Kim, Gi Mun Kim, Myung Ho Kim, Jae Su Kwak ASME 2016 Turbo Expo Poster Session June 13-17 Seoul, South Korea

Heat Transfer and Aerodynamic Loss near a Gas Turbine Blade Tip with a Partial Cavity Jung Shin Park, Jae Su Kwak, and Ki Don Lee ASME 2016 Turbo Expo Poster Session June 13-17 Seoul, South Korea

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