Effect of angle between the primary and auxiliary holes of an anti-vortex film cooling hole 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 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 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 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 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 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 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 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 Asian Joint Conference on Propulsion and Power March 1-4, 2012 Xi’an, China
Heat Transfer Augmentation by Rib-Dimple Compound Cooling Technique AIAC14 Fourteenth Australian International Aerospace Congress 28 February - 3 March 2011 Melbourne, Australia