Heat transfer augmentation in a 2:1 ribbed channel using 3-dimensional partial blockages APISAT 2017 October 16-18 Seoul Olympic Parktel, Seoul, Korea
Numerical study on the Improvement of the Film Cooling Effectiveness of an Inclined Slot using a Protrusion near exit Asian Conference on Thermal Sciences, ACTS2017 April 26 -May 01 Jeju, Republic of Korea
Measurement of Film cooling Effectiveness for the First-Stage Vane and Endwalll of a Gas Turbine with Fan-shaped Holes ASME Turbo Expo 2017 June 26-30 Charlotte, NC USA
Heat Transfer Augmentation in a 2:1 Ribbed Channel Using Non-uniform Inlet Flow Asian Congress on Gas Turbines, ACGT2016 November 14-16 Indian Institute of Technology Bombay, Mumbai, India
Enhancement of Heat Transfer Coefficient in a 2:1 Ribbed Channel Using Partial Flow Blockage Asian Joint Symposium on Aerospace Engineering May 18-21, 2016 Jeju, Korea
Study on the heat trasnfer characteristics in the 2:1 ribbed channel with the dimple and protrusion compound cooling technique 7th International Symposium on Fluid Machinery and Fluids Engineering October 18-22, 2016 Jeju, Korea
Experimental Investigation on the Effect of Plasma Actuator on a Flat Plate Film Cooling International Symposium on Transport Phenomena and Dynamics of Rotating Machinery April 11-15, 2016 Honolulu, USA
Application of DBD Plasma to the Film Cooling on a Flat Plate with a Rectangular Slot 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 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 Asian-Pacific Conference on Aerospace Technology and Science May 20-23, 2015 Jeju, Korea