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
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