Publication

International conference

  • 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

  • Heat Transfer Augmentation by Rib-Dimple Compound Cooling Technique Yong Duck Choi, Seok Beom Kim, Eun Yeong Choi, Yong Jin Lee, and Jae Su Kwak AIAC14 Fourteenth Australian International Aerospace Congress 28 February - 3 March 2011 Melbourne, Australia

  • Effect of channel orientation on the distribution of the heat transfer coefficient in smooth and dimpled rotating rectangular channels Seokbeom Kim, Eun Yeong Choi, and Jae Su Kwak IMECE2010 November 12-18 Vancouver, British Columbia, Canada

  • Effect of Inclined Blade Tip on the Aerodynamic Loss of a Turbine Cascade Jae Su Kwak, S.D.Park, Y.C.Nho ,and Y. JUN The 2nd International Conference on Advanced Materials and Structures October 28-31 Nanjing, P.R.China

  • Measurement of the Film Cooling Effectiveness on a Flat Plate using Pressure Sensitive Paint S. D. Park and K. S. Lee, J. S. Kwak, B. J. Cha AJCPP 2008 March 6-8 Gyeongju, Korea