| Experimental optimization of a fan-shaped film cooling hole with 30 degrees-injection angle and 6-hole length-to-diameter ratio SH Park, YJ Kang, HJ Seo, JS Kwak, YS Kang International Journal of Heat and Mass Transfer 144, 118652, 2019 | 66 | 2019 |
| Tip clearance effect on through-flow and performance of a centrifugal compressor HJ Eum, YS Kang, SH Kang KSME International Journal 18, 979-989, 2004 | 34 | 2004 |
| Prediction of the nonuniform tip clearance effect on the axial compressor flow field YS Kang, SH Kang | 31 | 2010 |
| Experimental and numerical study on the effect of fan-shaped hole configuration on film cooling effectiveness HJ Seo, SH Park, JS Kwak, YS Kang Turbo Expo: Power for Land, Sea, and Air 58653, V05BT19A013, 2019 | 30 | 2019 |
| Multi-stage turbocharger system analysis method for high altitude UAV engine YS Kang, BJ Lim, BJ Cha Journal of Mechanical Science and Technology 31, 2803-2811, 2017 | 28 | 2017 |
| Partial admission, axial impulse type turbine design and partial admission radial turbine test for SCO2 cycle H Shin, J Cho, YJ Baik, J Cho, C Roh, HS Ra, Y Kang, J Huh Turbo Expo: Power for Land, Sea, and Air 50961, V009T38A019, 2017 | 27 | 2017 |
| Film Cooling Performance Improvement With Optimized Hole Arrangements on Pressure Side Surface of Nozzle Guide Vane: Part II—Experimental Validation DH Rhee, YS Kang, BJ Cha, JS Kang, S Lee, K Yee Turbo Expo: Power for Land, Sea, and Air 49804, V05CT12A011, 2016 | 26 | 2016 |
| Multi disciplinary design optimization and performance evaluation of a single-stage transonic axial compressor YS Kang, TC Park, SS Yang, SI Lee, DH Lee Turbo Expo: Power for Land, Sea, and Air 44748, 361-369, 2012 | 26 | 2012 |
| Optimization of a high pressure turbine blade tip cavity with conjugate heat transfer analysis J Kim, YS Kang, D Kim, J Lee, BJ Cha, J Cho Journal of Mechanical Science and Technology 30, 5529-5538, 2016 | 23 | 2016 |
| Reliability-based design optimization of axial compressor using uncertainty model for stall margin S Hong, S Lee, S Jun, DH Lee, H Kang, YS Kang, SS Yang Journal of mechanical science and technology 25, 731-740, 2011 | 23 | 2011 |
| Aerodynamic design of high pressure turbine for aircraft turbofan engine YS Kang, DH Rhee, BJ Cha Proceeding of the 7th National Congress on Fluids Engineering, 246-247, 2012 | 20 | 2012 |
| Numerical study of roughness effects on a turbine stage performance YS Kang, JC Yoo, SH Kang Turbo Expo: Power for Land, Sea, and Air 41707, 1267-1274, 2004 | 19 | 2004 |
| Overall cooling effectiveness measurements on pressure side surface of the nozzle guide vane with optimized film cooling hole arrangements DH Rhee, YS Kang, BJ Cha, S Lee Turbo Expo: Power for Land, Sea, and Air 50879, V05AT10A001, 2017 | 18 | 2017 |
| Effects of inlet turbulence conditions and near-wall treatment methods on heat transfer prediction over gas turbine vanes JG Bak, J Cho, S Lee, YS Kang International Journal of Aeronautical and Space Sciences 17 (1), 8-19, 2016 | 18 | 2016 |
| Numerical Study on Blade Roughness Effect on the performance of turbomachines SH Kang, YS Kang, KH Han Proceedings International Gas Turbine Congress, Tokyo, Japan, 2-7, 2003 | 17 | 2003 |
| Large Eddy Simulation on Film Cooling Flow from a Fan-Shaped Cooling Hole on a Flat Plate YS Kang, S Jun, DH Rhee The KSFM Journal of Fluid Machinery 21 (6), 1-9, 2018 | 16 | 2018 |
| Establishment of multi-stage turbocharger layout for HALE UAV engine and its performance assessment YS Kang, BJ Lim, JK Kim The KSFM Journal of Fluid Machinery 18 (6), 31-36, 2015 | 16 | 2015 |
| Apparatus for preventing axial-flow compressor from stalling by employing casing treatment BJ Lim, TC Park, YS Kang US Patent 10,378,550, 2019 | 14 | 2019 |
| Design, Flow Simulation, and Performance Test for a Partial-Admission Axial Turbine Under Supercritical CO2 Condition J Cho, H Shin, J Cho, YJ Baik, B Choi, C Roh, HS Ra, Y Kang, J Huh Turbo Expo: Power for Land, Sea, and Air 51180, V009T38A019, 2018 | 14 | 2018 |
| A study on the numerical analysis methodology for thermal and flow characteristics of high pressure turbine in aircraft gas turbine engine J Kim, J Bak, Y Kang, L Cho, J Cho The KSFM Journal of Fluid Machinery 17 (3), 46-51, 2014 | 14 | 2014 |
