Heat transfer and flow characteristics of an engine representative impingement cooling system C Son, D Gillespie, P Ireland, GM Dailey J. Turbomach. 123 (1), 154-160, 2001 | 77 | 2001 |
An investigation of cross-corrugated heat exchanger primary surfaces for advanced intercooled-cycle aero engines (Part-I: Novel geometry of primary surface) JH Doo, MY Ha, JK Min, R Stieger, A Rolt, C Son International Journal of Heat and Mass Transfer 55 (19-20), 5256-5267, 2012 | 74 | 2012 |
An investigation of the application of roughness elements to enhance heat transfer in an impingement cooling system C Son, G Dailey, P Ireland, D Gillespie Turbo Expo: Power for Land, Sea, and Air 47268, 465-479, 2005 | 59 | 2005 |
An investigation of cross-corrugated heat exchanger primary surfaces for advanced intercooled-cycle aero engines (Part-II: Design optimization of primary surface) JH Doo, MY Ha, JK Min, R Stieger, A Rolt, C Son International journal of heat and mass transfer 61, 138-148, 2013 | 52 | 2013 |
Comparative study on steady and unsteady conjugate heat transfer analysis of a high pressure turbine blade S Hwang, C Son, D Seo, DH Rhee, B Cha Applied Thermal Engineering 99, 765-775, 2016 | 47 | 2016 |
A full engine cycle analysis of a turbofan engine for optimum scheduling of variable guide vanes S Kim, D Kim, C Son, K Kim, M Kim, S Min Aerospace Science and Technology 47, 21-30, 2015 | 43 | 2015 |
Numerical study on characteristics of flow and heat transfer in a cooling passage with protrusion-in-dimple surface JE Kim, JH Doo, MY Ha, HS Yoon, C Son International journal of heat and mass transfer 55 (23-24), 7257-7267, 2012 | 40 | 2012 |
A new transient performance adaptation method for an aero gas turbine engine S Kim, K Kim, C Son Energy 193, 116752, 2020 | 37 | 2020 |
Theoretical prediction of longitudinal heat conduction effect in cross-corrugated heat exchanger JH Doo, MY Ha, JK Min, R Stieger, A Rolt, C Son International Journal of Heat and Mass Transfer 55 (15-16), 4129-4138, 2012 | 35 | 2012 |
Three-dimensional unsteady simulation of a multistage axial compressor with labyrinth seals and its effects on overall performance and flow characteristics S Kim, K Kim, C Son Aerospace Science and Technology 86, 683-693, 2019 | 32 | 2019 |
Combining effect of optimized axial compressor variable guide vanes and bleed air on the thermodynamic performance of aircraft engine system S Kim, C Son, K Kim Energy 119, 199-210, 2017 | 29 | 2017 |
Full surface heat transfer characteristics of rotor ventilation duct of a turbine generator W Yoo, S Jeon, C Son, J Yang, D Ahn, S Kim, K Hwang, S Ha Applied thermal engineering 94, 385-394, 2016 | 29 | 2016 |
U-bend shaped turbine blade cooling passage optimization H Namgoong, C Son, P Ireland 12th AIAA/ISSMO multidisciplinary analysis and optimization conference, 5926, 2008 | 29 | 2008 |
Comparative study between a cut-back and conventional trailing edge film cooling system JC Telisinghe, PT Ireland, TV Jones, D Barrett, C Son Turbo Expo: Power for Land, Sea, and Air 4238, 983-993, 2006 | 29 | 2006 |
Study on the performance of a centrifugal compressor considering running tip clearance C Kim, H Lee, J Yang, C Son, Y Hwang International Journal of Refrigeration 65, 92-102, 2016 | 24 | 2016 |
Adaptation method for overall and local performances of gas turbine engine model S Kim, K Kim, C Son International Journal of Aeronautical and Space Sciences 19, 250-261, 2018 | 23 | 2018 |
Cooling arrangement RM Townes, C Son, C Young US Patent 7,207,776, 2007 | 22 | 2007 |
The effect of roughness element fillet radii on the heat transfer enhancement in an impingement cooling system C Son, P Ireland, D Gillespie Turbo Expo: Power for Land, Sea, and Air 47268, 263-273, 2005 | 21 | 2005 |
Transient system simulation for an aircraft engine using a data-driven model S Kim, K Kim, C Son Energy 196, 117046, 2020 | 18 | 2020 |
Heat transfer and flow characteristics of an engine representative impingement cooling system C Son, D Gillespie, P Ireland, GM Dailey Turbo Expo: Power for Land, Sea, and Air 78569, V003T01A027, 2000 | 18 | 2000 |