| A review of impinging jets during rocket launching C Jiang, T Han, Z Gao, CH Lee Progress in Aerospace Sciences 109, 100547, 2019 | 59 | 2019 |
| Combustion heat-release effects on supersonic compressible turbulent boundary layers Z Gao, C Jiang, S Pan, CH Lee AIAA Journal 53 (7), 1949-1968, 2015 | 58 | 2015 |
| Improvement and application of wall function boundary condition for high-speed compressible flows ZX Gao, CW Jiang, CH Lee Science China Technological Sciences 56, 2501-2515, 2013 | 48 | 2013 |
| On the laminar finite rate model and flamelet model for supersonic turbulent combustion flows Z Gao, C Jiang, CH Lee International Journal of Hydrogen Energy 41 (30), 13238-13253, 2016 | 33 | 2016 |
| Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine Z Gao, J Wang, C Jiang, C Lee Combustion Theory and Modelling 18 (6), 652-691, 2014 | 33 | 2014 |
| Representative interactive flamelet model and flamelet/progress variable model for supersonic combustion flows Z Gao, C Jiang, CH Lee Proceedings of the Combustion Institute 36 (2), 2937-2946, 2017 | 28 | 2017 |
| An in-depth numerical investigation of a supersonic cavity-ramp flow with DDES method Z Wu, Z Gao, C Jiang, C Lee Aerospace Science and Technology 89, 253-263, 2019 | 21 | 2019 |
| Prediction for the separation length of two-dimensional sonic injection with high-speed crossflow Z Wang, C Jiang, Z Gao, C Lee AIAA Journal 55 (3), 832-847, 2017 | 19 | 2017 |
| A new wall function boundary condition including heat release effect for supersonic combustion flows ZX Gao, CW Jiang, CH Lee Applied Thermal Engineering 92, 62-70, 2016 | 18 | 2016 |
| Prediction of ignition delay times of Jet A-1/hydrogen fuel mixture using machine learning Y Huang, C Jiang, K Wan, Z Gao, L Vervisch, P Domingo, Y He, Z Wang, ... Aerospace Science and Technology 127, 107675, 2022 | 17 | 2022 |
| Numerical study of combustion effects on the development of supersonic turbulent mixing layer flows with WENO schemes H Liu, Z Gao, C Jiang, C Lee Computers & Fluids 189, 82-93, 2019 | 17 | 2019 |
| A RANS model correction on unphysical over-prediction of turbulent quantities across shock wave Z Zhang, Z Gao, C Jiang, CH Lee International Journal of Heat and Mass Transfer 106, 1107-1119, 2017 | 16 | 2017 |
| The progress of the overlapping grid techniques LI Peng, GAO Zhenxun, J Chongwen Mechanics in Engineering 36 (5), 551-565, 2014 | 16 | 2014 |
| Influence of inter-car wind-shield schemes on aerodynamic performance of high-speed trains JS Yang, CW Jiang, ZX Gao, YC Lu, JB Zhang, CH Lee Journal of the China Railway Society 34 (11), 29-35, 2012 | 16 | 2012 |
| Numerical investigation of shock-turbulent mixing layer interaction and shock-associated noise F Shi, Z Gao, C Jiang, CH Lee Physics of Fluids 33 (2), 2021 | 15 | 2021 |
| Combined-Wedge Waverider for Airframe–Propulsion Integration S Hu, C Jiang, Z Gao, CH Lee AIAA Journal 56 (8), 3348-3352, 2018 | 15 | 2018 |
| Heat transfer and behavior of the Reynolds stress in Mach 6 boundary layer transition induced by first-mode oblique waves P Guo, F Shi, Z Gao, C Jiang, CH Lee, C Wen Physics of Fluids 34 (10), 2022 | 13 | 2022 |
| Sensitivity analysis on supersonic-boundary-layer stability subject to perturbation of flow parameters P Guo, Z Gao, C Jiang, CH Lee Physics of Fluids 33 (8), 2021 | 13 | 2021 |
| Grid generation criterions in hypersonic aeroheating computations Z Zhichao, GAO Zhenxun, J Chongwen, LEE Chunhian 北京航空航天大学学报 41 (4), 594-600, 2015 | 13* | 2015 |
| Local-variable-based model for hypersonic boundary layer transition P Guo, Z Gao, Z Zhang, C Jiang, CH Lee AIAA Journal 57 (6), 2372-2383, 2019 | 12 | 2019 |
