| A review of impinging jets during rocket launching C Jiang, T Han, Z Gao, CH Lee Progress in Aerospace Sciences 109, 100547, 2019 | 94 | 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 | 76 | 2015 |
| Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet ZX Gao, CH Lee Science China Technological Sciences 54 (4), 883-893, 2011 | 72 | 2011 |
| A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine ZX Gao, CH Lee Science China Technological Sciences 53 (8), 2111-2121, 2010 | 63 | 2010 |
| Improvement and application of wall function boundary condition for high-speed compressible flows ZX Gao, CW Jiang, CH Lee Science China Technological Sciences 56 (10), 2501-2515, 2013 | 57 | 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 | 43 | 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 | 42 | 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 | 34 | 2017 |
| 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 | 32 | 2022 |
| A flamelet model for turbulent diffusion combustion in supersonic flow ZX Gao, CH Lee Science China Technological Sciences 53 (12), 3379-3388, 2010 | 28 | 2010 |
| Numerical study on drag reduction by micro-blowing/suction compounding flow control on supercritical airfoil C Junxuan, GZ Xun Procedia Engineering 99, 613-617, 2015 | 27 | 2015 |
| 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 | 26 | 2021 |
| 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 | 25 | 2017 |
| 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 | 24 | 2019 |
| 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 | 24 | 2019 |
| 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 | 22 | 2022 |
| Studies of combustion effects on near-wall turbulence in supersonic flows by large eddy simulation H Liu, Z Gao, C Jiang, CH Lee Aerospace Science and Technology 107, 106328, 2020 | 22 | 2020 |
| 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 | 22 | 2016 |
| Numerical investigations of the slot blowing technique on the hypersonic vehicle for drag reduction F Mo, W Su, Z Gao, C Du, C Jiang, CH Lee Aerospace Science and Technology 121, 107372, 2022 | 21 | 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 | 21 | 2021 |
