| Recent research progress on unstart mechanism, detection and control of hypersonic inlet J Chang, N Li, K Xu, W Bao, D Yu Progress in Aerospace Sciences 89, 1-22, 2017 | 216 | 2017 |
| Research progress on strut-equipped supersonic combustors for scramjet application J Chang, J Zhang, W Bao, D Yu Progress in Aerospace Sciences 103, 1-30, 2018 | 166 | 2018 |
| Event-Triggered and Self-Triggered Control of Uncertain Switched Linear Systems Y Qi, P Zeng, W Bao IEEE Transactions on Systems, Man, and Cybernetics: Systems 50 (4), 1442-1454, 2018 | 153 | 2018 |
| Research progress on active thermal protection for hypersonic vehicles S Zhang, X Li, J Zuo, J Qin, K Cheng, Y Feng, W Bao Progress in Aerospace Sciences 119, 100646, 2020 | 136 | 2020 |
| Experimental study on effect of pressure on heat sink of n-decane W Zhou, Z Jia, J Qin, W Bao, B Yu Chemical Engineering Journal 243, 127-136, 2014 | 120 | 2014 |
| Thermal management method of fuel in advanced aeroengines J Qin, S Zhang, W Bao, W Zhou, D Yu Energy 49, 459-468, 2013 | 120 | 2013 |
| Mechanical equipment fault diagnosis based on redundant second generation wavelet packet transform R Zhou, W Bao, N Li, X Huang, D Yu Digital signal processing 20 (1), 276-288, 2010 | 120 | 2010 |
| Efficient utilization of heat sink of hydrocarbon fuel for regeneratively cooled scramjet W Bao, X Li, J Qin, W Zhou, D Yu Applied Thermal Engineering 33, 208-218, 2012 | 98 | 2012 |
| Numerical analysis of flowing cracked hydrocarbon fuel inside cooling channels in view of thermal management W Bao, S Zhang, J Qin, W Zhou, K Xie Energy 67, 149-161, 2014 | 97 | 2014 |
| Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios S Zhang, Y Feng, Y Jiang, J Qin, W Bao, J Han, OJ Haidn Acta Astronautica 127, 41-56, 2016 | 85 | 2016 |
| Switching control of thrust regulation and inlet buzz protection for ducted rocket W Bao, B Li, J Chang, W Niu, D Yu Acta Astronautica 67 (7-8), 764-773, 2010 | 84 | 2010 |
| Oscillation of the shock train in an isolator with incident shocks N Li, JT Chang, KJ Xu, DR Yu, W Bao, YP Song Physics of Fluids 30 (11), 2018 | 83 | 2018 |
| Prediction dynamic model of shock train with complex background waves N Li, JT Chang, KJ Xu, DR Yu, W Bao, YP Song Physics of Fluids 29 (11), 2017 | 82 | 2017 |
| Thermal behavior inside scramjet cooling channels at different channel aspect ratios S Zhang, J Qin, K Xie, Y Feng, W Bao Journal of Propulsion and Power 32 (1), 57-70, 2016 | 79 | 2016 |
| Modeling and analysis of heat and mass transfers of supercritical hydrocarbon fuel with pyrolysis in mini-channel Y Feng, J Qin, S Zhang, W Bao, Y Cao, H Huang International Journal of Heat and Mass Transfer 91, 520-531, 2015 | 79 | 2015 |
| Dynamic characteristics of combustion mode transitions in a strut-based scramjet combustor model W Bao, Q Yang, J Chang, Y Zong, J Hu Journal of Propulsion and Power 29 (5), 1244-1248, 2013 | 79 | 2013 |
| Novel oscillatory patterns of hypersonic inlet buzz J Chang, L Wang, W Bao, J Qin, J Niu, W Xue Journal of Propulsion and Power 28 (6), 1214-1221, 2012 | 77 | 2012 |
| Quasi-one-dimensional model of scramjet combustor coupled with regenerative cooling D Zhang, Y Feng, S Zhang, J Qin, K Cheng, W Bao, D Yu Journal of Propulsion and Power 32 (3), 687-697, 2016 | 76 | 2016 |
| 融合粗糙集和模糊聚类的连续数据知识发现 于达仁， 胡清华， 鲍文 中国电机工程学报 24 (6), 205-210, 2004 | 69 | 2004 |
| Performance evaluation of power generation system with fuel vapor turbine onboard hydrocarbon fueled scramjets D Zhang, J Qin, Y Feng, F Ren, W Bao Energy 77, 732-741, 2014 | 68 | 2014 |
