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 | 207 | 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 | 132 | 2014 |
Thermal management method of fuel in advanced aeroengines J Qin, S Zhang, W Bao, W Zhou, D Yu Energy 49, 459-468, 2013 | 130 | 2013 |
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 | 109 | 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 | 103 | 2014 |
Numerical study on a water cooling system for prismatic LiFePO4 batteries at abused operating conditions X Xu, W Li, B Xu, J Qin Applied Energy 250, 404-412, 2019 | 99 | 2019 |
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 | 97 | 2016 |
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 | 96 | 2016 |
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 | 87 | 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 | 87 | 2015 |
A lightweight and low-cost liquid-cooled thermal management solution for high energy density prismatic lithium-ion battery packs J Xu, Z Chen, J Qin, P Minqiang Applied Thermal Engineering 203, 117871, 2022 | 86 | 2022 |
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 | 80 | 2012 |
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 | 77 | 2014 |
Improved thermal performance of cooling channels with truncated ribs for a scramjet combustor fueled by endothermic hydrocarbon Y Li, F Sun, G Xie, J Qin Applied Thermal Engineering 142, 695-708, 2018 | 75 | 2018 |
Thermodynamic analysis and parametric study of a closed Brayton cycle thermal management system for scramjet J Qin, W Zhou, W Bao, D Yu international journal of hydrogen energy 35 (1), 356-364, 2010 | 74 | 2010 |
Power optimization and comparison between simple recuperated and recompressing supercritical carbon dioxide Closed-Brayton-Cycle with finite cold source on hypersonic vehicles K Cheng, J Qin, H Sun, H Li, S He, S Zhang, W Bao Energy 181, 1189-1201, 2019 | 73 | 2019 |
Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers D Zhang, S Yang, S Zhang, J Qin, W Bao Energy 90, 1046-1054, 2015 | 72 | 2015 |
Turbulent flow characteristics and heat transfer enhancement in a square channel with various crescent ribs on one wall G Xie, X Liu, H Yan, J Qin International Journal of Heat and Mass Transfer 115, 283-295, 2017 | 68 | 2017 |
Parametric numerical analysis of regenerative cooling in hydrogen fueled scramjet engines S Zhang, Y Feng, D Zhang, Y Jiang, J Qin, W Bao international journal of hydrogen energy 41 (25), 10942-10960, 2016 | 65 | 2016 |
Performance assessment of multi-stage thermoelectric generators on hypersonic vehicles at a large temperature difference K Cheng, J Qin, Y Jiang, C Lv, S Zhang, W Bao Applied Thermal Engineering 130, 1598-1609, 2018 | 64 | 2018 |