科研工作:

1. 火箭冲压组合发动机（RBCC）技术 2. 冲压发动机技术3. 超声速燃烧4. 发动机数值模拟 5. 多尺度烧蚀模型 1. Fei Qin*,Li-na Peng, et al., Oxidation kinetics and mechanisms of carbon-carboncomposites and their components in water vapour at high temperatures, CorrosionScience, Vol.90, 340-346, 2015.（SCI，影响因子3.686 ，2区）2. Zhi-wei Huang, Guo-qiang He, Fei Qin*, Xiang-geng Wei, Large eddy simulation of flame structureand combustion mode in a hydrogen fueled supersonic combustor, InternationalJournal of Hydrogen Energy, Vol.40, 9815-9824, 2015. （SCI ，影响因子3.313 ，2区，通讯作者）3. Ya-jun Wang, Jiang Li, Fei Qin*, Guo-qiang He, Lei Shi, Study of thermal throat of RBCCcombustor based on one-dimensional analysis, Acta Astronautica, Vol.117,130-141, 2015. （SCI，影响因子1.122 ，3区，通讯作者）4. Dong-gang Cao*, Guo-qiang He, Hongliang Pan, and Fei Qin, Numerical simulation of thethermal effect in the cavitating venturi flow, Journal of Thermophysics andheat transfer, Vol.29, No.1, 190-196, 2015.（SCI，影响因子0.87，4区）5. Fei Qin*,Li-na Peng, et al., Oxidation kinetics and mechanisms of four-directioncarbon-carbon composites and their components in carbon dioxide at hightemperature, Corrosion Science, Vol.77, 164-170, 2013. （SCI ，影响因子3.686 ，2区）6. Lei Shi*, Guoqiang He, Fei Qin and Xianggeng Wei, Numerical study of a boundary layerbleed for a rocket-based combined-cycle inlet in ejector mode, InternationalJournal of Turbo & Jet-Engines, Vol.31, 347-359, 2014. （SCI ，影响因子0.218 ，4区）7. Li-na Peng, Guo-qiang He, Jiang Li, Lei Wang, Fei Qin*, Effect of combustion gasmass flow rate on carbon/carbon composite nozzle ablation in a solid rocketmotor, Carbon, Vol.50, 1554-1562, 2012.（SCI，影响因子5.378，1区，通讯作者）8. 秦飞，何国强，刘佩进等，圆形燃烧室支板火箭超燃冲压发动机数值模拟，固体火箭技术，Vol.34, No.2, 150-155,2011. （EI）

教育背景:

1996年-2000年，西北工业大学，学士2000年-2003年，西北工业大学，硕士2004年-2008年，西北工业大学，博士