研究方向
1. 火箭衝壓組合發動機（RBCC）技術
2.衝壓發動機技術
3. 超聲速燃燒
4. 發動機數值模擬
5. 多尺度燒蝕模型
學習經歷
1996年-2000年，西北工業大學，學士
2000年-2003年，西北工業大學，碩士
2004年-2008年，西北工業大學，博士
主要學術成就
1.Fei Qin*, Li-na Peng, et al., Oxidation kinetics and mechanisms of carbon-carbon composites and their components in water vapour at high temperatures, Corrosion Science, Vol.90, 340-346, 2015.
2. Zhi-wei Huang, Guo-qiang He,Fei Qin*, Xiang-geng Wei, Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor, International Journal of Hydrogen Energy, Vol.40, 9815-9824, 2015.
3. Ya-jun Wang, Jiang Li,Fei Qin*, Guo-qiang He, Lei Shi, Study of thermal throat of RBCC combustor based on one-dimensional analysis, Acta Astronautica, Vol.117, 130-141, 2015.
4. Dong-gang Cao*, Guo-qiang He, Hongliang Pan, andFei Qin, Numerical simulation of the thermal effect in the cavitating venturi flow, Journal of Thermophysics and heat transfer, Vol.29, No.1, 190-196, 2015.
5.Fei Qin*, Li-na Peng, et al., Oxidation kinetics and mechanisms of four-direction carbon-carbon composites and their components in carbon dioxide at high temperature, Corrosion Science, Vol.77, 164-170, 2013.
6. Lei Shi*, Guoqiang He,Fei Qinand Xianggeng Wei, Numerical study of a boundary layer bleed for a rocket-based combined-cycle inlet in ejector mode, International Journal of Turbo & Jet-Engines, Vol.31, 347-359, 2014.
7. Li-na Peng, Guo-qiang He, Jiang Li, Lei Wang,Fei Qin*, Effect of combustion gas mass flow rate on carbon/carbon composite nozzle ablation in a solid rocket motor, Carbon, Vol.50, 1554-1562, 2012.
8. 秦飛，何國強，劉佩進等，圓形燃燒室支板火箭超燃衝壓發動機數值模擬，固體火箭技術，Vol.34, No.2, 150-155, 2011.
