秦飞


的个人主页 http://teacher.nwpu.edu.cn/qinfei

  被浏览次数:3051

基本信息 The basic information

秦飞

航天学院

博士研究生毕业

博士

教授

航空宇航科学与技术

qinfei@nwpu.edu.cn

教育经历 Education Experience

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 

教育教学 Education And Teaching

1.火箭发动机设计

2.吸气式推进技术


科学研究 Scientific Research

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 


学术成果 Academic Achievements

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.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 structure and combustion mode in a hydrogen fueled supersonic combustor, International Journal 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 RBCC combustor 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 the thermal effect in the cavitating venturi flow, Journal of Thermophysics and heat 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-direction carbon-carbon composites and their components in carbon dioxide at high temperature, 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 layer bleed for a rocket-based combined-cycle inlet in ejector mode, International Journal 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 gas mass flow rate on carbon/carbon composite nozzle ablation in a solid rocket motor, 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