[1] Yan, Dongfeng ; Wei, Zhijun; Xie, Kan; Wang, Ningfei. Simulation of thrust control by fluidic injection and pintle in a solid rocket motor. Aerospace Science and Technology, v 99, April 2020
[2] Yang, Xiaolong; Wei, Zhijun; Zhang,jingjia; Zhang, Zelin; Wang, Ningfei. Numerical study of the effect of electric fields on the combustion characteristics of PMMA under lateral inflow. Acta Astronautica, v 167, p 418-428, February 2020
[3] Yang, Xiaolong; Wei, Zhijun; Zhang, Zelin; Zhang, Jingjia. Study of the effect of DC high-voltage electric fields on the regression rate of PMMA. Acta Astronautica, v 165, p 117-128, December 2019
[4] Fang, Guanlin; Wei, Zhijun; Wu, Zhiwen; Guo, Changchao; Wang, Lihe; Du, Rui; Zhang, Hao; Wang, Ningfei. Experimental study on a long-time working solid-fuel scramjet combustor. Science and Technology of Energetic Materials, v 80, n 1-2, p 31-40, 2019
[5] Fang, Guanlin; Wei, Zhijun; Wu, Zhiwen; Du, Rui; Wang, Ningfei. Experimental and numerical investigation of an embedded rocket ramjet combustor. Acta Astronautica, v 165, p 105-116, December 2019
[6] Yan, Dongfeng; Wei, Zhijun; Xie, Kan. Effect of oxidative jet flow in throat and divergence section on nozzle performance. AIAA Propulsion and Energy Forum and Exposition, 2019, 2019, AIAA Propulsion and Energy Forum and Exposition, 2019
[7] 杨小龙,魏志军,张泽霖,张靖佳,王佳兴.直流高压电场对固体燃料PMMA燃烧特性的影响[J].含能材料,2019,27(04):282-289.
[8] Guo, Changchao; Wei, Zhijun; Xie, Kan; Yan, Dongfeng; Wang, Ningfei. One-dimensional theoretical analysis of dilute particle-gas swirling flow in the laval nozzle. AIAA Journal, v 56, n 3, p 1277-1283, 2018
[9] Zhang, Jing-Jia; Wei, Zhi-Jun; Zhang, Ze-Lin; Yang, Xiao-Long; Wang, Ning-Fe. Numerical studies of magnetohydrodynamic gas jet deflection considering gas parameters. 2018 Joint Propulsion Conference, 2018, 2018 Joint Propulsion Conference
[10] Zhang, Ze-Lin; Wei, Zhi-Jun; Zhang, Jing-Jia; Yang, Xiao-Long; Wang, Ning-Fei. Initial research for the influence of magnetic field on the combustion processes of PMMA. 2018 Joint Propulsion Conference, 2018, 2018 Joint Propulsion Conference
[11] Hu, Ming; Wei, Zhijun; Ding, Shiqi; Wang, Ningfei. Numerical investigation of a combined solid fuel scramjet combustor. Acta Astronautica, v 148, p 210-219, July 2018
[12] Guo, Changchao; Wei, Zhijun; Xie, Kan; Wang, Ningfei. Thrust control by fluidic injection in solid rocket motors. Journal of Propulsion and Power, v 33, n 4, p 815-829, 2017
[13] Hu, Ming; Li, Biao; Wei, Zhijun. Effect of compression ratio on performance of solid fuel scramjet. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, 2017, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
[14]迟鸿伟,魏志军,李彪,王利和,王宁飞.燃烧室构型对固体燃料超燃冲压发动机自点火的影响[J].航空动力学报,2016,31(08):1985-1994.
[15]陶欢,魏志军,迟鸿伟,孙巍伟,王宁飞.燃烧室长度对固体燃料超燃冲压发动机燃烧室性能的影响[J].航空动力学报,2016,31(03):598-607.
[16]李彪,魏志军,迟鸿伟,王宁飞.进气道内压缩比对固体燃料超燃冲压发动机性能的影响[J].航空动力学报,2016,31(02):459-466.
