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[2] 鹿畅, 曹勇, 夏广庆. 离子推力器双阶栅极系统引出性能研究[J].推进技术, 2022, 43(03): 392-398.
[3] 鹿畅, 夏广庆, 韩亚杰, 关思琦. 碳纳米管阵列推力器放电特性的数值模拟研究[J].宇航学报, 2021, 42(05):634-641.
[4] Lu Chang, Xia Guangqing, Sun Bin, and Han Yajie. A particle model of ion thruster plume Mo source based on grid erosion[J]. Acta Astronautica, 2020,177, 217–231.
[5] Lu Chang, Wan Jie, Cao Yong, and He Xiaoming. A fully decoupled iterative method with three-dimensional anisotropic immersed finite elements for Kaufman type discharge problems[J]. Computer Methods in Applied Mechanics and Engineering, 2020, 372, 113345.
[6] Lu Chang, Xia Guangqing, Sun Bin, and Han Yajie. Confinement characteristic of primary electrons with the variation of channel width in the discharge chamber of annular ion thruster[J]. Chinese Journal of Aeronautics, 2021, 34, 79–92.
[7] Lu Chang, Yang Zhi, Bai Jinwei, Cao Yong, and He Xiaoming. Three-dimensional immersed finite element method for anisotropic magnetostatic/electrostatic interface problems with nonhomogeneous flux jump[J]. International Journal for Numerical Methods in Engineering, 2020, 121, 2107–2127.
[8] Lu Chang, Zhang Tianping, Qiu Pei, Chen Juanjuan, Cao Yong, Zheng Liang. Barrel erosion of ion thruster accelerator grid under different operating conditions[J]. IEEE Transactions on Plasma Science , 2018;46(12):4065–77.
[9] Lu Chang, Zhao Yide, Wan Jie, Chu Yuchuan, Zheng Liang, Cao Yong. Influence of the decelerator grid on the optical performance of the ion thruster[J]. International Journal of Aerospace Engineering , 2019;2019(2):1–11.
[10] Lu Chang, Luo Yang, Xia Guangqing, Gao Hui, Xu Nuo. Numerical study of the grid erosion of field emission electric propulsion[J]. Plasma Science and Technology, 2021, 23(10):104001
鹿 畅,夏广庆,张军军,等. 考夫曼离子推力器放电室数值模拟研究综述及展望[J]. 推进技术,2022,43(6):201004. (LU Chang,XIA Guang-qing,ZHANG Jun-jun,et al. Review and Prospect of Numerical Simulation for Discharge Chamber of Kaufman Ion Thruster[J]. Journal of Propulsion Technology,2022,43(6):201004.)