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个人信息Personal Information
副教授
硕士生导师
性别：男
毕业院校：大连理工大学
学位：博士
所在单位：力学与航空航天学院
学科：飞行器设计. 航空宇航推进理论与工程. 人机与环境工程. 航空宇航制造工程
办公地点：航空航天实验室104、海域楼201
电子邮箱：sunbin83@dlut.edu.cn
扫描关注
- [1]孙斌, Zhang, Yue, Zhou, Cheng, 夏广庆, 鹿畅, Han, Daoman.Influence Mechanism of Magnetic Field and Wave Modes on Helicon Plasma Thruster[J],AIAA JOURNAL,2024
- [2]孙斌, 常悦, 艾亮, 一鸣, Liu, Xuhui, Han, Daoman, Hu, Peng, 鹿畅, 夏广庆.Radial ablation uniformity of cathode and design of double anode micro-cathode arc thruster[J],Acta Astronautica,2024,221:108-120
- [3]Du, M. Q., 丁振峰, Qi, L. W., Wen, X. D., 孙斌.Effects of impedance matching network on α-γ mode transition in atmospheric pressure RF dischar...[J],JAPANESE JOURNAL OF APPLIED PHYSICS,2024,63(8)
- [4]张军军, 孙斌, 鹿畅, 夏广庆, 陈冲.Energy Coupling Mechanism of Electrodeless Plasma Thruster with Rotating Electric Field[J],AIAA JOURNAL,2024,61(5):1939-1953
- [5]韩亚杰, 张军军, 夏广庆, 孙斌, 鹿畅, SAETCHNIKOV, Vladimir A..Plasma transport simulation under different conditions and optimization analysis of dual-stage gr...[J],Chinese Journal of Aeronautics,2024,36(7):388-399
- [6]鹿畅, 夏广庆, 孙斌, Han, Yajie.A particle model of ion thruster plume Mo source based on grid erosion[J],ACTA ASTRONAUTICA,2022,177:217-231
- [7]张军军, 鹿畅, Kang, Huifeng, 夏广庆, 孙斌.Numerical Investigation of Electrodeless Plasma Thruster with Rotating Electric Field[J],AIAA JOURNAL,2024,62(8):3066-3076
- [8]王梓平, 范益朋, Han, Daoman, 夏广庆, 鹿畅, 孙斌, 陈冲.Multi-hole grid thruster plume simulation model based on single grid aperture analytical model[J],FirePhysChem,2024
- [9]陈冲, 鹿畅, 夏广庆, Chen, Maolin, 孙斌.A sharp immersed method for electrohydrodynamic flows accompanied by charge evaporation[J],International Journal for Numerical Methods in Fluids,2024
- [10]韩亚杰, 张军军, 陈留伟, 夏广庆, 孙斌, 鹿畅.A Novel Transversal-Feed Electron Cyclotron Resonance Plasma Thruster: Design and Plasma Characte...[J],AEROSPACE,2024,10(10)
- [11]陈冲, 范益朋, 夏广庆, 鹿畅, 孙斌, 韩亚杰.Ion evaporation-induced tip streaming from liquid drops of ionic liquids[J],PHYSICS OF FLUIDS,2024,36(3)
- [12]鹿畅, 夏广庆, 孙斌, 韩亚杰.The confinement characteristic of primary electrons with the variation of channel width in the di...[A],未来空间技术高峰论坛,2022
- [13]韩亚杰, 夏广庆, 孙斌, 陈留伟.电子回旋共振等离子体推力器结构优化及实验研究[A],第十五届中国电推进技术学术研讨会,2019
- [14]鹿畅, 夏广庆, 孙斌, 韩亚杰.离子推力器双阶栅极系统引出性能的研究[A],中国航天第三专业信息网第四十一届技术交流会暨第五届空天动力联合会议,2020
- [15]范益朋, 夏广庆, 韩亚杰, 鹿畅, 孙斌, 丁亮.离子液体微推进技术研究进展[J],航空动力学报,2020,35(6):1275-1285
- [16]范益朋, 夏广庆, 鹿畅, 孙斌, 丁亮.离子液体推力器性能影响因素仿真研究[J],航天器环境工程,2021,38(04):381-388
- [17]鹿畅, 夏广庆, 孙斌, Han, Ya-Jie, Guan, Si-Qi.碳纳米管阵列推力器放电特性的数值模拟研究[J],Yuhang Xuebao/Journal of Astronautics,2021,42(5):634-641
- [18]鹿畅, 夏广庆, 孙斌, 韩亚杰.考夫曼离子推力器放电室数值模拟研究综述及展望[A],第三届中国空天推进技术论坛,2020
- [19]郭明坤, 韩亚杰, 夏广庆, 孙斌.微纳卫星新型动力系统研究进展[A],第十四届中国电推进技术学术研讨会,2022
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