[1] Wei Sun, Zhiwen Wu, Xuhui Liu, Jin Li, Pengkun Li, Zening Du, Wei Mao, Yuntao Guo*. Measurement of long-time performance changes of porous electrowetting ionic liquid electrospray thrusters[J].Chinese Journal of Aeronautics, online. https://doi.org/10.1016/j.cja.2025.103724
[2] Pengkun Li, Yuntao Guo*, Jin Li, Zening Du, Wei Sun and Zhiwen Wu. Performance diagnosis of ionic liquid electrospray thruster at different plume angles[J]. Plasma Science and Technology, 2025, 27: 064010.
[3] Yiqiao Zhang, Zhiwen Wu*, Yuntao Guo*, Zhihui Zhang, Pengxin Chen and Xiaodong Chen. Study on the aerodynamic effects on the excitation of the combustion flow field in solid rocket ramjet engines[J]. Aerospace Science and Technology, 2025, 164:110364.
[4] Yiqiao Zhang, Zhiwen Wu*, Yuntao Guo, Zhihui Zhang and Pengxin Chen. Study on the effect of gas injection hole radius on mixing and combustion in solid propellant ducted rockets based on total pressure distribution[J]. Aerospace Science and Technology, 2025, 165:110456.
[5] Pengxin Chen, Zhiwen Wu, Tianyu Lu, Yuntao Guo, Zhihui Zhang, Yiqiao Zhang. Numerical study on the influence of inlet cover opening process on the stage transition performance of solid propellant ducted rockets[J]. Physics of Fluids, 2025, 37(7): 075217.
[6] Wei Sun, Zhiwen Wu*, Yuntao Guo*, Zening Du, Zhenning Sun, Jin Li, Pengkun Li and Ningfei Wang. Lifetime experiment and analysis of an electrowetting ionic liquid electrospray thruster[J]. Acta Astronautica, 2024, 224:465-470.
[7] Zening Du, Zhiwen Wu, Jin Li, Wei Sun, Pengkun Li and Yuntao Guo*. Study on the plume self-neutralization of ionic liquid electrospray thruster based on median potential[J]. Plasma Sources Science and Technology, 2024, 33(5): 055016.
[8] Wei Sun, Yuntao Guo*, Zhiwen Wu*, Zening Du, Ningfei Wang and Zhenning Sun. Design and Performance of an Electrowetting Ionic Liquid Electrospray Thruster Prototype[J]. Journal of Propulsion and Power, 2024, 40(3):1-8.
[9] Yuntao Guo, Wei Sun, Zhenning Sun, Zhiwen Wu*, Jianwu He, Chao Yang and Ningfei Wang. Direct thrust test and asymmetric performance of porous ionic liquid electrospray thruster[J]. Chinese Journal of Aeronautics, 2023, 36(4): 120-133.
[10] Wei Sun, Zhiwen Wu*, Zhenning Sun, Yuntao Guo*, Tiankun Huang, Guorui Sun, Jingran Xue and Ningfei Wang. Study on the control of propellant flow by electric field in ionic liquid electrospray thruster[J]. International Journal of Heat and Mass Transfer, 2022,183:121926.
[11] Yuntao Guo, Shipeng Li, Zhiwen Wu*, Kangwu Zhu and Ningfei Wang. Pulsation characteristics of corona discharge in electrohydrodynamic process using ionic liquid[J]. IEEE Transactions on Plasma Science, 2019, 47(12):5234-5238.
[12] Yuntao Guo, Shipeng Li, Zhiwen Wu*, Kangwu Zhu, Han Yuning and Ningfei Wang. Interaction between electrospray using ionic liquid and simultaneous corona discharge under positive and negative polarity[J]. Physics of Plasmas, 2019, 26(7):073511.
[13] 武志文，孙伟，郭云涛*，孙振宁，杜泽宁，李锦，王宁飞. 被动型离子液体电喷推力器寿命影响因素分析[J]. 宇航学报, 2025, 46(01): 157-167.
[14] 汪宇欣, 武志文, 黄天坤, 陈茂林, 叶剑民, 郭云涛, 王云冰, 刘旭辉, 胡鹏. 微牛级高精度直流离子推进系统的推力调节特性[J]. 宇航学报, 2024, 45(05): 770-777.
[15] 孙振宁，武志文，郭云涛，韩雨宁，孙国瑞，王宁飞. 离子液体电喷推力器羽流中和特性研究[J]. 推进技术, 2022, 43(4):200310.
[16] 郭云涛, 李世鹏, 武志文*, 朱康武，韩雨宁，孙振宁，王宁飞. 离子液体电喷微推力器系统设计及性能初步研究[J]. 推进技术, 2020, 41(1):212-219.
项目承担情况
1. 国家自然科学基金面上项目、青年项目
2. 中国博士后科学基金面上资助
3. 国家重点研发计划科研攻关应急项目子课题
4. 全国重点实验室开放课题
5. 航天院所委托课题
