2017.06-2021.09，南京理工大学瞬态物理国家重点实验室，讲师；

    2021.10-至今，南京理工大学瞬态物理国家重点实验室，副研究员。

    2010年毕业于南京理工大学，热能与动力工程专业，获工学学士学位；

    2017年毕业于南京理工大学，工程热物理专业，师从翁春生教授，获工学博士学位。

[1] Zheng Quan^*, Meng Haolong, Weng Chunsheng, et al. Experimental research on the instability propagation characteristics of liquid kerosene rotating detonation wave[J]. Defence Technology, 2020, 16(6): 1106-1115.

[2] Meng Haolong, Zheng Quan^*, Weng Chunsheng, Wu Yuwen, Feng Wenkang, Xu Gao. Propagation mode analysis of rotating detonation waves fueled by liquid kerosene[J]. Acta Astronautica, 2021, 187: 248-258.

[3] Haolong Meng, Qiang Xiao, Wenkang Feng, Mingliang Wu, Xinpei Han, Fang Wang, Chunsheng Weng, Quan Zheng^*. Air-breathing rotating detonation fueled by liquid kerosene in cavity-based annular combustor, Aerospace Science and Technology, 2022, 122:107407.

[4] Zheng Quan^*, Weng Chunsheng, Bai Qiaodong . Experimental Research on the Propagation Process of Continuous Rotating Detonation Wave[J]. Defence Technology, 2013, 9( 4):201-207.

[5] 郑权^*,魏万里,翁春生,等.液态燃料喷注压力对旋转爆轰波影响的实验研究[J]. 推进技术, 2020, 41(12):2790-2797.

[6] 郑权^*,李宝星,翁春生,白桥栋.燃烧室长度对液态燃料旋转爆轰发动机性能影响实验研究[J]. 推进技术, 2018, 39(12): 2764-2771.

[7] 郑权^*,李宝星,翁春生,白桥栋.双波对撞模态下液态燃料旋转爆轰发动机推力测试[J]. 兵工学报, 2017, 38(4):679-689.

[8] 郑权,翁春生,白桥栋.当量比对液体燃料旋转爆轰发动机爆轰影响实验研究[J]. 推进技术, 2015, 36(6):6.

[9] 郑权,翁春生,白桥栋.倾斜环缝喷孔式连续旋转爆轰发动机试验[J]. 推进技术, 2014, 35(004):570-576.

[10] Zheng Quan, Meng Haolong, Weng Chunsheng, Wu Yuwen. Experimental Research on Effects of Center Cone on Liquid-Fueled Rotating Detonation Engine Performance[C]. Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019). 2019.

[11] 魏万里,郑权^*,鲁江涛,翁春生,武郁文.中心锥对液态燃料旋转爆轰发动机工作过程与性能的影响[J]. 兵工学报, 2021, 42(06): 1185-1194.

[12] 吴明亮,郑权^*,续晗,翁春生,白桥栋.氢气占比对常温煤油-空气旋转爆轰波传播特性影响的数值模拟研究[J]. 兵工学报. 2022, 43(01).

[13] 李宝星, 翁春生, 郑权^*, 武郁文, 魏万里. 推进剂总质量流量对连续旋转爆轰发动机性能影响实验研究[J]. 推进技术, 2018, 39(6): 1217-1226.

[14] Wu Yuwen^*, Weng Chunsheng, Zheng Quan, Wei Wanli, Bai Qiaodong. Experimental research on the performance of a rotating detonation combustor with a turbine guide vane [J]. Energy, 2021, 218: 119580.

[15] Yuwen Wu^*, Quan Zheng, Chunsheng Weng. An experimental study on the detonation transmission behaviours in acetylene-oxygen-argon mixtures. Energy, 2018, 143: 554-561.

[16] Meng Haolong, Weng Chunsheng^*, Xiao Qiang, Zheng Quan, Wu Yuwen, Wang Fang. Numerical analysis on evolution process of multiple rotating detonation waves with ethylene-oxygen-nitrogen mixture [J]. Proc IMechE Part G: J Aerospace Engineering, 2021, 0(0): 1-14.

[17] Baoxing Li, Yuwen Wu^*, Chunsheng Weng, Quan Zheng, Wanli Wei. Influence of equivalence ratio on the propagation characteristics of rotating detonation wave. Experimental Thermal and Fluid Science, 2018, 93: 366-378.

[18] Wanli Wei, Chunsheng Weng^*, Yuwen Wu, Quan Zheng. Experimental research on influence of turbine guide vane on propagation characteristics of rotating detonation wave. Acta Physica Sinica, 2020, 69(6): 064703.

[19] Wei Wanli, Wu Yuwen*, Weng Chunsheng, Zheng Quan. Influence of propagation direction on operation performance of rotating detonation combustor with turbine guide vane[J]. Defence Technology, 2021, 17(5): 1617-1624.

[20] Fang Wang, Chunsheng Weng*, Yuwen Wu, Qiaodong Bai, Quan Zheng, Han Xu. Numerical research on kerosene/air rotating detonation engines under different injection total temperatures. Aerospace Science and Technology, 2020, 103: 105899.

[21] Fang Wang, Chun-sheng Weng*, Yu-wen Wu, Qiao-dong Bai, Quan Zheng, Han Xu,. Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method [J]. Defence Technology, 2021, 17(6):1805-1816.

  目前指导硕士研究生1名，协助指导硕士研究生6名，博士研究生3名。

  指导学生为第一作者发表SCI论文3篇，EI论文5篇，指导学生申请国防发明专利7件；指导学生获得国家奖学金博士研究生1人，硕士研究生1人，获北方工业奖学金1人，指导研究生申报江苏省研究生科研创新计划项目1项；协助指导钱学森学院本科生国家级科研训练1项。

  隶属于南京理工大学瞬态物理国家重点实验室副主任翁春生教授“爆轰推进”团队。