宫继双 副研究员

邮件：gongjsh@mail.tsinghua.edu.cn

地址：北京市海淀区清华大学

教育背景

2012年6月 毕业于南京航空航天大学 获博士研究生学历，工学博士学位

工作履历

2026.1-至今，清华大学，航空发动机研究院

2019.9至2025.12，中山大学/航空航天学院，副教授

2018.8至2019.8，中国航天某研究院，高级工程师、发动机总计技术副主任设计师

2015.8至2018.7，中国人民解放军装备学院，博士后

2012.8至2015.7，中国航天科工三院，工程师、高级工程师

研究领域

旋转爆震燃烧技术及其工程化应用

空天组合动力技术

研究概况

长期从事旋转爆震燃烧机理、爆震发动机工程化技术、新型材料在航空发动机领域应用等方向研究。先后承担和作为核心骨干参与国家自然科学基金、基础加强领域基金、重点实验室基金、国家重点工程等课题20余项。迄今为止在国内外权威期刊和国内外会议发表学术论文20余篇，其中SCI论文10余篇；授权国家发明专利10余项。

学术成果

1.J. Tan, J. Gong*, Y. Liao, S. Li, J. Wang, C. Xue, S. Zheng, D. Tabusi, Q. Zhu, Experimental study of kerosene-fueled cylindrical air-breathing continuous rotating detonation engine, Aerosp. Sci. Technol. 164 (2025) 110419. https://doi.org/10.1016/j.ast.2025.110419.

2. 1. S. Lu, Q.Y. Zhu, J.S. Gong*, H. Chen, H. Ying, Experimental study on transpiration cooling with phase change in rotating detonation engine, Appl. Therm. Eng., 258 (2025) 124633.

3. S. Lu, Q.Y. Zhu, J.S. Gong*, H. Chen, L.Z. Fan, Numerical study of phase change heat transfer in rotating detonation combustion chamber with transpiration cooling using liquid coolant, Appl. Therm. Eng., 265 (2025) 125571.

4.  Jishuang Gong*; Hu Ma ; Experimental Study on Pulse Detonation Engine with Two-Phase Inhomogeneous Mixture, International Journal of Aerospace Engineering, 2020. 2020(2020): 1-11  

5.  Jianyong Wang*; Kan Qin; Jishuang Gong*; Kamel Hooman ; Turbulent Heat Transfer of Highly Buoyant Supercritical CO2 Flow in Various Horizontal Pipes, International Communications in Heat and Mass Transfer, 2022, 133(2022): 105939-105939

6.  Jianyong WANG*; Jun YANG; Jishuang GONG*; Chunrong ZHAO; Kamel HOOMAN ; A Designed Wall Roughness Approach to Improve Turbulent Heat Transfer to Supercritical CO2 Flowing in Horizontal Tubes, Journal of Supercritical Fluids, 2022, 190(2022): 105738-105738

7.  Jianyong Wang*; Jishuang Gong*; Xin Kang; Chunrong Zhao; Kamel Hooman ; Assessment of RANS turbulence models on predicting supercritical heat transfer in highly buoyant horizontal flows, Case Studies in Thermal Engineering, 2022, 34(2022): 102057-102057  

8.  Xiongzhou Xie; Daoming Ye; Jishuang Gong; Shilong Zhao; Jianyong Wang*; Influence of conjugate thermal boundary on turbulent heat transfer of supercritical CO2 in the horizontal tube, Applied Thermal Engineering, 2024, 248(2024): 123182-123182      

9. 宫继双*, 周林, 张义宁, 滕宏辉.基于特征线法的旋转爆震波特征研究[J].实验流体力学，2019,33(1):89-96.

10. Experimental study on Initiation of Oblique Detonation Waves. International Space Plane and Hypersonic Systems and Technology Conference，AIAA 2017-2350. EI：20171603581723