Gong Jishuang, Associate Research Professor
Email: gongjsh@mail.tsinghua.edu.cn
Address: Tsinghua University, Haidian District, Beijing, China
Education background
Sep. 2002-Jun. 2012, Nanjing University of Aeronautics and Astronautics, B.E. and Ph.D.
Professional Experience
Aug. 2012-Jul. 2015, A research institute of China Aerospace, Engineer and Senior Engineer.
Aug. 2015-Jul. 2018, Academy of Equipment, People's Liberation Army, Postdoctoral Fellow.
Aug. 2018-Aug. 2019, A research institute of China Aerospace, Senior Engineer and Deputy Chief Designer for engine overall technical design.
Sep. 2019-Jan. 2026, School of Aeronautics and Astronautics, Sun Yat-sen University, Associate Professor.
2026-Present, Institute for Aero Engine, Tsinghua University, Associate Research Fellow.
Research Interests
Turbine, ramjet, and combined-cycle engine technologies
Detonation combustion technology
Gas-liquid two-phase flow technology
Research Overview
Dr. Gong has long been engaged in research on aero engines and rotating detonation engines. He has led or served as a core member in more than 20 research projects, including projects supported by the National Natural Science Foundation of China, national key laboratory foundations, and rotating detonation xxx research programs. To date, he has published more than 30 academic papers in authoritative journals and international and domestic conferences, including 11 SCI-indexed papers, and has been granted 14 national invention patents.
Academic Achievements
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. 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: 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: 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: 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: 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: 123182.
9. J. Gong, L. Zhou, Y. Zhang, H. Teng. Study on characteristics of rotating detonation waves based on the method of characteristics [J]. Journal of Experiments in Fluid Mechanics, 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.
