王宇辉，北京化工大学机电工程学院见习教授，硕士生导师，流体力学专业，研究方向为旋转爆轰发动机和界面不稳定性，博士毕业于北京大学。第一或通讯作者发表SCI论文14篇，其他论文20多篇。现为美国航空航天学会会员（AIAA member），SCI期刊 International Journal of Hydrogen Energy, Experimental Thermal and Fluid Science, Aerospace Science and Technology, Applied Thermal Engineering, International Journal of Heat and Mass Transfer, shock waves等的审稿人。担任8th International Symposium on Nonequilibrium Processes, Plasma, Combustion, and Atmospheric Phenomena (俄罗斯索契，2018)分会主席。获得第十八届全国激波与激波管学术会议优秀青年论文奖(2018)。主持科研项目十余项。
代表性论文：
1.Zhu W., Wang Y.*, Wang J. Flow field of a rotating detonation engine fueled by carbon. Phys. Fluids, 2022, 34: 073311.
2.Zhu W., Wang Y.*. Effect of hydrogen flow rate and particle diameter on coal-hydrogen-air rotating detonation engines. Int. J. Hydrogen Energy, 2022, 47: 1328 8-1342.
3.Wang Y., Le J. Experimental study of sharp noise caused by rotating detonation waves. Noise Control Engr. J., 2022, 70: 527-539.
4.Wang Y., Le J. Combustion Characteristics in Rotating Detonation Engines. Int. J. Aerosp. Eng., 2021.https://doi.org/10.1155/2021/8839967
5.Wang Y., Le J. A rotating detonation engine using methane-ethylene mixture and air. Acta Astronaut., 2021, 188: 25-35.
6.Wang Y., Le J. A hollow combustor that intensifies rotating detonation. Aerosp. Sci. Technol., 2019, 85:113-124.
7.Wang Y., Le J. Rotating detonation engines with two fuel orifice schemes. Acta Astronaut., 2019, 161: 262-275.
8.Wang Y., Le J., Wang C., Zheng Y., Huang S. The effect of the throat width of plug nozzles on the combustion mode in rotating detonation engines. Shock Waves, 2019, 29: 471-485.
9.Wang Y., Le J., Wang C., Zheng Y. A non-premixed rotating detonation engine using ethylene and air. Appl. Therm. Eng., 2018, 137: 749-757.
10.Wang Y., Le J. How multiple rotating detonation waves are produced. AIAA 2018-5202.
11.Wang Y., Le J. High-speed Imaging in an Optically Accessible Non-premixed Rotating Detonation combustor. AIAA 2018-4781.
12.Wang Y., Wang J. Coexistence of detonation with deflagration in rotating detonation engines. Int. J. Hydrogen Energy, 2016, 41:14302-14309.
13.Wang Y. Rotating detonation in a combustor of trapezoidal cross section for the hydrogen-air mixture. Int. J. Hydrogen Energy, 2016, 41: 5605-5616.
14.Wang Y., Wang J., Qiao W. Effects of thermal wall conditions on rotating detonation. Comput. Fluids, 2016, 140:59-71.
15.Wang Y., Wang J. Effect of equivalence ratio on the velocity of rotating detonation. Int. J. Hydrogen Energy, 2015, 40:7949-7955.
16.Wang Y., Wang J., et al. Induction for multiple rotating detonation waves in the hydrogen-oxygen mixture with tangential flow. Int. J. Hydrogen Energy, 2014. 39: 11792-11797.
17.李世全，杨帆，王宇辉*，王健平，张国庆．当量比对铝粉/空气旋转爆轰发动机流场影响的数值模拟研究，航空动力学报．https://doi.org/10.13224/j.cnki.jasp.20210560.
18.杨帆，姜春雪，王宇辉*，李世全，王健平，张国庆．煤油液滴直径对两相旋转爆轰发动机流场的影响，爆炸与冲击． https://kns.cnki.net/kcms/detail/51.1148.O3.20221026.1556.012.html.
19.杨帆，王宇辉*，李世全，张国庆．基于煤油的旋转爆轰发动机流场数值模拟，航空动力学报，2022, 37, 1620-1632．
20.祝文超，王健平，王宇辉*，李世全，杨帆，相博，张国庆．空气流量对煤粉-空气两相旋转爆轰波的影响，煤炭学报，2022, 47, 3715-3728．
21.王宇辉，王 超，郑榆山，乐嘉陵，黄思源．基于乙烯或氢气的吸气式旋转爆轰发动机实验，气体物理，2018, 3 (6): 16-25．
招收研究生：
本人长期接收研究生，研究方向为旋转爆轰发动机和界面不稳定性。欢迎同学们报考！邮箱aowuki@163.com.