基本情况
王健平，北京大学工学院燃烧推进动力研究中心教授兼主任，北京大学环境学院教授。
研究领域
主要从事爆轰和计算流体力学的研究。
部分论文
1. Shen, Dawen,Cheng, Miao,Rong, Guangyao, et al.Effects of film cooling injection inclination angle on cooling performance in rotating detonation combustors[J].PHYSICS OF FLUIDS,2024,36(02).DOI:10.1063/5.0188972.
2. Cheng, Miao,Sheng, Zhaohua,Wang, JianPing.BYCFoam: An Improved Solver for Rotating Detonation Engines Based on OpenFOAM[J].ENERGIES,2024,17(04).DOI:10.3390/en17040769.
3. Wang, Yingnan,Zhang, Xiangjun,Liu, Peilin, et al.Effect of the inlet spatial fluctuation on the gas-solid continuous rotating detonation flow field characteristics[J].PHYSICS OF FLUIDS,2024,36(07).DOI:10.1063/5.0215308.
4. Zhang, Yunzhen,Cheng, Miao,Liu, Xiangyang, et al.The influence of plug nozzle and Laval nozzle on the flow field and performance of non-premixed rotating detonation combustor[J].PHYSICS OF FLUIDS,2024,36(05).DOI:10.1063/5.0207508.
5. He, XiaoJian,Gong, XiaoPeng,Wang, JianPing, et al.Investigation of the total pressure gain in rotating detonation combustors with dilution holes[J].PHYSICS OF FLUIDS,2024,36(04).DOI:10.1063/5.0195613.
6. He, XiaoJian,Wang, JianPing,Ma, John Z..Investigation of the evolution process and propulsion performance of the longitudinal pulsed detonation in rotating detonation combustors[J].PHYSICS OF FLUIDS,2024,36(03).DOI:10.1063/5.0187773.
7. Rong, Guangyao,Cheng, Miao,Sheng, Zhaohua, et al.Flow field characteristics and particle path tracking of a hollow rotating detonation engine with a Laval nozzle[J].PHYSICS OF FLUIDS,2023,35(05).DOI:10.1063/5.0144651.
8. Rong, Guangyao,Cheng, Miao,Zhang, Yunzhen, et al.Investigation of flow field characteristics and performance of carbon-hydrogen/oxygen-rich air rotating detonation engine[J].PHYSICS OF FLUIDS,2023,35(09).DOI:10.1063/5.0154599.
9. Sheng, Zhaohua,Cheng, Miao,Wang, JianPing.Multi-wave effects on stability and performance in rotating detonation combustors[J].PHYSICS OF FLUIDS,2023,35(07).DOI:10.1063/5.0144199.
10. Shen, Dawen,Sheng, Zhaohua,Zhang, Yunzhen, et al.Predicting combustion behavior in rotating detonation engines using an interpretable deep learning method[J].PHYSICS OF FLUIDS,2023,35(07).DOI:10.1063/5.0155991.
11. Wu, Wenbin,Wang, Yingnan,Wu, Kewen, et al.Experimental evaluation of aluminum powder fuel in a hydrogen/oxygen detonation tube[J].INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,2023,48(62):24089-24100.DOI:10.1016/j.ijhydene.2023.03.078.
12. He, XiaoJian,Liu, XiangYang,Wang, JianPing.Numerical study of the mechanisms of the longitudinal pulsed detonation in two-dimensional rotating detonation combustors[J].PHYSICS OF FLUIDS,2023,35(03).DOI:10.1063/5.0136290.
13. Rong, Guangyao,Cheng, Miao,Sheng, Zhaohua, et al.Investigation of counter-rotating shock wave and wave direction control of hollow rotating detonation engine with Laval nozzle[J].PHYSICS OF FLUIDS,2022,34(05).DOI:10.1063/5.0089207.
14. Rong, Guangyao,Cheng, Miao,Sheng, Zhaohua, et al.Investigation of counter-rotating shock wave phenomenon and instability mechanisms of rotating detonation engine with hollow combustor and Laval nozzle[J].INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,2022,47(54):23019-23037.DOI:10.1016/j.ijhydene.2022.05.082.
15. Zhu, Wenchao,Wang, Yuhui,Wang, Jianping.Flow field of a rotating detonation engine fueled by carbon[J].PHYSICS OF FLUIDS,2022,34(07).DOI:10.1063/5.0099787.
16. Sheng, Zhaohua,Cheng, Miao,Shen, Dawen, et al.An active direction control method in rotating detonation combustor[J].INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,2022,47(55):23427-23443.DOI:10.1016/j.ijhydene.2022.05.135.
荣誉奖励
1. 2012年，获十二五航空基金优秀项目奖。
2. 2011年，获Semenov and Zeldovich杰出论文奖。
3. 1999年，国家杰出青年基金。
4. 1998年，组织部、人事部、中国科协中国青年科技奖。
5. 1998年，中国力学学会青年科技奖。