副高级
副高级
姚松柏
姚松柏，副研究员，硕士生导师
研究方向包括：爆轰推进技术、数据驱动燃烧计算方法。
邮箱：yaosongbai@nimte.ac.cn
2018-2021年在德国斯图加特大学燃烧技术研究所开展博士后研究。
作为项目负责人承担国家自然科学基金、宁波市自然科学基金等项目，现任《推进技术》、《航空动力学报》、《空天技术》、《火箭推进》等期刊青年编委，国际燃烧学会会员。已发表SCI论文20余篇，引用超过800次，出版专著2本。Combustion and Flame、Aerospace Science And Technology、AIAA Journal、Physics of Fluids、Fuel、Energy & Fuels等期刊审稿人。
代表性论文：
[1] J. Li, S. Yao, J. Yu, J. Li, Y. Lei, W. Zhang, Shock interactions and re-initiation mechanism of liquid ethanol-fueled rotating detonation wave, Phys. Fluids 36 (2024).
[2] J. Yu, S. Yao, J. Li, J. Li, R. Wang, W. Zhang, Experimental investigation of the hydrogen-air rotating detonation engine with cat-ear-shaped film cooling holes, Int. J. Hydrogen Energy 89 (2024) 1454–1465.
[3] J. Yu, S. Yao, J. Li, J. Li, C. Guo, W. Zhang, Numerical investigation of the rotating detonation engine with cat-ear-shaped film cooling holes under varying operating modes, Aerospace Sci. Technol. 142 (2023) 108642.
[4] S. Yao, X. Tang, W. Zhang, Structure of a heterogeneous two-phase rotating detonation wave with ethanol–hydrogen–air mixture, Phys. Fluids 35 (2023) 031712.
[5] S. Yao, X. Tang, W. Zhang, Adaptive operating mode switching process in rotating detonation engines, Acta Astronautica 205 (2023) 239–246.
[6] J. Li, Y. Lei, S. Yao, J. Yu, J. Li, W. Zhang, Investigation of multi-stage evaporation and wave multiplicity of two-phase rotating detonation waves fueled by ethanol, Acta Astronautica 213 (2023) 418–430.
[7] S. Yao, A. Kronenburg, O.T. Stein, Efficient modeling of the filtered density function in turbulent sprays using ensemble learning, Combust. Flame 237 (2022) 111722.
[8] S. Yao, A. Kronenburg, A. Shamooni, O.T. Stein, W. Zhang, Gradient boosted decision trees for combustion chemistry integration, Appl. Energy Combust. Sci. 11 (2022) 100077.
[9] S. Yao, B. Wang, A. Kronenburg, O.T. Stein, Conditional scalar dissipation rate modeling for turbulent spray flames using artificial neural networks, Proc. Combust. Inst. 38 (2021) 3371–3378.
[10] S. Yao, X. Tang, M. Luan, J. Wang, Numerical study of hollow rotating detonation engine with different fuel injection area ratios, Proc. Combust. Inst. 36 (2017) 2649–2655.
