滕宏辉_北京理工大学宇航学院

力学系

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正高级职称（按拼音排序）

滕宏辉

所在学科：力学

联系电话：

通讯地址：北京理工大学宇航学院　

职称：教授，博导

邮箱：hhteng@bit.edu.cn

邮编：100081

教育经历

2003年09月–2008年07月，在中国科学院力学研究所获得流体力学博士学位
1999年09月–2003年07月，在中国科学技术大学获得理论与应用力学学士学位

工作经历

　2018年08月–至今，北京理工大学，宇航学院，教授
　2017年06月–2018年08月，北京理工大学宇航学院，副教授
　2011年12月–2017年05月，中国科学院力学研究所，副研究员
　2010年08月–2011年12月，中国科学院力学研究所，助理研究员
　2008年10月–2010年08月，中国科学院物理研究所，博士后

主要研究领域

1、激波与气相爆轰波
2、爆震推进中的流动问题
3、复杂介质气体动力学

获奖情况

1、2023年获国家自然科学基金委杰出青年科学基金
2、2018年获国家自然科学基金委优秀青年科学基金
3、2016年获中国科学院杰出科技成就奖
4、2014年入选中国科学院青年创新促进会

社会兼职

1、《推进技术》、《气体物理》编辑委员会委员
2、《力学学报》、《航空学报》中英文版编辑委员会青年委员
3、中国力学学会高温气体动力学专业组成员
4、中国航空学会燃烧与传热传质专业委员会委员
5、中国工程热物理学会爆震与新型推进专业委员会委员

近年来主要发表论文

[1]Z. Jiang, H. Teng. Gaseous Detonation Physics and Its Universal Framework Theory. Singapore: Springer, 2022.（专著）

[2]S. Niu, P. Yang, Y. Yang, H. Teng. Numerical study of the effect of a sudden change in inflow velocity on the stability of an oblique detonation reflected wave system (in Chinese). Sci Sin-Phys Mech Astron, 2023, 53, 234711

[3]G. Bakalis, M. Valipour, J. Bentahar, L. Kadem, H. Teng, H. Ng. Detonation cell size prediction based on artificial neural networks with chemical kinetics and thermodynamic parameters. Fuel Communications, 2023, 14, 100084.

[4]K. Yao, P. Yang, H. Teng, Z. Chen, C. Wang. Effects of injection parameters on propagation patterns of hydrogen-fueled rotating detonation waves. international journal of hydrogen energy, 2022, 47 (91), 38811−38822.

[5]A. Wang, J. Bian, H. Teng. Numerical study on initiation of oblique detonation wave by hot jet. Applied Thermal Engineering, 2022, 213, 118679.

[6]P. Yang, H. Li, Z. Chen, C. Wang, H. Teng. Numerical investigation on movement of triple points on oblique detonation surfaces. Physics of Fluids, 2022, 34, 066113.

[7]J. Bian, L. Zhou, P. Yang, H. Teng, H. D. Ng. A reconstruction method of detonation wave surface based on convolutional neural network. Fuel, 2022, 315, 123068.

[8]H. Teng, X. Xi, K. Wang, P. Yang. Instability of wave complex resulting from oblique detonation decoupling. Acta Mechanica Sinica, 2022, 38 (5), 121391.

[9]X. Xi, H. Teng, Z. Chen, P. Yang. Effects of longitudinal disturbances on two-dimensional detonation waves. Physical Review Fluids, 2022, 7 (4), 043201.

[10]H. Teng, Y. Zhang, P. Yang, Z. Jiang. Oblique detonation wave triggered by a double wedge in hypersonic flow. Chinese Journal of Aeronautics, 2022, 35 (4), 176−184.

[11]P. Yang, Z. Zhang, R. Yang, H. Teng, Z. Jiang. Theorical study on propulsive performance of oblique detonation engine. Chinese Journal of Theoretical and Applied Mechanics, 2021, 53 (10), 2853−2864.

[12]C. Yan, H. Teng, H. D. Ng. Effects of slot injection on detonation wavelet characteristics in a rotating detonation engine. Acta Astronautica, 2021, 182, 274−285.

[13]H. Teng, C. Tian, Y. Zhang, L. Zhou, H. D. Ng. Morphology of oblique detonation waves in a stoichiometric hydrogen-air mixture. Journal of Fluid Mechanics, 2021, 913, A1.

[14]H. Teng; H.D. Ng; P. Yang; K. Wang. Near-field relaxation subsequent to the onset of oblique detonations with a two-step kinetic model. Physics of Fluids, 2021, 33, 096106.

[15]P. Yang, H. D. Ng, H. Teng. Unsteady dynamics of wedge-induced oblique detonations under periodic inflows. Phys. Fluids, 2021, 33, 016107.

[16]H. Teng, J. Bian, L. Zhou, Y. Zhang. A numerical investigation of oblique detonation waves in hydrogen-air mixtures at low mach numbers. International Journal of Hydrogen Energy, 2021, 46 (18), 10984−10994.

[17]J. Bian, L. Zhou, H. Teng. Structural and thermal analysis on oblique detonation influenced by different forebody compressions in hydroge-air mixtures. Fuel, 2021, 286, 119458.

[18]K. Wang, P. Yang, H. Teng. Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner. Aerospace Science and Technology, 2021, 112, 106592.

[19]L. Zhou, H. Teng, H.D. Ng, P. Yang, Z. Jiang. Reconstructing shock front of unstable detonations based on Multi-Layer Perceptron, Acta Mechanics Sinica, 2021, 37(11), 1612−1625.

[20]杨鹏飞, 张子健, 杨瑞鑫, 滕宏辉, 姜宗林. 斜爆轰发动机的推力性能理论分析. 力学学报, 2021, 53(10), 2853-2864.

[21]K. Wang, H. Teng, P. Yang, H.D. Ng. Numerical investigation of flow structures resulting from the interaction between an oblique detonation wave and an upper expansion corner. J. Fluid Mech., 2020, 903, A28.

[22]K. Wang, Z. Zhang, P. Yang, H. Teng. Numerical study on reflection of an oblique detonation wave on an outward turning wall. Physics of Fluids, 2020, 32 (4), 046101.

[23]H. Teng, S. Liu, Z. Zhang. Unsteady combustion mode with a super-high frequency induced by a curved shock. Phys. Fluids, 2020, 32, 116101.

[24]G. Xiang, P. Yang, H. Teng, Z. Jiang. Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model. Combustion Science and Technology, 2020, 192(10), 1931−1945.

[25]Y. Zhang, L. Zhou, H. Meng, H. Teng. Reconstructing cellular surface of gaseous detonation based on artificial neural network and proper orthogonal decomposition. Combustion and Flame, 2020, 212, 156−164.

[26]H. Teng, L. Zhou, P. Yang, Z. Jiang. Numerical investigation of wavelet features in rotating detonations with a two-step induction-reaction model. International Journal of Hydrogen Energy, 2020, 45 (7), 4991−5001.

[27]滕宏辉, 杨鹏飞, 张义宁, 周林. 斜爆震发动机的流动与燃烧机理. 中国科学：物理学力学天文学 2020, 50(9), 090008.

[28]滕宏辉, 姜宗林. 斜爆轰的多波结构及其稳定性研究进展. 力学进展. 2020, 50, 202002.

[29]P. Yang, H. D. Ng, H. Teng. Numerical study of wedge-induced oblique detonations in unsteady flow. Journal of Fluid Mechanics, 2019, 876, 264−287.

[30]C. Yan, H. Teng, X. Mi, H. D. Ng. The Effect of Chemical Reactivity on the Formation of Gaseous Oblique Detonation Waves. Aerospace, 2019, 6 (6), 62.

[31]C. Tian, H. Teng, H. D. Ng. Numerical investigation of oblique detonation structure in hydrogen-oxygen mixtures with Ar dilution. FUEL, 2019, 252, 496−503.

[32]Y. Zhang, Y. Fang, H. D. Ng, H. Teng. Numerical investigation on the initiation of oblique detonation waves in stoichiometric acetylene-oxygen mixtures with high argon dilution. Combust. Flame, 2019, 204, 391−396.

[33]Y. Fang, Y. Zhang, X. Deng, H. Teng. Numerical study of wedge-induced oblique detonation in acetylene-oxygen-argon mixtures. Phys. Fluids, 2019, 31, 026198.

[34]P. Yang, H. Teng, H. D. Ng, Z. Jiang. Instability of oblique detonation surface with a two-step induction-reaction kinetic model. Proc. Combust. Inst., 2019, 37, 3537−3544.

[35]X. Deng, B. Xie, H. Teng, F. Xiao. High resolution multi-moment finite volume method for supersonic combustion on unstructured grids. Applied Mathematical Modelling, 2019, 66, 404–423.

[36]X. Deng, B. Xie, F. Xiao, H. Teng. New accurate and efficient method for stiff detonation capturing. AIAA Journal, 2018, 56, 4024−4038.

[37]Y. Fang, Z. Hu, H. Teng. Numerical investigation of oblique detonations induced by a finite wedge in a stoichiometric hydrogen-air mixture. FUEL, 2018, 234, 502−507.