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：北京理工大学空天科学与技术学院

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，空天科学与技术学院，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、临空飞行器复杂流动
2、激波与气相爆轰波
3、爆震推进气体动力学

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（现青A）
2、2018年获国家自然科学基金委优秀青年科学基金（现青B）
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、中国力学学会副秘书长
2、中国力学学会激波与激波管专业委员会、中国空天动力联合会爆震推进专业委员会副主任委员
3、中国力学学会流体力学专业委员会、中国航空学会燃烧与传热传质专业委员会、中国工程热物理学会爆震与新型推进专业委员会委员
4、 Chinese Journal of Aeronautics、《航空学报》、《推进技术》、《气体物理》期刊编委

近年来主要发表论文

教材：

[1] 滕宏辉, 王宽亮, 张义宁. 化学流体力学. 北京: 北京理工大学出版社, 2025.

[2] 董刚, 滕宏辉. 气相爆轰理论. 北京: 科学出版社, 2025.

专著：

[1] 滕宏辉, 杨鹏飞. 斜爆轰流动燃烧现象及其机理. 北京: 科学出版社, 2024.

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

期刊论文：

[1] W. Chang, H. Hu, Y. Xi, M. Kloker, H. Teng, J. Ren. Data-driven fine-grained prediction of laminar–turbulent transition in zero-pressure-gradient flat-plate boundary layers. Physics of Fluids, 2026, 38: 014103.

[2] T. Qiao, H. Xiong, W. Wu, H. Teng. Investigation on the cavitation characteristics induced by high-intensity focused ultrasonic waves in a near-wall region. Journal of Fluid Mechanics, 2026, 1028: A48.

[3] Z. Kang, R. Huang, Y. Huang, Y. Huang, Z. Liu, Z. Li, H. Teng, J. M. Floryan. Effect of salting-out on Marangoni spreading at a miscible interface. Journal of Fluid Mechanics, 2026, 1032: A20.

[4] S. Niu, P. Yang, Z. Zhang, H. Teng. Three-dimensional morphology and formation mechanism of tongue-shaped oblique detonation waves in elliptical flow channels. Combustion and Flame, 2025, 282: 114468.

[5] C. Xu, P. Yang, H. Teng. Effects of annular channel widths on wave system structures in wall-detached rotating detonation. Combustion and Flame, 2025, 278: 114249.

[6] W. Du, S. Niu, P. Yang, H. Teng. Destabilization mechanism of oblique detonation induced by the recirculation zone in a channel flow. Combustion and Flame, 2025, 280: 114401.

[7] L. Liu, B. Meng, H. Teng, B. Tian. Numerical investigation of particle transport and deposition mechanisms driven by multiphase explosion coupling with buffer gas stream. International Journal of Multiphase Flow, 2025, 192: 105336.

[8] Y. Guo, H. Luo, H. Xiong, Y. Li, J. Deng, W. Wu, H. Teng. Cavitation characteristics near the wall in the presence of an attached preset air bubble. Physics of Fluids, 2025, 37: 013305.

[9] W. Du, J. Ren, H. Teng. Sparse-sensor reconstruction of oblique detonation-wave temperature fields using a diffusion-guided residual coordinate-attention U-shaped network. Physics of Fluids, 2025, 37: 126117.

[10] 陆亚辉, 牛淑贞, 张子健, 滕宏辉. 侧壁约束下三维燃烧室斜爆轰结构的数值研究. 空气动力学学报, 2025, 43(10): 70−84.

[11] C. Tian, H. Teng, B. Shi, P. Yang, K. Wang, M. Zhao. Propagation instabilities of the oblique detonation wave in partially prevaporized n-heptane sprays. Journal of Fluid Mechanics, 2024, 984: A16.

[12] P. Yang, D. Yu, Z. Chen, H. Teng, H. D. Ng. Effects of thermal stratification on detonation development in hypersonic reactive flows. Physical Review Fluids, 2024, 9(8): 083202.

[13] H. Teng, S. Liu, Z. Li, P. Yang, K. Wang, C. Tian. Effect of ozone addition on oblique detonations in hydrogen-air mixtures. Applied Thermal Engineering, 2024, 240: 122292.

[14] Z. Zhao, C. Tian, J. Bian, Q. Liu, X. Wang, G. He, H. Teng. Numerical study on effects of a module-scale crater on lunar plume-surface interaction. Acta Mechanica Sinica, 2024, 40(5): 323626.

[15] C. Tian, Z. Zhao, Z. Sun, G. He, K. Wang, H. Teng. Numerical investigation of impinging plume under vacuum and realistic nozzle outlet condition. Physics of Fluids, 2024, 36: 013328.

[16] S. Niu, P. Yang, X. Xi, Z. Li, H. Teng. Evolution of weakly unstable oblique detonation in disturbed inflow. Physics of Fluids, 2024, 36: 016117.

[17] G. He, Z. Feng, K. Wang, H. Teng. Unsteady wave characteristics of oblique detonation wave in a contraction–expansion channel. International Journal of Hydrogen Energy, 2024, 71: 999–1005.

[18] 郗雪辰, 牛淑贞, 杨鹏飞, 杜文强, 何国胜, 滕宏辉. 氢气燃料斜爆轰发动机内波系对楔面调控的动态响应特性. 航空学报, 2024, 45(22): 130275.

[19] H. Teng, C. Tian, P. Yang, M. Zhao. Effect of droplet diameter on oblique detonations with partially pre-vaporized n–heptane sprays. Combustion and Flame, 2023, 258: 113062.

[20] L. Zhou, S. Tu, Y. Zhang, P. Yang, H. Teng. Numerical investigation of oblique detonation waves on a truncated cone in hydrogen–air mixtures. Physics of Fluids, 2023, 35: 116114.

[21] S. Niu, P. Yang, K. Wang, H. Teng. Unsteady oblique detonation waves in a tunnel induced by inflow mach number variation. Aerospace, 2023, 10(4): 330.

[22] Z. Feng, K. Wang, H. Teng. Numerical Investigation of the Oblique Detonation Waves and Stability in a Super-Detonative Ram Accelerator. Aerospace, 2023, 10(6): 549.

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

[24] 牛淑贞, 杨鹏飞, 杨旸, 滕宏辉. 来流速度突变对斜爆轰反射波系驻定特性影响的数值研究. 中国科学: 物理学力学天文学, 2023, 53: 234711.

[25] 张义宁, 金虹, 涂胜甲, 周林, 滕宏辉. 环形燃烧室中圆台斜爆震燃烧特性研究. 推进技术, 2023, 44(12): 119–129.

[26] 刘思远, 汪洋, 李真珍, 滕宏辉, 田诚. 中心锥喷管喉道比参数对旋转爆轰燃烧影响的数值研究. 推进技术, 2023, 44(9): 115–126.

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

[28] 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.

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

[30] 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.

[31] 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.

[32] 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.

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

[34] 郗雪辰, 杨鹏飞, 滕宏辉. 一维爆轰波在扰动来流中传播的数值研究. 气体物理, 2022, 7(4): 1–9.

[35] 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.

[36] L. Zhou, H. Teng, H. D. Ng, P. Yang, Z. Jiang. Reconstructing shock front of unstable detonations based on multi-layer perceptron. Acta Mechanica Sinica, 2021, 37(11): 1610–1623.

[37] 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.

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

[39] 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.

[40] 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.

[41] 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.

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

[43] 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.

[44] 刘帅, 张子健, 滕宏辉. 不同直径圆球诱导燃烧的振荡机制与频率特性. 推进技术, 2021, 42(4): 745-754.

[45] 边靖, 周林, 滕宏辉. 两种前体压缩方式对斜爆震燃烧影响的数值研究. 推进技术, 2021, 42(4): 815-825.

[46] 王兵, 谢峤峰, 闻浩诚, 滕宏辉, 张义宁, 周林. 爆震发动机研究进展. 推进技术, 2021, 42(4): 721–737.

[47] 杨旸, 滕宏辉, 姜宗林. 三维双楔面定常超声速流动研究. 空气动力学学报, 2021, 30(6): 713–718.

[48] 汪球, 赵伟, 滕宏辉, 姜宗林. 高焓激波风洞喷管流场非平衡特性研究. 空气动力学学报, 2021, 33(1): 66–71.

[49] 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. Journal of Fluid Mechanics, 2020, 903: A28.

[50] 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.

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

[52] 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: 046101.

[53] 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.

[54] 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.

[55] 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.

[56] 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: 090008.