5123导航取五湖之利取四-欢迎莅临

Professor of Aerospace Science and Technology & Fluid Mechanics

Tel:8610-62782154

E-mail address:wbing@tsinghua.edu.cn

Introduction

Wang Bing, Alexander von Humboldt Scholar, Ph.D. supervisor, PhD in Engineering

Professor Wang Bing has a long experience in basic and engineering application researches in two-phase flows and reactive flows under extreme conditions. Throughout his career, he has served as the principal investigator or a key participant in over 40 major national engineering projects. His research contributions are widely recognized, as evidenced by his publication of over 160 papers in SCI indexed journals, including renowned publications such as Progress of Aerospace Sciences, Journal of Fluid Mechanics, Combustion and Flame, Physics of Fluids and Aerospace Science and Technology. Additionally, he has presented over 70 conference papers and holds the distinction of being a co-inventor of more than 15 Chinese and international patents.

Professor Wang Bing's exceptional achievements have been honored with numerous accolades. He has received multiple prestigious golden awards at world-class international invention exhibitions and has been recognized with the Beijing Municipal Award for Scientific Progress. Furthermore, he holds the distinguished status of being an Associate Fellow of the American Institute of Aeronautics and Astronautics (AIAA). In 2019, the Technical University of Munich bestowed upon him the honorary title of "TUM Ambassador."

Contact information:

Phone: 010-62782154

Email: wbing@tsinghua.edu.cn

Education

Sept. 1996 - Jul. 2000, Bachelor, Engineering Thermo-physics, Department of Engineering Mechanics, Tsinghua University

Sept. 2000 - Jan. 2005, Master and Doctor, Power and Thermo-physics, School of Aerospace Engineering (Department of Engineering Mechanics), Tsinghua University

Experience

Mar. 2005 - Present, Assistant Professor, Associate Professor and Professor, School of Aerospace Engineering, Tsinghua University

Oct. 2006- Apr. 2008, Humboldt Fellow, Technische Universitaet Muenchen

Research Interests

A. Fundamentals of turbulent combustion and multiphase flows, such as ignition, two-phase flows, and steady combustion, especially under the extreme operation conditions of different modern engines.

B. Combustion instabilities of, high-pressure diffusion in Liquid Rocket Engine(LRE), supersonic partial premixing in Scramjet, lean premixing in Aero-Turbine, detonation in Rotation Detonation Engine, etc.

C. Numerical simulation (CFD) and modern numerical schemes, such as Large eddy Simulation (LES), hybrid WENO scheme.

D. New conception propulsion, energy and environment science & application such as cavitations triggering and bubble collapse, as well as their interaction in multi-physics.

Publication

A. Extreme compressible two-phase flow mathematical modelling and physical mechanism

Sheng, X.; Fan, W.; Wu, W.; Wen, H.; Wang, B.*; 2023. Analysis of Wave Converging Phenomena inside the Shocked Two-Dimensional Cylindrical Water Column, Journal of Fluid Mechanics, 964. https://doi.org/10.1017/jfm.2023.239

王兵; 范文琦; 徐胜; 高瞻; 2022. 极端条件两相界面流与反应流机理、模型与算法研究进展, 气体物理, 7(06): 1-32. https://doi.org/10.19527/j.cnki.2096-1642.0941

Jin, X.; Cheng, X.; Wang, Q.; Wang, B.; 2022. Numerical simulation for rarefied hypersonic flows over non-rectangular deep cavities, Physics of Fluids, 34(8). https://doi.org/10.1063/5.0102685

吴汪霞; 王兵; 王晓亮; 刘青泉; 2021. 非等强度多道冲击波作用下空泡溃灭机制分析, 航空学报, 40(12): 625894-625894. https://doi.org/10.7527/S1000-6893.2021.25894

Gao, Z.; Wu, W.; Wang, B.*; 2021. The effects of nanoscale nuclei on cavitation, Journal of Fluid Mechanics, 911, A20. https://doi.org/10.1017/jfm.2020.1049

Gao, Z.; Wu, W.; Sun, W.; Wang, B.*; 2021. Understanding the stabilization of a bulk nanobubble: a molecular dynamics analysis, Langmuir, 37(38), 11281-11291. https://doi.org/10.1021/acs.langmuir.1c01796(封面文章)

Wu, W.; Liu, Q.; Wang, B.; 2021. The effects of nanoscale nuclei on cavitation, 25th International Congress of Theoretical and Applied Mechanics - ICTAM, 2020+1, Milan, Italy, on August 22-27, 2021.

Wu, W.; Liu, Q.; Wang, B.*; 2021. Curved surface effect on high-speed droplet impingement, Journal of Fluid Mechanics, 909, A7. https://doi.org/10.1017/jfm.2020.926

Wu, W.; Wang, B.; Liu, Q.*; 2021. Tandem cavity collapse in a high-speed droplet impinging on a 180° constrained wall, Journal of Fluid Mechanics, 932, A52. https://doi.org/10.1017/jfm.2021.1044.

Xiang, G.; Ren, Z.; Kim, S.; Wang, B.*; 2020. Numerical analysis on the disintegration of gas-liquid interface in two-phase shear-layer flows, Aerospace Science and Technology, 98, 105710. https://doi.org/10.1016/j.ast.2020.105710

Wu, W.; Wang, B.*; Xiang, G.; 2019. Impingement of high-speed cylindrical droplets embedded with an air/vapour cavity on a rigid wall: numerical analysis, Journal of Fluid Mechanics, 864, 1058–1087. https://doi.org/10.1017/jfm.2019.55

Xiang, G.; Wang, B.*; 2019. Theoretical and numerical studies on shock reflection at water/air two-phase interface: fast-slow case, International Journal of Multiphase Flow, 114, 219–228. https://doi.org/10.1016/j.ijmultiphaseflow.2019.03.002

Zhang, C.; Xiang, G.M.; Wang, B.; Hu, X.Y.*; Adams, N.A.; 2019. A weakly compressible SPH method with WENO reconstruction, Journal of Computational Physics, 392, 1–18. https://doi.org/10.1016/j.jcp.2019.04.038

Herty, M.; Müller, S.*; Gerhard, N.; Xiang, G.; Wang, B.; 2018. Fluid-structure coupling of linear elastic model with compressible flow models, International Journal for Numerical Methods in Fluids, 86, 365–391. https://doi.org/10.1002/fld.4422

Wang, B.; Xiang, G.; Hu, X.Y.*; 2018. An incremental-stencil WENO reconstruction for simulation of compressible two-phase flows, International Journal of Multiphase Flow, 104, 20–31. https://doi.org/10.1016/j.ijmultiphaseflow.2018.03.013

Wu, W.; Xiang, G.; Wang, B.*; 2018. On high-speed impingement of cylindrical droplets upon solid wall considering cavitation effects, Journal of Fluid Mechanics, 857, 851–877. https://doi.org/10.1017/jfm.2018.753

Xiang, G.; Wang, B.*; 2018. Numerical investigation on the interaction of planar shock wave with an initial ellipsoidal bubble in liquid medium, AIP Advances, 8, 075128. https://doi.org/10.1063/1.5047570(编辑精选)

Xiang, G.; Wang, B.*; 2017. Numerical study of a planar shock interacting with a cylindrical water column embedded with an air cavity, Journal of Fluid Mechanics, 825, 825–852. https://doi.org/10.1017/jfm.2017.403

Zhang, P.; Wang, B.*; 2017. Effects of elevated ambient pressure on the disintegration of impinged sheets, Physics of Fluids, 29, 042102. https://doi.org/10.1063/1.4981777

Hu, X.Y.*; Wang, B.; Adams, N.A.; 2015. An efficient low-dissipation hybrid weighted essentially non-oscillatory scheme, Journal of Computational Physics, 301, 415–424. https://doi.org/10.1016/j.jcp.2015.08.043

B.Extreme reactive flow mechanism and dynamics

Chen, Q.*; Wang B.*; 2021. The spatial growth of supersonic reacting mixing layers: Effects of combustion mode, Aerospace Science and Technology, 116, 106888. https://doi.org/10.1016/j.ast.2021.106888.

Shahsavari, M.; Wang, B.*; Zhang, B.; Jiang, G.; Zhao, D.; 2021. Response of supercritical round jets to various excitation modes, Journal of Fluid Mechanics, 915, A47. https://doi.org/10.1017/jfm.2021.78

Ren, Z.; Wang, B.*; Xiang, G.; Zhao, D.; Zheng, L.; 2019. Supersonic spray combustion subject to scramjets: progress and challenges, Progress in Aerospace Sciences, 105, 40–59. https://doi.org/10.1016/j.paerosci.2018.12.002

Ren, Z.; Wang, B.*; Zhang, F.; Zheng, L.; 2019. Effects of eddy shocklets on the segregation and evaporation of droplets in highly compressible shear layers, AIP Advances, 9, 125101. https://doi.org/10.1063/1.5125121

Ren, Z.; Wang, B.*; Hu, B.; Zheng, L.; 2018. Numerical analysis of supersonic flows over an aft-ramped open-mode cavity, Aerospace Science and Technology, 78, 427–437. https://doi.org/10.1016/j.ast.2018.05.003

Ren, Z.; Wang, B.*; Zhao, D.; Zheng, L.; 2018. Flame propagation involved in vortices of supersonic mixing layers laden with droplets: Effects of ambient pressure and spray equivalence ratio, Physics of Fluids, 30, 106107. https://doi.org/10.1063/1.5049840

Ren, Z.; Wang, B.*; Zheng, L.; 2018. Numerical analysis on interactions of vortex, shock wave, and exothermal reaction in a supersonic planar shear layer laden with droplets, Physics of Fluids, 30, 036101. https://doi.org/10.1063/1.5011708 (特色文章)

Ren, Z.; Wang, B.*; Zheng, L.; Zhao, D.; 2018. Numerical studies on supersonic spray combustion in high-temperature shear flows in a scramjet combustor, Chinese Journal of Aeronautics, 31, 1870–1879. https://doi.org/10.1016/j.cja.2018.06.020

Ren, Z.; Wang, B.*; Xie, Q.; Wang, D.; 2017. Thermal auto-ignition in high-speed droplet-laden mixing layers, Fuel, 191, 176–189. https://doi.org/10.1016/j.fuel.2016.11.073

Ren, Z.; Wang, B.*; Yang, S.; Xie, Q.; Liu, H.; Wang, D.; 2017. Evolution of flame kernel in one eddy turnover of high-speed droplet laden shear layers, Journal of Loss Prevention in the Process Industries, 49, 938–946. https://doi.org/10.1016/j.jlp.2017.05.009

Wang, B.*; Wei, W.; Zhang, Y.; Zhang, H.; Xue, S.; 2015. Passive scalar mixing in Mc <1 planar shear layer flows, Computers & Fluids, 123, 32–43. https://doi.org/10.1016/j.compfluid.2015.09.006

Zhang, Y.; Wang, B.*; Zhang, H.; Xue, S.; 2015. Mixing enhancement of compressible planar mixing layer impinged by oblique shock waves, Journal of Propulsion and Power, 31, 156–169. https://doi.org/10.2514/1.B35423

C.Continuous rotating detonation and oblique detonation

Wen, H.; Fan, W.; Xu, S.; Wang, B.*; 2023. Numerical Study on Droplet Evaporation and Propagation Stability in Normal-Temperature Two-Phase Rotating Detonation System, Aerospace Science and Technology, 138. https://doi.org/10.1016/j.ast.2023.108324

Yan, C.; Nie, W.; Wang, B.; Lin, W.*; 2023. Rotating Detonation Combustion of Liquid Kerosene under near-Ramjet Limit Conditions, AIP Advances, 13(6). https://doi.org/10.1063/5.0157988

Wen, H.; Fan, W.; Wang, B.*; 2023. Theoretical analysis on the total pressure gain of rotating detonation systems, Combustion and Flame, 248. https://doi.org/10.1016/j.combustflame.2022.112582

Ren, Z.; Sun, Y.; Wang B.*; 2022. Propagation behaviors of the rotating detonation wave in kerosene-air two-phase mixtures with wide equivalence ratios, Flow Turbulence and Combustion, 110, 735-753. https://doi.org/10.1007/s10494-022-00393-z

Wen, H.; Wei, W.; Fan, W.; Xie, Q.; Wang, B.*; 2022. On the propagation stability of droplet-laden two-phase rotating detonation waves. Combustion and Flame, 244. https://doi.org/10.1016/j.combustflame.2022.112271

Zhang, B.; Shahsavari, M.; Chen, J.; Wen, H.; Wang, B.; Tian, X.; 2022. The propagation characteristics of particle-laden two-phase detonation waves in pyrolysis mixtures of C(s)/H2/CO/CH4/O2/N2, Aerospace Science and Technology, 130. https://doi.org/10.1016/j.ast.2022.107912

师迎晨; 张任帅; 计自飞; 王兵; 2022. 高速飞行器的连续旋转爆震推进技术, 空气动力学学报, 40(01): 101-113.

Ji, Z.; Zhang, B.; Zhang, H.; Wang, B.*; Wang, C.; 2022. Reduction of feedback pressure perturbation for rotating detonation combustors, Aerospace Science and Technology, 126, 1070635. https://doi.org/10.1016/j.ast.2022.107635

Zhang, B.; Chen, J.; Shahsavari, M.; Wen, H.; Wang, B.; Tian, X.; 2022. Effects of Inert Dispersed Particles on the Propagation Characteristics of a H2/Co/Air Detonation Wave, Aerospace Science and Technology, 126, 107660. https://doi.org/10.1016/j.ast.2022.107660

王兵, 谢峤峰, 闻浩诚, 滕宏辉, 张义宁 周林 2021. 爆震发动机研究进展, 推进技术, 42(04): 721-737+716.

Ji, Z.; Zhang, H.; Wang, B.*; 2021. Thermodynamic performance analysis of the rotating detonative airbreathing combined cycle engine, Aerospace Science and Technology 113, 106694. https://doi.org/10.1016/j.ast.2021.106694.

Ren, Z.; Wang, B.*; Zheng, L.; 2021. Wedge-induced oblique detonation waves in supersonic kerosene-air premixing flows with oscillating pressure, Aerospace Science and Technology, 110. https://doi.org/10.1016/j.ast.2020.106472

Ren, Z.,; Wang, B.*; Wen, J.; Zheng, L.; 2021. Stabilization of wedge-induced oblique detonation waves in pre-evaporated kerosene–air mixtures with fluctuating equivalence ratios, Shock Waves, 31(7), 727-739. https://doi.org/10.1007/s00193-021-01050-6

Ji, Z.; Duan, R.; Zhang, R.; Zhang, H.; Wang, B.*; 2020. Comprehensive performance analysis for the rotating detonation-based turboshaft engine, International Journal of Aerospace Engineering, 9587813. https://doi.org/10.1155/2020/9587813

Ji, Z.; Zhang, H.; Wang, B.*; He, W.; 2020. Comprehensive performance analysis of the turbofan with a multi-annular rotating detonation duct burner, Journal of Engineering for Gas Turbines and Power-Transactions 142(2), 021007. https://doi.org/10.1115/1.4045518

Ma, J.; Luan, M.; Xia, Z..; Wang, J.*; Zhang, S.; Yao, S.; Wang, B.; 2020. Recent progress, development trends, and consideration of continuous detonation engines, AIAA Journal, 58(12), 4976-5035. https://doi.org/10.2514/1.J058157

Ren, Z.; Wang, B.*; 2020. Numerical study on stabilization of wedge-induced oblique detonation waves in premixing kerosene-air mixtures, Aerospace Science and Technology, 107, 106245. https://doi.org/10.1016/j.ast.2020.106245

Wang, B.; Wang, J.; 2020. Introduction to the special section on recent progress on rotating detonation and its application, AIAA Journal, 58(12), 4974-4975. https://doi.org/10.2514/1.J060144

Wen, H.; Wang, B.*; 2020. Experimental study of perforated-wall rotating detonation combustors, Combustion and Flame, 213, 52-62. https://doi.org/10.1016/j.combustflame.2019.11.028

He, W.; Xie, Q.; Ji, Z.; Rao, Z.; Wang, B.*; 2019. Characterizing continuously rotating detonation via nonlinear time series analysis, Proceedings of the Combustion Institute, 37, 3433–3442. https://doi.org/10.1016/j.proci.2018.07.045

Ji, Z.; Zhang, H.; Wang, B.*; 2019. Performance analysis of dual-duct rotating detonation aero-turbine engine, Aerospace Science and Technology, 92, 806–819. https://doi.org/10.1016/j.ast.2019.07.011

Ren, Z.; Wang, B.*; Xiang, G.; Zheng, L.; 2019. Numerical analysis of wedge-induced oblique detonations in two-phase kerosene–air mixtures, Proceedings of the Combustion Institute, 37, 3627–3635. https://doi.org/10.1016/j.proci.2018.08.038

Wen, H.; Xie, Q.; Wang, B.*; 2019. Propagation behaviors of rotating detonation in an obround combustor, Combustion and Flame, 210, 389–398. https://doi.org/10.1016/j.combustflame.2019.09.008

Xie, Q.; Wang, B.*; Wen, H.; He, W.; 2019. Thermoacoustic instabilities in an annular rotating detonation combustor under off-design condition, Journal of Propulsion and Power, 35, 141–151. https://doi.org/10.2514/1.B37044

Xie, Q.; Wang, B.*; Wen, H.; He, W.; Wolanski, P.; 2019. Enhancement of continuously rotating detonation in hydrogen and oxygen-enriched air, Proceedings of the Combustion Institute, 37, 3425–3432. https://doi.org/10.1016/j.proci.2018.08.046

Ren, Z.; Wang, B.*; Xiang, G.; Zheng, L.; 2018. Effect of the multiphase composition in a premixed fuel–air stream on wedge-induced oblique detonation stabilisation, Journal of Fluid Mechanics, 846, 411–427. https://doi.org/10.1017/jfm.2018.289

Xie, Q.; Wen, H.; Li, W.; Ji, Z.; Wang, B.*; Wolanski, P.; 2018. Analysis of operating diagram for H2/Air rotating detonation combustors under lean fuel condition, Energy, 151, 408–419. https://doi.org/10.1016/j.energy.2018.03.062

Zheng, D.; Wang, B.*; 2018. Utilization of nonthermal plasma in pulse detonation engine ignition, Journal of Propulsion and Power, 34, 539–549. https://doi.org/10.2514/1.B36591

D.Combustion instability mechanisms, modelling and control

Rao, Z.; Li, R.; Zhao, P.; Wang, B.*; Zhao, D.; Xie, Q.; 2022. Similarity phenomena of lean swirling flames at different bulk velocities with acoustic disturbances, Chinese Journal of Aeronautics. https://doi.org/10.1016/j.cja.2022.07.001

Saqib Akhtar, M.; Shahsavari, M.; Ghosh, A.; Wang, B.*; Hussain, Z.; Rao, Z.; 2023. Effect of fuel reactivity on flame properties of a low-swirl burner, Experimental Thermal and Fluid Science, 142. https://doi.org/10.1016/j.expthermflusci.2022.110795

Li, W.; Zhao, D.*; Chen,X.; Sun, Y.; Ni, S.; Guan, D.;Wang, B.; 2021. Numerical investigations on solid-fueled ramjet inlet thermodynamic properties effects on generating self-sustained combustion instability, Aerospace Science and Technology, 119, 107097. https://doi.org/10.1016/j.ast.2021.107097

Rao, Z.; Li, R.; Zhang, B.; Wang, B.*; Zhao, D.; Akhtar, M.S.; 2021. Experimental investigations of equivalence ratio effect on nonlinear dynamics features in premixed swirl-stabilized combustor, Aerospace Science and Technology, 112,106601. https://doi.org/10.1016/j.ast.2021.106601

Rao, Z.; Li, R.; Zhang, B.; Wang, B.*; Zhao, D.; Shahsavari, M.; 2021. Nonlinear dynamics of a swirl-stabilized combustor under acoustic excitations: influence of the excited combustor natural mode oscillations, Flow, Turbulence and Combustion, 107, 683-708. https://doi.org/10.1007/s10494-021-00249-y

Shahsavari, M.*; Farshchi, M.; Arabnejad, M.H.; Wang, B.; 2021. The role of flame–flow interactions on lean premixed lifted flame stabilization in a low swirl flow, Combustion Science and Technology, 1-26. https://doi.org/10.1080/00102202.2021.1976766

Zhang, B.;Shahsavar, M.; Rao, Z.; Yang, S.; Wang, B.*; 2021. Thermoacoustic Instability Drivers and Mode Transitions in a Lean Premixed Methane-Air Combustor at Various Swirl Intensities, Proceedings of the Combustion Institute, 38(4): 6115-6124. https://doi.org/10.1016/j.proci.2020.06.226

Ji, S.; Wang, B.*; Zhao, D.; 2020. Numerical analysis on combustion instabilities in end-burning-grain solid rocket motors utilizing pressure-coupled response functions, Aerospace Science and Technology, 98, 105701. https://doi.org/10.1016/j.ast.2020.105701

Qin, J.; Zhou, L.; Zhang, H.*; Wang, B.; 2020. Numerical evaluation of acoustic characteristics of a thrust chamber with quarter-wave resonators, Science China-Technological Sciences, 64, 375-386. https://doi.org/10.1007/s11431-019-1575-6

Sun, Y.; Rao, Z.; Zhao, D.*; Wang, B.; Sun, D.; Sun, X.; 2020. Characterizing nonlinear dynamic features of self-sustained thermoacoustic oscillations in a premixed swirling combustor, Applied Energy, 264, 114698. https://doi.org/10.1016/j.apenergy.2020.114698

Zhang, B.; Shahsavari, M.; Rao, Z.; Li, R.; Yang, S.; Wang, B.*; 2020. Effects of the fresh mixture temperature on thermoacoustic instabilities in a lean premixed swirl-stabilized combustor, Physics of Fluids, 32, 047101. https://doi.org/10.1063/1.5133859

Ji, S.; Wang, B.*; 2019. Modeling and analysis of triggering pulse to thermoacoustic instability in an end-burning-grain model solid rocket motor, Aerospace Science and Technology, 95, 105409. https://doi.org/10.1016/j.ast.2019.105409

Shahsavari, M.*; Farshchi, M.; Chakravarthy, S.R.; Chakraborty, A.; Aravind, I.B.; Wang, B.; 2019. Low swirl premixed methane-air flame dynamics under acoustic excitations, Physics of Fluids, 31, 095106. https://doi.org/10.1063/1.5118826 (Editor's Pick)

Zhang, B.; Shahsavari, M.; Rao, Z.; Yang, S.; Wang, B.; 2019. Contributions of hydrodynamic features of a swirling flow to thermoacoustic instabilities in a lean premixed swirl stabilized combustor, Physics of Fluids, 31, 075106. https://doi.org/10.1063/1.5108856 (Editor's Pick)

Qin, J.; Zhang, H.; Wang, B.*; 2018. Numerical evaluation of acoustic characteristics and their damping of a thrust chamber using a constant-volume bomb model, Chinese Journal of Aeronautics, 31, 470–480. https://doi.org/10.1016/j.cja.2018.01.007

Qian, C.; Bing, W.*; Huiqiang, Z.; Yunlong, Z.; Wei, G.; 2016. Numerical investigation of H2/air combustion instability driven by large scale vortex in supersonic mixing layers, International Journal of Hydrogen Energy, 41, 3171–3184. https://doi.org/10.1016/j.ijhydene.2015.11.029

E.Other

Jin, X.; Cheng, X.; Wang, Q.; Wang, B.*; 2023. Numerical Analysis of Rarefied Hypersonic Flows over Inclined Cavities, International Journal of Heat and Mass Transfer, 214. https://doi.org/10.1016/j.ijheatmasstransfer.2023.124401

Jin, X.*; Wang, B.; 2023. Numerical investigation of the effects of axial temperature gradient and cooling rate on InGaSb crystal growth under microgravity, Journal of Crystal Growth, 607. https://doi.org/10.1016/j.jcrysgro.2023.127110

Liu, Y.; Zhang, Q.*; Zhang, H.; Wang, B.; 2022. Numerical investigation on the performance of internal flow and atomization in the recessed gas-centered swirl coaxial injectors, Aerospace Science and Technology, 129. https://doi.org/10.1016/j.ast.2022.107858

Cai, T.; Backer, S.M.; Cao, F.; Wang, B.; Tang, A.; Fu, J.; Han, L.; Sun, Y.; Zhao, D.*; 2021. NOx emission performance assessment on a perforated plate-implemented premixed ammonia-oxygen micro-combustion system, Chemical Engineering Journal, 417, 128033. https://doi.org/10.1016/j.cej.2020.128033

Cai, T.; Zhao, D.*; Sun, Y.; Ni, S.; Li, W.; Guan, D.; Wang, B.; 2021. Evaluation of NOx emissions characteristics in a CO2-Free micro-power system by implementing a perforated plate, Renewable and Sustainable Energy Reviews, 145, 111150. https://doi.org/10.1016/j.rser.2021.111150

Chen, Z.; Huang, F.; Jin, X.*; Cheng, X.; Wang, B.; 2021. A novel lightweight aerodynamic design for the wings of hypersonic vehicles cruising in the upper atmosphere, Aerospace Science and Technology, 109, 106418. https://doi.org/10.1016/j.ast.2020.106418

Jin, X.; Huang, F.; Miao, W.; Cheng, X.; Wang, B.; 2021. Effects of the boundary-layer thickness at the cavity entrance on rarefied hypersonic flows over a rectangular cavity, Physics of Fluids, 33, 036116. https://doi.org/10.1063/5.0045056

Jin, X.*; Wang, B.; Cheng, X.; Wang, Q.; Huang, F.; 2021. Effects of corner rounding on aerothermodynamic properties in rarefied hypersonic flows over an open cavity, Aerospace Science and Technology, 110, 106498. https://doi.org/10.1016/j.ast.2021.106498

Um, K.; Hu, X.; Wang, B.; Thuerey, N.; 2021. Spot the Difference: Accuracy of numerical simulations via the human visual system, ACM Transactions on Applied Perception, 18(2), 6:1-6:15. https://doi.org/10.1145/3449064

Sun, Y.; Cai, T.; Shahsavari, M.; Sun, D.; Sun, X.; Zhao, D.*; Wang, B.; 2021. RANS simulations on combustion and emission characteristics of a premixed NH3/H2 swirling flame with reduced chemical kinetic model, Chinese Journal of Aeronautics, 34(12), 17-27. https://doi.org/10.1016/j.cja.2020.11.017

Cai, T.; Zhao, D.*; Wang, B.; Li, J.; Guan, Y.; 2020. NOx emission and thermal performances studies on premixed ammonia-oxygen combustion in a CO2-free micro-planar combustor, Fuel, 280, 118554. https://doi.org/10.1016/j.fuel.2020.118554

Jin, X.*; Wang, B.; Cheng, X.; Wang, Q.; Huang, F.; 2020. The effects of Maxwellian accommodation coefficient and free-stream Knudsen number on rarefied hypersonic cavity flows, Aerospace Science and Technology, 97, 105577. https://doi.org/10.1016/j.ast.2019.105577

Jin, X.; Huang, F.; Cheng, X.; Wang, Q.; Wang, B.*; 2019. Monte Carlo simulation for aerodynamic coefficients of satellites in low-earth orbit, Acta Astronautica, 160, 222–229. https://doi.org/10.1016/j.actaastro.2019.04.012

Rao, Z.; Luo, Y.; Wang, B.*; Xie, Q.; He, W.; 2019. Mitigation of H2/air gaseous detonation via utilization of PAN-based carbon fiber felt, International Journal of Hydrogen Energy, 44, 5054–5062. https://doi.org/10.1016/j.ijhydene.2018.12.196

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