王兵，副教授，博士生导师，工学博士，1977年2月生于河北唐山。2005年起在清华大学航天航空学院承担教学科研工作至今，历任讲师、副教授；2009年5月起负责学院学生工作，曾任航院党委研究生工作组组长，现任航院党委副书记。
联系方式：https://www.labxing.com/scpthu
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Email：wbing@tsinghua.edu.cn
教育背景1996年9月由河北省唐山市第一中学考入清华大学工程力学系工程热物理专业学习，2000年7月获工学学士学位，历任热六班班长、力学系学生会副主席；
2000年9月保送直接攻读清华大学工程力学系工程热物理专业硕博连读研究生，研究方向为湍流燃烧与两相流体动力学，2005年1月毕业并获工学硕士、博士学位，历任研究生班党支部书记，清华大学研究生会副主席，清华大学研究生团委副书记，清华大学博士生报告团团长等。

工作履历2005年3月进入清华大学航天航空学院工程力学系流体力学研究所工作；2008年4 月进入清华大学航天航空学院航空宇航工程系动力与推进技术研究所，2010年12月晋升为副教授，2012年6月被授予博士生导师资格，招收航空宇航科学与技术、流体力学博士究生。
2006年10月，获得德国洪堡（Alexander von Humboldt）奖学金，赴德国慕尼黑工业大学访问研究，2008年4月回校继续任教；后多次赴德国慕尼黑工业大学、德国亚琛工业大学、波兰理工大学等研究机构进行短期学术交流。
教学情况：
2014年获清华大学青年教师教学基本功大赛理工组一等奖，2015年获北京市青年教师教学基本功大赛理工组三等奖.
承担教学课程如下：
航空宇航推进的数值方法 48学时
航空宇航推进理论 64学时
液体火箭发动机 32学时
高超声速推进理论（航空宇航推进技术） 32学时
推进中的两相流体动力学 32学时
航空宇航基础实验（合讲）32学时
多次开设SRT（本科生研究训练），正在进行和结题项目有“连续旋转爆震发动机”、“空天组合发动机新概念”、“好奇号火星探测任务分析”、“液滴微重力燃烧”、 “垂直起降发动机喷管流场数值仿真”、 “液滴的复杂碰撞行为”等，培养本科生20余名。

学术兼职担任the 11th International Symposium on Hazards, Prevention, and Mitigation of Industrial Explosion组委会副主席。
国家节能中心专家（2010年起）、教育部留学基金委评审专家（2012年起）、国家自然科学基金评审专家、浙江省自然科学基金评审专家、河北省自然科学基金评审专家、黑龙江省自然科学基金评审专家、黑龙江科技奖、河北科技奖评审专家。
《Journal of Engineering》期刊编委，《Chinese Journal of Aeronautics》期刊青年编委，《火箭推进》、《兵器工程学报》期刊编委，《航空学报》期刊编委。
担任《International Journal of Heat and Mass Transfer》、《Numerical Heat Transfer》、《Experimental Heat and Fluids》、《Physics of Fluids》、《Applied Physics Letter》、《Shock Wave》、《ASME-Journal of Fluid Engineering》、《Journal of Aerospace Engineering》、等多个著名国际期刊和《推进技术》、《力学进展》、《航空学报》、《航空动力学报》等国内重要期刊审稿人。

研究概况清华大学航天航空学院航空宇航工程系喷雾燃烧与推进实验室负责人，主要研究概况如下：
航空宇航推进领域的前沿基础科学问题，包括先进发动机极端条件下的点火及湍流两相燃烧过程机理、规律与控制机制（国家自然科学基金、国家重大工程项目等资助）；
燃烧不稳定性，包括液体火箭发动机高压燃烧不稳定性、超燃冲压发动机超音速燃烧不稳定性、固体火箭发动机燃烧本质不稳定性、航空燃气涡轮发动机贫燃预混燃烧不稳定性、旋转爆震发动机爆震燃烧不稳定性等（国家自然科学基金、国家重大工程项目等资助）；
航空宇航推进中的先进数值模拟方法及其工程应用，包括大涡模拟，直接模拟，现代数值格式，混合LES/RANS模拟，高性能计算等（科技部重点研发计划、国家重大工程项目等资助）；
新概念推进及组合发动机总体与数字化集成设计，包括组合循环推进系统性能与关键技术、液体火箭发动机系统与集成设计、固体火箭发动机数字化设计等（工程单位课题资助）；
能源与环境基础科学问题，包括环境力学中颗粒污染物弥散与控制、空化初生与气泡溃灭及其多物理作用机理与控制等（国家自然科学基金资助）。
本实验室招收致力于从事“中国心”（包括“航天心”和“航空心”）的研究生，开展下一代航空发动机、火箭发动机、超燃冲压发动机、新概念组合推进与空天动力等相关研究工作。热烈欢迎清华本校、国内知名985和211等兄弟院校、国外知名大学的优秀学生加盟本实验室。实验室将为研究生（包括博士生、工学硕士、工程硕士）提供广阔的研究平台，充足的生活补助，赴国外著名大学（包括美国、德国、日本等）交流研究的机会和精彩的研究生生活。本实验室长期招聘博士后。
实验室已毕业研究生目前主要去向有：西北工业大学、中山大学等，中国航天一院、三院、五院、六院、八院等京沪地区航天核心单位，航空主机所，中国兵器集团核心研究所，国家电网以及五大发电集团核心研究部门等央企核心部门，国外著名大学与科研机构研究人员或博士后，世界五百强外资企业在京沪地区重要研发部门（包括通用电气、斯伦贝谢、爱立信等）。
拟招生人数：博士生1-2人/年，硕士生1-2人/年，博士后工作人员名额不限。欢迎有力学、能源动力、航天航空、船舶与海洋等相关工科背景的同学加入本实验室。

奖励与荣誉北京市教学成果奖一等奖(2018，排名第六)；
清华大学教学成果奖一等奖(2017，排名第四)；
清华大学“廖凯原”奖教金(2015)；
清华大学“泰豪”奖教金(2015)；
清华大学优秀共产党员(2015，2003)；
北京高校优秀德育工作者(2014)；
清华大学教学成果二等奖(2014，排名第一，2012，排名第二)；
北京高校“英才计划”（2013）；
清华大学林枫辅导员奖(2011)；
清华大学就业先进集体奖(2011)、个人奖(2012)；
清华大学百年校庆工作“先进个人”(2011)；
工程热物理学会优秀青年论文奖(2010)；
“清华大学优秀班（级）主任工作优秀奖”一等奖(2009)；
北京市优秀学生干部(2004)；
清华大学一二九辅导员奖(2004) ；
北京市三好学生(2003)；
清华大学特等奖学金(2003)；
清华大学十优秀研究生 (2003)；
清华大学优良毕业生(2000)。

学术成果主要学术贡献及领域影响包括：
（1）“探月工程”落月变推力发动机关键技术攻关及成果应用。
（2）姿控发动机点火基础理论及成功应用。
（3）卫星通用第二代发动机推力室关键技术及成功应用。
（4）液体火箭发动机燃烧不稳定性机理及评估方法。
（5）涡轴发动机高速旋转轴端动密封（两相介质密封）理论与设计软件。
作为项目负责人先后主持国家自然科学基金、国家重点研发计划、“两机工程”、国家重大科技工程、原国家973、863等航天航空类、力学与能源类重大课题20余项、作为主要骨干参与国家自然科学基金重点项目、国家重大课题10余项。作为主要完成人编著《航空宇航推进理论》、《空气动力学》等教材；在专业领域内国际权威杂志《Journal of Fluid Mechanics》、《Proceedings of Combustion Institute》、《Progress of Aerospace Sciences》、《International Journal of Heat and Mass Transfer》、《Energy》、《International Journal of Multiphase Flow》、《Physics of Fluids》、《Journal of Computational Physics》、《AIAA-Journal of Power and Propulsion》、《Shock Wave》《Numerical Heat Transfer》、《International Journal of Numerical Methods in Fluids》等发表多篇论文。目前已发表论文150余篇，其中SCI收录50余篇，EI收录60余篇。
代表性论文
[1].Ren Z., Wang B.*, Xiang G., Zheng L., 2018, "Numerical analysis of wedge-induced oblique detonations in two-phase kerosene-air mixtures," Proceedings of the Combustion Institute, https://doi.org/10.1016/j.proci.2018.08.038
[2].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, https://doi.org/ 10.1063/1.**
[3].Xie Q., Wang B. *, Wen H., He W., Wolanski P., 2018, " Enhancement of continuously rotating detonation in hydrogen and oxygen-enriched air," Proceedings of the Combustion Institute, Vol.37, https://doi.org/10.1016/j.proci.2018.08.046
[4].Xie Q., Wang B. *, Wen H., He W., 2018, "Thermoacoustic Instabilities in an Annular Rotating Detonation Combustor Under Off-design Condition," Journal of Propulsion and Power, https://doi.org/10.2514/1.B37044
[5].Wu W., Xiang G. L., Wang B. *, 2018, “On high-speed impingement of cylindrical droplets upon solid wall considering cavitation effects,” Journal of Fluid Mechanics, https://doi.org/10.1017/jfm.2018.753
[6].He W., Xie Q., Ji Z., Rao Z., Wang B. *, 2018, “Characterizing continuously rotating detonation via nonlinear time series analysis,” Proceedings of the Combustion Institute, https://doi.org/10.1016/j.proci.2018.07.045
[7].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, Vol. 31(9): 1870-1879.
[8].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, Vol. 78: 427-437.
[9].Gaoming Xiang, and Bing Wang* , 2018, “Numerical investigation on the interaction of planar shock wave with an initial ellipsoidal bubble in liquid medium,” AIP Advances 8, 075128.
[10].Zhang W.*, Zou L., Zheng X., Wang B., 2018, “Numerical study on the interaction of a weak shock wave with an elliptic gas cylinder,” Shock Wave, https://doi.org/10.1007/s00193-018-0828-y
[11]. Ren Z. X., Wang B.*, Xiang G. M., and Zheng L. X., 2018, “Effects of the multiphase composition in a premixed fuel-air stream on wedge-induced oblique detonation stabilization,” Journal of Fluid Mechanics, Vol. 846: 411-427.
[12].Zhang F. Zhang H Q*, Wang B. 2018, “Conceptual study of a dual-rocket-based-combined-cycle powered two-stage-to-orbit launch vehicle,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 232(5): 944-957
[13]. Zheng D. F, and Wang B.*, 2018, “Utilization of nonthermal plasma in pulse detonation engine ignition,” Journal of Propulsion and Power, Vol. 34(2), pp. 539-549.
[14]. Liu N.*, Wang Z. G., Sun M. B., Wang H. B., and Wang B., 2018, “Numerical simulation of liquid droplet breakup in supersonic flows,” Acta Astronautica, Vol. 145, 115-120.
[15]. Wang B., Xiang G. M., and Hu X. Y*., 2018, “An incremental-stencil WENO reconstruction for simulation of compressible two-phase flows,” International Journal of Multiphase Flow, Vol. 104, pp.20-31.
[16]. Zhao D*., Lu Z. L., Zhao H., Li X. Y., and Wang B., Liu P. J., 2018, “A review of active control approaches in stabillizing combustion systems in aerospace industry,” Progress of Aerospace Sciences, Vol. 97, pp. 35-60.
[17]. Xie Q. F., Wen H. C., Li W. H., Ji Z. F., and Wang B.*, 2018, “Analysis of operating diagram for H2/air rotating detonation combustors under lean fuel condition,” Energy, Vol. 151, pp. 408-419.
[18]. Herty M., Mueller S., Gerhard N., Xiang G. M., and Wang B., 2018, “Fluid-structure coupling of linear elastic model with compressible flow models,” International Journal for Numerical Methods in Fluids, Vol. 86(6), pp. 365-391.
[19]. Qin J. X., Zhang H. Q., and 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, Vol. 21(3), pp. 470-480.
[20]. Ren Z. X., Wang B.*, and Zheng L. X., 2018, “Numerical analysis on interactions of vortex, shock wave, and exothermal reaction in a supersonic planar shear layer laden with droplets,” Physics of Fluids, Vol. 30, 036101
[21]. Xiang G. M. and Wang B.*, 2017, “Numerical study of a planar shock interacting with a cylindrical water column embedded with an air cavity,” Journal of Fluid Mechanics, Vol.825, pp. 825-852.
[22]. Zhang P. Y. and Wang B.*, 2017, “Effects of elevated ambient pressure on the disintegration of impinged sheets,” Physics of Fluids, Vol. 29, 042102.
[23]. Ren Z. X., Wang B.*, Yang S. R., Xie Q. F., Liu H. X. and Wang D. L., 2017, “Evolution of flame kernel in one eddy turnover of high-speed droplet laden shear layers,” Journal of Loss Prevention in the Process Industries, Vol. 49, pp.938-949
[24]. Wang B.*, Rao Z. M., and Xie Q. F. et al., 2017, “Brief review on passive and active methods for explosion and detonation suppression in tubes and galleries,” Journal of Loss Prevention in the Process Industries, Vol. 49, pp. 280-290.
[25]. Ren Z. X., Wang B.., Xie Q. F. and Wang D. L., 2017, “Thermal auto-ignition in high-speed droplet-laden mixing layers,” Fuel, Vol. 191(1), pp. 176–189.
[26]. Xie Q. F., Wen H. C., Liu H. X., and Wang B*. et al, 2017, “Effects of Silicone Rubber and Aerogel Blanket Walled Tubes on H2/Air Gaseous Detonation,” Journal of Loss Prevention in the Process Industries, Vol. 49, pp. 753-761.
[27]. Wang B*., Wei. W., Ma S. N., and Gao W*., 2016, “Construction of one-step H2/O2 reaction mechanism for predicting ignition and its application in simulation of supersonic combustion,” International Journal of Hydrogen Energy, Vol. 41(42), pp.19191-19206.
[28]. Chen Q., Wang B*., Zhang H. Q., Zhang Y. L., and Gao W., 2016, “Numerical investigation of H2/air combustion instability driven by large scale vortex in supersonic mixing layers,” International Journal of Hydrogen Energy, Vol. 41, pp. 3171-3184.
[29]. Hu B. W., Wang B*., and Tian X. T., 2016, “Numerical modeling and studies of ignition transients in end-burning grain solid rocket motors,” Journal of Propulsion and Power, Vol. 32, pp. 1333-1342.
[30]. Hu X.Y.*, Wang B., and Adams N.A., 2015, “An efficient low-dissipation hybrid weighted essentially non-oscillatory scheme,” Journal of Computational Physics, Vol. 301, pp. 415-424.
[31]. Wang B*., Wei. W., Zhang Y. L., Zhang H. Q., and Xue S. Y., 2015, “Passive scalar mixing in Mc<1 planar shear layer flows,” Computers and Fluids, Vol. 123, pp. 32-43.
[32]. He S. D., and Wang B*., 2015, “Dispersion of particles in wall-bounded particle-laden turbulent flows with high wall permeability,” International Journal of Multiphase Flow, Vol. 77, pp.104-119.
[33]. Zhang Y. L., Wang B*., and Zhang H. Q., 2014, “Ignition, flame propagation and extinction in the supersonic mixing layer flow,” Science China- Technological Sciences, Vol. 57(11), pp. 2256-2264.
[34]. Wang B., Zhang H. Q*., and Cao H. J., 2013, “Flow dynamics of a spiral-groove dry-gas seal,” Chinese Journal of Mechanical Engineering, Vol. 26(1), pp. 78-84.
[35]. Zhang H. Q., Ga Y. J., Wang B*., and Wang X. L., 2012, “Analysis of combustion instability via constant volume combustion in a LOX/RP-1 bipropellant liquid rocket engine,” Science in China - Series E: Technological Sciences, Vol. 55(4), pp. 1066-1077.
[36]. Wang B*., and Manhart M., 2012, “Two-phase micro- and macro-time scales in particle-laden turbulent channel flows,” Acta Mechanica Sinica, Vol. 28(3), pp. 595-604.
[37]. Zhang H. Q., Liu M., Wang B*., and Wang X. L., 2012, “Dense gas-particle flow in vertical channel by multi-lattice trajectory model,” Science China Technological Sciences, Vol. 55(2), pp. 542-554.
[38]. Wang B*., and Zhang H. Q., 2011, “Numerical analysis of a spiral-groove dry-gas seal considering micro-scale effects,” Chinese Journal of Mechanical Engineering, 24(1), pp 146-153.
[39]. Wang B*., Zhang H. Q., Manhart M., and Chan C. K., 2011, “A numerical study on statistical temporal scales in inertia particle dispersion,” Journal of Computational and Applied Mathematics, Vol. 235(13), pp. 3807-3816.
[40]. Zhang H. Q., Rong Y., Wang B*., and Wang X. L., 2011, “Large eddy simulation of a 3-D spatially developing turbulent round jet,” Science China Technological Sciences, Vol. 54(11), pp. 2916-2923.
[41]. Wang B.*, 2010, “Inter-phase interaction in a turbulent, vertical channel flow laden with heavy particles Part I: Numerical methods and particle dispersion properties,” International Journal of Heat and Mass Transfer, Vol. 53(11-12), pp. 2506-2521.
[42]. Wang B. *, 2010, “Inter-phase interaction in a turbulent, vertical channel flow laden with heavy particles Part II: Two-phase velocity statistical properties,” International Journal of Heat and Mass Transfer, Vol. 53(11-12), pp. 2522-2529.
[43]. Wang B. *, Manhart M.,and Zhang H. Q., 2010, “A study on turbulence modulation via an analysis of turbulence anisotropy-invariants,” Science China-Physics Mechanics & Astronomy, Vol. 53(3), pp. 508-513.
[44]. Wang B. *, Zhang H. Q., and Wang X. L., 2010, “Large-eddy simulation of near-field dynamics in a particle-laden round turbulent jet,” Chinese Journal of Aeronautics, Vol. 23(2), pp. 162-169.
[45]. Wang B. *, Zhang H. Q., and Wang X. L., 2009, “A Time-series stochastic separated flow (TSSSF) model for turbulent two-phase flows,” Numerical Heat Transfer Part B-Fundamentals, Vol. 55(1), pp. 73-90.
[46]. Wang B. *, Zhang H. Q., Liu Y, Yan X. F., and Wang X. L., 2009, “Particle modulations to turbulence in two-phase round jets,” Acta Mechanica Sinica, Vol. 25(5), pp. 611-617.
[47]. Zhang H. Q., Wang B., Chan C. K.*, and Wang X. L., 2008, “Large Eddy Simulation of a dilute particle-laden turbulent flow over a backward-facing step,” Science in China Series E-Technological Sciences, Vol. 51(11), pp. 1957-1970.
[48]. Du T., Wu Z. N.*, and Wang B., 2006, “On steady state computation of turbulent flows using k-epsilon models approximated by the time splitting method,” International Journal for Numerical Methods in Fluids, Vol. 51(1), pp. 77-115.
[49]. Wang B. *, Zhang H. Q., and Wang X. L., 2006, “Large eddy simulation of particle response to turbulence along its trajectory in a backward-facing step turbulent flow,” International Journal of Heat and Mass Transfer, Vol. 49(1-2), pp. 415-420.
[50]. Cui J. L., Zhang H. Q.*, Wang B., Rong Y., and Wang X. L., 2005, “Flow visualization and laser measurement on particle modulation to gas-phase turbulence,” Journal of Visualization, Vol. 9(3), pp. 339-345.
国内外会议邀请报告
[1].Wang B. , “Recent numerical studies on two-phase reacting flows ,” Invited talk, International Seminar on the Dynamics of Explosions and Reactive Flow, Sept. 21st, 2018, Beijing, China.
[2].Wang B., “Recent study on rotating detoantion in Tsinghua Univesity,” Invited talk, 9th Internaitonal Workshop on Detonation Proplusion, Sept. 9-13, 2018, Xi’an, China.
[3]. Wang B., “An overview of numerical studies on two-phase flow problems,”Invited talk, International Workhsop on Computational Methods in Compressible Complex Flow, Sept. 1st, 2018, Xi’an, China.
[4]. Wang B., “Combution instatiblities in engines applied in aerospace propulsion system,” Plenary talk, 4th National Young Scholar Meeting on Combustion of China, Mar. 30-31, 2018, Changsha, China.（第四届全国青年燃烧会，大会报告）
[5]. Wang B., “Recent research on rotating detonation in Tsinghua University,” Invited speaker, 2017 International Workshop on Detonation for Propulsion, Dec. 6-8, 2017, Poitiers, France.
[6]. Wang B., “Stabilities of rotating detonation,” Plenary talk, 5th National Conference of Detonation and New-Types of Propulsion of China. Nov. 14-17, 2017, Changsha, China.（第五届全国爆震与新型推进大会，大会报告）
[7]. Wang B., “Rotating detonation Engines,” Invited speaker, 1st National Conference of Ordnance Science and Technology of China, Oct. 20-22, 2017, Chongqing, China.（第一届全国兵器科学与技术大会，主题报告）
[8]. Wang B., “From combustion instabilities and continuously rotating detonation,” Invited speaker, 3th National Young Scholar Meeting on Combustion of China, Apr. 14-17, 2017, Xian, China. （第三届全国青年燃烧会，邀请报告）
[9]. Wang B., “Combustion Modes in Rotating Detonation Combustor of H2-Air,” Plenary talk, XXIII International Symposium on Combustion Processes, 2017, Ryan, Poland.
[10]. Wang B., “Experimental study on instabilities of rotating detonation combustion,” Invited speaker, International Constant Volume and Detonation Combustion Workshop, 2017, 13-16 Jun, Poitiers, France.
[11]. Wang B., “Direct numerical simulation of impinging jets atomization,” 1st International Symposium on Combustion Instabilities, Jan. 5-9, 2017, Beijing, China.
[9]. Wang B., “Instabilities of reacting flows,” Session Keynote, 8th International Symposium on Multiphase Flows, Heat Mass Transfer and Energy Conversion. Dec. 16-19, 2016, Chengdu
[12]. Wang B., “Instabilities of rotational detonation,” Session Keynote. 1st International Conference in Aerospace for Yong Scientists, Nov. 11-13, 2016, Beijing.
[13]. Wang B., “Gas-liquid two-phase interfacial mechanics in cavitation flows,” Session Keynote talk, 2nd International Symposium of Cavitation and Multiphase Flow ISCM, Oct. 21-25 2016, Zhenjiang, China.
[14]. Wang B., “Auto-ignition/extinction and combustion modes in shear reactive flows,” Session Keynote talk, 10th International Symposium on Safety Science and Technology, Oct.17-19,2016, Kunming, China.
[15]. Wang B., “LES of compressible reacting flows,” Keynote speaker, 2nd Annual International conference on Material Engineering and Mechanical Engineering, Oct. 14-16, 2016, Wuhan, China.
[16]. Wang B., “Numerical analysis of combustion instabilities in different engines,” Keynote talk, International Conference on Power and Energy Engineering, Sept. 29-30, 2016, London, UK.
[17]. Wang B., “Stabilities of rotation detonation engines,” Invited lecture, 2016 International Symposium on Innovation and Prospect of Liquid Propulsion Technology, Sept. 4-6, 2016, Xi’an, China.
[18]. Wang B., “Stability and instability in combustors of propulsion devices,” Invited keynote speaker in 2nd International Forum on Specialized Equipment and Engineering Mechanics, Jul. 26-30, 2016, Nanjing, China.
[19]. Wang B., “Stabilities of rotation detonation engine,” Invited speaker, 2016 International Workshop on Detonation for Propulsion, Jul. 12-15, 2016, Singapore.