北航能源与动力工程学院航空宇航推进理论与工程导师介绍：单鹏

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导师详细信息

姓名：单鹏

性别：男

出生年份：1955

职称：教授

院系：能源与动力工程学院

首次聘任导师时间：2004

现聘任导师一级学科名称：航空宇航科学与技术

现聘任导师二级学科名称：航空宇航推进理论与工程

聘任在第二学科培养博士生专业名称：无

聘任在自主设置学科培养博士生专业名称：无

主要研究方向及特色：叶轮机气体动力学航空发动机气动热力学（涡轮,冲压,螺桨）计算流体力学

电子信箱：PShan@buaa.edu.cn

办公电话：82316372

办公地点：北航教学区北配楼

通信地址：北京航空航天大学407教研室

个人简介：

单鹏，男，北京航空航天大学能源与动力工程学院教授，博士生导师。1955年10月生。78-82年获北航发动机系固体火箭及固体冲压组合发动机专业学士学位。89年获北航航空发动机专业硕士学位。97年春获北航航空发动机专业博士学位。82年以来在涡轮式、冲压式和活塞螺旋桨式发动机总体性能，轴流式、离心式和斜流式压气机气动设计与实验，计算流体力学方法等方面进行教学与研究。93年以来主攻高负荷掠形风扇设计、实验及其激波结构机理等的研究。是高负荷单级后掠风扇ATS-2的主要设计和试验者之一。2000年参加北航某国防重点工程的设计，任推进系统负责人，2007年又在该工程二期研究中负责推进系统总体设计。2001年赴德国亚琛大学进行多孔性金属材料传热问题的短期合作研究。在国际重要刊物美国机械工程师协会（ASME）叶轮机杂志（Journal of Turbomachinery），国际重要系列会议ASME国际燃气轮机学会年会（ASMEIGTITURBOEXPO），和国内多种核心刊物上发表气体动力学论文40余篇。特别在高负荷压气机激波系结构方面，在ASME国际燃气轮机学会发表了系列论文。2000年以来将现代高负荷压气机设计技术用于飞机和导弹用涡轮发动机的设计和改型设计研究，开展了微型涡轮发动机领域的研究与设计，在国家自然科学基金资助下也持续开展了超声速燃烧冲压发动机的总体设计与关键技术实验研究。主讲基础课程多维气体动力学，气体动力学基础，航空发动机概论，航空概论。建立课程实验课“叶轮机设计与制作”。出版高等学校通用教材《多维气体动力学基础》（单鹏编著）,《气体动力学基础(2011年修订版)》（潘锦珊，单鹏主编，共六人）。89年获航空工业部科技进步三等奖（姜籍成等六人）。92年领衔获北航优秀教学成果二等奖（单鹏等两人）。98年个人获美国联合技术公司UTC在中国设立的“容闳科技教育奖”（该奖项为在中国科教领域作出突出贡献的青年学者而设）。2004年领衔获北京市高等教育优秀教学成果二等奖和北航优秀教学成果一等奖（单鹏等五人）。2006年《多维气体动力学基础》被评为北京高等教育精品教材，2008年微型单叶轮涡轮风扇发动机获第六届中国国际发明展览会银奖（单鹏等四人）。

Peng Shan, Male, professor of the School of Jet Propulsion (SJP), Beijing University of Aeronautics and Astronautics (BUAA). Born on Oct. 9, 1955. Enrolled discipline of solid propellant rocket engine and ramjet engine, SJP, BUAA at 1978, acquired Bachelor of Science degree at 1982. Acquired Master of Science degree in discipline of Air-breathing Engine, SJP, BUAA at 1989. Acquired Ph. D. degree in discipline of Air-breathing Engine, SJP, BUAA at spring, 1997. Since 1982, teaches and researches primarily among the fields of Computational Fluid Dynamics, engine total performance design and simulation including aviation turbine engine, ramjet engine and reciprocating engine, and compressor and turbine aerodynamic design and experiment study including axial-flow, radial-flow and mixed-flow types. After 1993, mainly engages in aviation high-loading swept-compressor and fan design and experiment research, especially in the research of shock system structure within high-loading compressor and fan cascades. Is one of the main designer and researcher of BUAA’s single-stage high loading backward-swept investigation fan ATS-2. In 2000 was sent to a national funding engineering project, served as the principal of the propulsion system. In 2007, was responsible again for the overall design of the propulsion system updating research and engineering in the second phase of the same project. At 2001, as a visiting scientist at Aachen University, Germany, researched the porous metal heat transfer issue, named “Thermally highly loaded, porous and cooled multi-layer systems for combined cycle power plants”. Published more than 40 scientific and engineering articles in aerothermodynamics and engines among the transactions of the ASME, Journal of Turbomachinery, the transactions of the ASME, ASME IGTI TURBO EXPO paper, and various China’s domestic journals. Especially, in the field of high-loading compressor shock system structure, published a series of research papers. After 2000, applied the high-loading compressor design technology to airplane and missile turbojet and turbofan engine design and updating engineering, meanwhile processed the research and design activities in micro-turbojet and turbofan engines, while engaged in also the investigation on the overall design and the supersonic combustion technology experiment of the supersonic combustion ramjet engine. The university teachings are mainly including course “Three-dimensional gas dynamics” for aerodynamic field SJP undergraduate students, course “Fundamentals of gas dynamics” for all SJP undergraduate students, course “Introduction to aviation engine”. Compiled the university text books “Fundamentals of three-dimensional gas dynamics”(Peng Shan) and “Fundamentals of gasdynamics (Fourth edition)”(Jin-shan Pan, Peng Shan etc.). Established the experimental course “Design and Fabrication of Turbomachines” as an elective course for all university undergraduate and graduate students. In 1989, project "Library Inner-transport System" was granted the third rank award of Science & Technology Progress by the Aviation Industry Ministry of People's Republic of China, Shan is one of the six designers. In 1992, project "Teaching Software for the Course of CNC Machine Practice" was granted the second rank award of Excellent Teaching Progress by BUAA, Shan is the first performer of the project. In 1998, United Technologies (UTC, The United States of America) awarded a "Rong Hong Endowment" to Peng Shan for his Excellence in Chinese science & technology education, the award is established by UTC to commend China's young scholars. In 2004, project " Design and Fabrication of Turbomachines" was granted the second rank award of Excellent Teaching Progress by Beijing City University Education Committee, and was granted the first rank award of Excellent Teaching Progress by BUAA, Shan is the first performer of the project. In 2007, Shan’s text book “Fundamentals of three-dimensional gas dynamics” was evaluated as “Elaborate Books of Higher Education of Beijing City”. In 2008, the invention " Micro-Turbofan Engine Using Single Blisk of Fan & Compressor Rotor " was granted the silver award of the 6th China International Exhibition of Inventions, Shan is the first inventor of the four.