北京航空航天大學(xué)

導(dǎo)師詳細(xì)信息

姓名：單鵬

性別：男

出生年份：1955

職稱：教授

院系：能源與動力工程學(xué)院

首次聘任導(dǎo)師時間：2004

現(xiàn)聘任導(dǎo)師一級學(xué)科名稱：航空宇航科學(xué)與技術(shù)

現(xiàn)聘任導(dǎo)師二級學(xué)科名稱：航空宇航推進理論與工程

聘任在第二學(xué)科培養(yǎng)博士生專業(yè)名稱：無

聘任在自主設(shè)置學(xué)科培養(yǎng)博士生專業(yè)名稱：無

主要研究方向及特色：葉輪機氣體動力學(xué)航空發(fā)動機氣動熱力學(xué)（渦輪,沖壓,螺槳）計算流體力學(xué)

電子信箱：PShan@buaa.edu.cn

辦公電話：82316372

辦公地點：北航教學(xué)區(qū)北配樓

通信地址：北京航空航天大學(xué)407教研室

個人簡介：

單鵬，男，北京航空航天大學(xué)能源與動力工程學(xué)院教授，博士生導(dǎo)師。1955年10月生。78-82年獲北航發(fā)動機系固體火箭及固體沖壓組合發(fā)動機專業(yè)學(xué)士學(xué)位。89年獲北航航空發(fā)動機專業(yè)碩士學(xué)位。97年春獲北航航空發(fā)動機專業(yè)博士學(xué)位。82年以來在渦輪式、沖壓式和活塞螺旋槳式發(fā)動機總體性能，軸流式、離心式和斜流式壓氣機氣動設(shè)計與實驗，計算流體力學(xué)方法等方面進行教學(xué)與研究。93年以來主攻高負(fù)荷掠形風(fēng)扇設(shè)計、實驗及其激波結(jié)構(gòu)機理等的研究。是高負(fù)荷單級后掠風(fēng)扇ATS-2的主要設(shè)計和試驗者之一。2000年參加北航某國防重點工程的設(shè)計，任推進系統(tǒng)負(fù)責(zé)人，2007年又在該工程二期研究中負(fù)責(zé)推進系統(tǒng)總體設(shè)計。2001年赴德國亞琛大學(xué)進行多孔性金屬材料傳熱問題的短期合作研究。在國際重要刊物美國機械工程師協(xié)會（ASME）葉輪機雜志（Journal of Turbomachinery），國際重要系列會議ASME國際燃?xì)廨啓C學(xué)會年會（ASMEIGTITURBOEXPO），和國內(nèi)多種核心刊物上發(fā)表氣體動力學(xué)論文40余篇。特別在高負(fù)荷壓氣機激波系結(jié)構(gòu)方面，在ASME國際燃?xì)廨啓C學(xué)會發(fā)表了系列論文。2000年以來將現(xiàn)代高負(fù)荷壓氣機設(shè)計技術(shù)用于飛機和導(dǎo)彈用渦輪發(fā)動機的設(shè)計和改型設(shè)計研究，開展了微型渦輪發(fā)動機領(lǐng)域的研究與設(shè)計，在國家自然科學(xué)基金資助下也持續(xù)開展了超聲速燃燒沖壓發(fā)動機的總體設(shè)計與關(guān)鍵技術(shù)實驗研究。主講基礎(chǔ)課程多維氣體動力學(xué)，氣體動力學(xué)基礎(chǔ)，航空發(fā)動機概論，航空概論。建立課程實驗課“葉輪機設(shè)計與制作”。出版高等學(xué)校通用教材《多維氣體動力學(xué)基礎(chǔ)》（單鵬編著）,《氣體動力學(xué)基礎(chǔ)(2011年修訂版)》（潘錦珊，單鵬主編，共六人）。89年獲航空工業(yè)部科技進步三等獎（姜籍成等六人）。92年領(lǐng)銜獲北航優(yōu)秀教學(xué)成果二等獎（單鵬等兩人）。98年個人獲美國聯(lián)合技術(shù)公司UTC在中國設(shè)立的“容閎科技教育獎”（該獎項為在中國科教領(lǐng)域作出突出貢獻的青年學(xué)者而設(shè)）。2004年領(lǐng)銜獲北京市高等教育優(yōu)秀教學(xué)成果二等獎和北航優(yōu)秀教學(xué)成果一等獎（單鵬等五人）。2006年《多維氣體動力學(xué)基礎(chǔ)》被評為北京高等教育精品教材，2008年微型單葉輪渦輪風(fēng)扇發(fā)動機獲第六屆中國國際發(fā)明展覽會銀獎（單鵬等四人）。

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.