基本情况
1987年7月本科毕业于北京航空学院发动机系固体火箭发动机专业，获学士学位；1990年3月研究生毕业于北京航空航天大学动力系固体火箭发动机专业，获硕士学位；2000年3月研究生毕业于北京航空航天大学航空宇航推进理论与工程专业，获博士学位。
1990年3月至1993年8月留校任教于北京航空航天大学机电工程系第六研究室，从事磨擦学流体润滑专业方向的教学与科研方向；1993年9月至今，在北京航空航天大学leyucom乐鱼官网宇航推进系从事航天推进领域的教学与科研工作。1995年7月晋升为副教授，2002年7月晋升为教授，2004年被聘为博士生导师。
现任2018-2022年教育部高等学校航空航天类专业教学指导委员会秘书长（2018.11-），中国航天第三专业信息网副网长（2017.8-），中国航天第三专业信息网（中国空天动力联合会）液体推进技术专业委员会主任（2019.8-），核心期刊《推进技术》副主编（2016.1-），核心期刊《固体火箭技术》编委会委员（2016.8-），核心期刊《火箭推进》编委会委员（2017.9-），内部期刊《固体推进技术》编委会委员（2016-）、内部期刊《空间推进》编委会委员（2007.1-）。
曾任北航leyucom乐鱼官网宇航推进系教学副主任和科研副主任（1994-2009），中国空气动力学学会物理气体动力学第五届专业委员会委员（2005-2010），期刊《推进技术》编委会成员（2004-2015），中国机械工程学会焊接学会第九届切割专业委员会委员（2011-2016），2013-2017年教育部高等学校航空航天类专业教学指导委员会秘书长（2013-2017），北航leyucom乐鱼官网教学副院长（2009-2019）。
研究方向
火箭发动机设计、仿真与优化集成研究；火箭发动机点火与燃烧过程研究；新型点火技术研究；运载火箭贮箱增压输送系统动力学研究；航天飞行器姿轨控动力系统总体设计与实验研究；姿轨控发动机地面与高空模拟试验技术研究。
教学与科研成果
北京市1997年度优秀教师（1997），北京市高等教育一等奖（2008）。
主持或参与多项包括国家自然科学基金项目、863项目和航天院所合作项目的研究工作。在国内外刊物和学术会议上发表学术论文100多篇。
获航空总公司科技进步三等奖一项（1996），航天总公司科技进步三等奖一项（1997）。
主讲课程
主要讲授本科生核心专业课“火箭发动机原理”和硕士生专业基础理论课“两相流体动力学”，以及外国留学研究生专业课“Fundamentals of Rocket Propulsion（火箭推进基础）”。曾主讲硕士生专业课“火箭发动机工作过程数值仿真”。
现指导多名硕士、博士研究生和外国留学生。
Liang Guozhu
Ph.D., Professor, and Doctorial Advisor
E-mail：lgz@buaa.edu.cn
Office：Main Building D621（Shahe Campus），BUAA
Phone：010-61716982
Education
1987, B.S., Solid Rocket Engine, Beijing University of Aeronautics and Astronautics(BUAA)
1990, M.Sc, Solid Rocket Engine, Beijing University of Aeronautics and Astronautics(BUAA)
2000, Ph.D., Aerospace Propulsion Theory and Engineering, Beijing University of Aeronautics and Astronautics(BUAA)
Biography
Liang Guozhureceived his BEng (1987) and MSc (1990) in Solid Rocket Motor Design, and Ph.D. (2000) in Aerospace Propulsion Theory and Engineering from Beijing University of Aeronautics and Astronautics (BUAA), respectively. He was promoted to associated professor in 1995 and to full professor in 2002. His research interests cover a wide spectrum of topical areas focusing on combustion, flow, heat transfer, and design for solid and liquid rocket propulsion, and tank pressurization system dynamics for launch vehicles. He supervises domestic and foreign M.S. and Ph.D. students in the field of rocket propulsion. He is the author or co-author of more than 100 technical papers and was the recipient of several teaching and research awards from government organizations. At present, He is Secretary General of the Teaching Steering Committee of the Ministry of Education of China for Aeronautics and Astronautics, Vice-Chairman of China Aerospace Propulsion Technology Information Society and Associate Editor of Chinese Journal of Propulsion Technology.
Teaching
Principle of rocket engine for undergraduate students
Numerical Simulation of rocket engine working process for graduate students
Two-phase fluid dynamics of rocket engine for graduate students
Fundamentals of rocket propulsion for foreign M.S. and Ph.D. students
Research
Integrated study on rocket engine design, simulation, and optimization
Experimental study on dynamic process of rocket engine ignition and combustion
Study on dynamics of launch vehicle pressurization feed system
Design and experimental study on attitude control and orbit maneuvering propulsion system for spacecraft
Honors and Distinctions
Third Prize of Science and Technology, China Aeronautical Industry Corporation, 1996
Third Prize of Science and Technology, China Astronautical Industry Corporation, 1997
Third Prize of Science and Technology, Ministry of Industry and Information Technology (MIIT) of the People's Republic of China, 2009
Annual Excellent Teacher, Beijing Municipal Commission of Education, 1997
First Prize of Higher Education, the People's Government of Beijing Municipality, 2008
Social Activities
Secretary General of the Teaching Steering Committee of the Ministry of Education of China for Aeronautics and Astronautics, 2018-2022
Deputy Dean of School of Astronautics, BUAA, 2009-2019
Associate editor of Chinese Journal of Propulsion Technology, 2016-present
Member of the editorial advisory boards of the Journal of Solid Rocket Technology, 2016- present
Member of the editorial advisory boards of the Journal of Solid Propulsion Technology, 2014- present
Member of the editorial advisory boards of the Journal of Space Propulsion, 2007-present
Member of the 9th Cutting Technology Committee of Chinese Welding Society, 2012-pressent
Member of the editorial advisory boards of the Journal of Propulsion Technology, 2004-2015
Vice head of the Department of Aerospace Propulsion, 1994-2009
Member of the 5th Physical Gas dynamics Committee of China Academic Society of Aerodynamics, 2005-2010
近五年发表的代表性文章/Selected Papers Published in recent 5 years
[1]Adel, Walid M., Liang, Guozhu. Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior[J]. CHINESE JOURNAL OF AERONAUTICS, 2019,32（2）：361-368
[2]Mahyar Naderi; Liang Guozhu. Static performance modeling and simulation of the staged combustion cycle LPREs[J]. Aerospace Science and Technology, 86, March 2019, Pages 30-46.
[3]Du Jialei, Liang Guozhu. Performance comparative analysis of hydrostatic bearings lubricated with low-viscosity cryogenic fluids[J]. Tribology International, 2019, 137: 139-151.
[4]Jiachao LI, Guozhu LIANG. Simulation of mass and heat transfer in liquid hydrogen tanks during pressurizing[J]. Chinese Journal of Aeronautics, 2019, 32(9):2068-2084.
[5]Jiachao LI, Guozhu LIANG, Pingping ZHU, et al. Numerical investigation of the operating process of the liquid hydrogen tank under gaseous hydrogen pressurization[J]. Aerospace Science and Technology, 2019.10, 93:1-16.
[6]Jiachao LI, Guozhu LIANG. Simulation of the gas and liquid behaviors in a liquid hydrogen tank with a straight pipe injector during pressurization[J]. Interfacial Phenomena and Heat Transfer, 2019, 7(1): 69-84.
[7]Liu, Shijie, Liang, Guozhu, Yang, Yichuan. A Strategy to fast determine Chaboche elasto-plastic model parameters by considering ratcheting[J]. INTERNATIONAL JOURNAL OF PRESSURE VESSELS AND PIPING, 2019, 172:251-260.
[8]Wei, Qiang, Liang, Guozhu. Numerical Simulation of ignition process for the Monomethyl Hydrazine-Nitrogen Tetroxide Thrusters[J]. JOURNAL OF PROPULSION AND POWER, 2019，35（4）：704-719
[9]李佳超,梁国柱.液氮贮箱常压停放实验与数值仿真[J].北京航空航天大学学报, 2018, 44(1): 99-107.
[10]李佳超,梁国柱.液氮贮箱自增压停放实验与数值仿真[J].宇航学报, 2018, 39(4): 426-434.
[11]Zhongjian FANG; Guozhu LIANG. Transient simulation of a differential piston warm gas self-pressurization system for liquid attitude and divert propulsion system. Chinese Journal of Aeronautics, 2018，31（4）：698-709.
[12]杜家磊，闫攀运，梁国柱.涡轮泵流体静压轴承性能计算与试验研究[J].北京航空航天大学学报, 2018, 44 (2): 322-332.
[13]方忠坚,梁国柱.差动活塞式热气自增压系统优化设计（英文）.推进技术，39（8），2018，1905-1920.
[14]方忠坚,刘洌,梁国柱.差动活塞式热气自增压系统静态特性仿真研究.推进技术，39（3），2018，538-545.
[15]Walid M. Adel, LIANG Guo-zhu. Comparative Study on Different Methods for Developing Relaxation Modulus Master Curves of AP-HTPB Solid Propellant [J], Chinese Journal of Energetic Materials, 2017, 25(10) :810-816.
[16]Walid M. Adel, LIANG Guo-zhu. Analysis of Mechanical Properties for AP/HTPB Solid Propellant under Different Loading Conditions [J], International Journal of Aerospace and Mechanical Engineering, 2017, 11(12).
[17]Liu Shijie;Liang Guozhu. OPTIMIZATION OF CHABOCHE KINEMATIC HARDENING PARAMETERS BY USING AN ALGEBRAIC METHOD BASED ON INTEGRAL EQUATIONS. JOURNAL OF MECHANICS OF MATERIALS AND STRUCTURES. 2017 ,12, (4), 439-455.
[18]Wei, Qiang; Liang, Guozhu. Coupled Lagrangian impingement spray model for doublet impinging injectors under liquid rocket engine operating conditions. Chinese Journal of Aeronautics, Volume 30, Issue 4, August 2017, Pages 1391-1406.
[19]卫强,梁国柱.液体姿控发动机76 km高空模拟试验系统性能仿真[J].北京航空航天大学学报, 2017, 43(9): 1779-1788.
[20]Yan Panyun, Liang Guozhu, Lyu Yongzhi, et al. Modelling and simulation on multibody dynamics for vehicular cold launch systems based on subsystem synthesis method[A]. IOP Conference Series: Science and Engineering[C].3RD INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING AND AUTOMATION SCIENCE (ICMEAS 2017). IOP Publishing, 2017, 280(1): 012026.
[21]闫攀运,梁国柱,吕永志,等.车载冷发射刚柔耦合动力学建模与仿真[J].兵工学报, 2017, 22(1): 88-91.
[22]卫强,郭红杰,刘洌,等.基于PXI的液体姿轨控发动机试验测控系统设计与实现[J].航空动力学报, 2016, 31(12): 2979-2987.
[23]闫攀运,梁国柱,吕永志,等.车载冷发射多刚体动力学快速仿真研究[J].北京航空航天大学学报, 2016, 43(1): 71-78.
[24]刘洌,卫强,梁国柱等.小推力高室压NTO/MMH发动机试验系统管路流阻特性试验[J].航空动力学报, 2016, 31(3): 746-755.
[25]Liu Lie, Liang Guozhu. Optimization Selection of Regulated Pressurization System Schemes for Liquid Attitude and Divert Propulsion Systems [J]. Procedia Engineering, 2015, 99: 1247-1251.
[26]刘士杰，梁国柱.航天飞机主发动机高压燃料涡轮泵的故障模式[J].航空动力学报，2015 30（03）：611-626
[27]刘士杰，梁国柱.重复使用液体火箭发动机可用度的数字仿真[J].北京航空航天大学学报，2015 41（12）：2319-2327
[28]Lei, Zong-qi; Liang, Guo-zhu. Solution of turbine blade cascade flow using an improved panel method. International Journal of Aerospace Engineering, 2015,DOI: 10.1155/2015/312430.
