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梁国柱
职称\职位:博士\教授\博士生导师
出生年月:1966年3月
电子邮箱:lgz@buaa.edu.cn 办公地点:北航新主楼B座1030
办公电话:010-82339944 传真:010-82338798
基本情况
梁国柱

19877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;19903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;20003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。19957月晋升为副教授,20027月晋升为教授,2004年被聘为博士生导师。

现任北航宇航学院教学副院长(2009-),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(2013.4-),固体火箭发动机燃烧、热结构与内流场国防科技重点实验室第六届学术委员会委员(2016.12-),中国航天第三专业信息网副网长,中国航天第三专业信息网液体推进技术专业委员会主任(2017.8-),核心期刊《推进技术》副主编(2016-),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-)。  

曾任北航宇航学院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)。  

研究方向
梁国柱

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。

科研成果
梁国柱

主持和完成了多项包括国家自然科学基金、863项目和航天基金等项目的研究工作。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),中国国防科学技术三等奖二项(19992009),中国国防科学技术二等奖一项(2001)。  

北京市1997年度优秀教师(1997),北京市高等教育一等奖(2008)。  

 

主讲课程
梁国柱

讲授本科生专业课“火箭发动机原理”和硕士生专业课“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。  

 

 

梁国柱

Liang Guozhu
Ph.D., Professor, and Doctorial Advisor
Deputy Dean of School of Astronautics, Beijing University of Aeronautics and Astronautics (BUAA)                                                                  

E-maillgz@buaa.edu.cn
Office
New Main Building B1030BUAA
Phone
010-82339944 Fax: 010-82338798                                                                  

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
Dr. Liang Guozhu received his Ph.D. from the Beijing University of Aeronautics and Astronautics (BUAA) in 2000. 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, and design for chemical rocket propulsion. He supervises domestic and foreign M.S. and Ph.D. students in the discipline of Aerospace Propulsion Theory and Engineering. 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.                                                                  

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, China National Defence Industry Committee, 1999
Second Prize of Science and Technology, China National Defence Industry Committee, 2001
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
Deputy Dean of School of Astronautics, BUAA, 2009-present
Deputy Editors in Chief of the 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

English Papers Published in recent years                                                                        

[1] Chen Wei, Liang Guo-zhu. Internal ballistic simulation of multi-burning-rate solid rocket motor based on parameterized feature CAD model. Journal of Aerospace Power, Vol.30, No. 12, 2015, 3017-3028.                                                                  

[2] Tarek M ElhederyLIANG Guo-zhu. Experimental Study on Influence of Composition on Mechanical Properties of Fuel-rich Composite Propellants. Chinese Journal of Energetic Materials, Vol23No82015 (802806)                                                                  

[3] Rafique, Amer F.; Zeeshan, Qasim; Kamran, Ali;Liang Guozhu. A new paradigm for star grain design and optimization. Aircraft Engineering and Aerospace Technology, 87(5), pp 476-482, 2015                                                                  

[4] Lei, Zong-qi; Liang, Guo-zhu. Solution of Turbine Blade Cascade Flow Using an Improved Panel Method. International Journal of Aerospace Engineering, 2015                                                                  

[5] Liu, Lie; Liang, Guozhu. Optimization Selection of Regulated Pressurization System Schemes for Liquid Attitude and Divert Propulsion Systems. Procedia Engineering, v 99, p 1247-1251, 2015, Asia-Pacific International Symposium on Aerospace Technology, APISAT 2014.                                                                  

[6] Chen, Liang;Liang, Guo-zhu. Simulation Research of Vaporization and Pressure Variation in a Cryogenic Propellant Tank at the Launch Site. Microgravity Science and Technology, 25(4), pp 203-211, 2013/12.                                                                    

[7] Kamran, Ali;Liang Guozhu; Rafique, Amer Farhan; Zeeshan, Qasim. +/- 3-Sigma based design optimization of 3D Finocyl grain. AEROSPACE SCIENCE AND TECHNOLOGY, 26(1), pp 29-37, 2013/5 APR-MAY.                                                                    

[8] Wang, Chong; Liang, Guozhu. Numerical simulation of pressurization system with real-gas equation. Proceedings of 2012 9th International Bhurban Conference on Applied Sciences and Technology, IBCAST 2012, p 241-246, 2012. Publisher:IEEE Computer Society.                                                                  

[9] Liang, Guozhu;Kamran, Ali. Performance analysis of a SRM nozzle-based on modeling of two-phase flow. Proceedings of 2012 9th International Bhurban Conference on Applied Sciences and Technology, IBCAST 2012, p 165-170, 2012. Publisher:IEEE Computer Society.                                                                  

[10] Kamran, Ali;Liang Guozhu. An integrated approach for optimization of solid rocket motor. Aerospace Science and Technology, 17(1), pp 50-64, 2012/3.                                                                    

[11] Amr, Elhefny; Liang, Guozhu. Stress of a rocket turbine under different loads using finite element modeling. Applied Mechanics and Materials, v 232, p 691-696, 2012; 2012 3rd International Conference on Mechanical and Aerospace Engineering, ICMAE 2012, July 7, 2012 - July 8, 2012.                                                                  

[12] Elhefny, Amr;Guozhu, Liang. Stress analysis of rotating disc with non-uniform thickness using finite element modeling. 1st International Conference on Engineering and Technology, ICET 2012, October 10, 2012 - October 11, 2012; Publisher:IEEE Computer Society.                                                                  

[13] Kamran, Ali;Liang Guozhu. Design and Optimization of 3D Radial Slot Grain Configuration. CHINESE JOURNAL OF AERONAUTICS, 23(4), pp 409-414, 2010/8.                                                                    

[14] Wang Dong;Liang Guozhu. Numerical Simulation of Internal Flow in Nitrous Oxide/Propane Coaxial Swirling Injector. PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, pp 1184-1187, 2010.                                                                    

[15] Tun, Zaw Naing;Liang Guozhu. Application of Method of Characteristics in Three Dimensional Supersonic Flows of Nozzles . PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, pp 359-362, 2010.                                                                    

[16] Guo, Hongjie;Liang, Guozhu. Theoretical and experimental investigation of influence of mixture ratio on hydrogen-oxygen detonation characteristics. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, August 2, 2009 - August 5, 2009; Publisher:American Institute of Aeronautics and Astronautics Inc.                                                                  

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