期刊文献+

陈乃兴先生的主要学术成就和对科技发展的重要贡献:隆重纪念陈乃兴先生逝世一周年

Professor Naixing Chen’s main academic achievements and significant contributions to the development of science and technology:In memory of professor Naixing Chen’s one-year anniversary
原文传递
导出
摘要 2019年8月6日是中国著名工程热物理学家陈乃兴先生逝世一周年的纪念日。从6个方面详细阐述了陈乃兴先生的主要学术成就和对科技发展的重要贡献。他一生献身祖国、献身科学研究的拼搏精神,将鼓舞大家砥砺奋进。 August 6,2019 is one-year anniversary in memory of Professor Naixing Chen,one of the renowned engineering thermophysicists in China.This article consists of six parts,elaborating Professor Chen's main academic achievements and major contributions to the scientific development in China.He devoted all his life to the engineering thermophysics field of his country,and his spirit in terms of the pursuit of excellence will always be an inspiration for us to forge ahead.
作者 王保国 黄伟光 徐燕骥 WANG Baoguo;HUANG Weiguang;XU Yanji(Beijing Institute of Technology,Beijing 100081,China;Shanghai Advanced Research Institute,Chinese Academy of Sciences,Shanghai 201210,China;Shanghai Xinzhe Mechatronics Technology Development Co.,Ltd.,Shanghai 201821,China)
出处 《航空学报》 EI CAS CSCD 北大核心 2019年第10期1-8,共8页 Acta Aeronautica et Astronautica Sinica
关键词 学术贡献 工程热物理 航空发动机 气动热力学 优化设计 反问题 scientific contributions engineering thermophysics aero-engine aerothermodynamics optimal design inverse problem
  • 相关文献

参考文献23

二级参考文献68

  • 1黄伟光,刘建军.两种TVD格式在跨音透平叶栅流场计算中的应用[J].工程热物理学报,1995,16(3):309-312. 被引量:1
  • 2陈乃兴,黄伟光,周倩.跨音速单转子压气机三维湍流流场的数值计算[J].航空动力学报,1995,10(2):109-112. 被引量:22
  • 3高学林,袁新.叶轮机械全三维粘性气动优化设计系统[J].中国电机工程学报,2006,26(4):88-92. 被引量:23
  • 4Naixing Chen Hongwu Zhang Yanji Xu Weiguang Huang Institute of Engineering Thermophysics,Chinese Academy of Sciences,P.O.Box 2706,Beijing 100080,CHINA.E-mail:nxc@mail.etp.ac.cn,Fax:+8610-62573335.Blade Parameterization and Aerodynamic Design Optimization for a 3D Transonic Compressor Rotor[J].Journal of Thermal Science,2007,16(2):105-114. 被引量:4
  • 5[1]Luu T S,Viney B,Bencherif L.Inverse Problem Using S1 and S2 Approach for the Design of the Turbomachine with Splitter Blades[J].Revue Francaise de Mecanique,1992,(3).
  • 6[2]Chen Nai-xing,Li Wei-hong.A Method for Solving Aerodynamic Hybric Problem of Profile Cascade on S1 Stream Surface of Revolution by Employing Stream-Function Equation Expressed with Non-Orthogonal Coordinate System[A].Proc.International Conference on Inverse Design Concepts in Engineering Sciences (ICIDES)[C],Edited by G.S.Dulikravich,1984.
  • 7[3]Chen Nai-xing,Zhang Feng-xian,Li Wei-hong.An Inverse (Design) Problem Solution Method for Blade Cascade Flow on Stream Surface of Revolution[J].Journal of Turbomachinery, Trans. ASME,1986,108(2):194-199.
  • 8[4]Chen Nai-Xing,John J J,Chen X D.A SFC Inverse Method with the Distribution of Target Circulation or its First Derivative for Turbomachine Design[A].Proceeding,the 7th International Rotational Machinery Conference[C],Feb.,1998:1386-1393.
  • 9[5]Chen Nai-xing.Numerical Methods for Inverse Solution in Aerodynamic Design of Turbomachinery[J].Recent Development of Aerodynamic Design Methodologies-Inverse Design and Optimization-,Edited by K.Fujii and G.S.Dulikravich,Friedr.Vieweg and Sohn Verlagsgesellschaft mbH,Braunschweig/Wiesbaden,1999:113-145.
  • 10[6]Chen Nai-xing,Xu Yan-ji.Numerical Computation of 3-D Turbulent Flow in Turbine Cascade[J].Chinese Sciences Bulletin,1990,35(14).

共引文献1381

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部