|
1 |
Luo Mingqiang Feng Haocheng Liu Hu Wu Zhe (School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Rapid wing structure design and automated scheme adjustment for civil aircraft[J];Journal of Beijing University of Aeronautics and Astronautics;2009-04 |
2 |
Lan Yuanpei Jiao Qixiang Guan Zhidong(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Xu Guangxing(Material Application Office,Structure Department,AVIC Shenyang Aircraft Design Institute,Shenyang 110035,China);Development of aircraft-design material-selection expert system[J];Journal of Beijing University of Aeronautics and Astronautics;2010-11 |
3 |
Feng Haocheng Luo Mingqiang Liu Hu Wu Zhe(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Rapid aircraft structure modeling based on structure case base[J];Journal of Beijing University of Aeronautics and Astronautics;2012-05 |
4 |
ZHANG Tianyun1,3,CHEN Kui2,3,YANG Guang2,GU Li2 (1 Center of Information and Network,Lanzhou City University,Lanzhou 730070;2 College of Peili Engineering Technology,Lanzhou City University,Lanzhou 730070;3 State Key Laboratory of Gansu Advanced Non-ferrous Metal Materials,Lanzhou University of Technology,Lanzhou 730050);Development of Optimizing Selection Method for Engineering Materials[J];Materials Review;2011-23 |
5 |
JIA Jie,WANG Tao(Information Engineering College,Nanchang University of Aeronautics,Nanchang 330063,China);Aerodynamic optimization design for the three-dimensional wing[J];Flight Dynamics;2011-04 |
6 |
WANG Wei(College of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China);A New Evolutionary Structural Optimization Method and Its Application in the Wing Structure Topology Optimization[J];Aircraft Design;2007-04 |
7 |
HU Tian-yuan,YU Xiong-qing(College of Aerospace Engineering,Nanjing University of Aeronautics andAstronautics,Nanjing 210016,China);A Parametric Modeling of Flying-Wing Configuration Using API in CATIA[J];Aircraft Design;2007-06 |
8 |
CHENG Wenyuan1,CHANG Yan2,CUI Degang*1,XIE Xianghui2(1.School of Aeronautic Science and Technology,Beijing University of Aeronautics and Astronautics,Beijing100083,China;2.Jiangnan Institute of Computing Technology,Wuxi214083,China);Composite wing optimization design based on distributed computing[J];Acta Materiae Compositae Sinica;2007-01 |
9 |
LAN Yuan-pei1,MENG Qing-chun1,LI Feng2,XU Guang-xing3,GUAN Zhi-dong1(1.School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China;2.Military Representative Office in AVIC Shenyang Aircraft Corporation,Shenyang 110034,China;3.Structure Department,AVIC Shenyang Aircraft Design & Research Institute,Shenyang 110035,China);Aircraft Design Material-Selection Method Based on MAUT Theory[J];Journal of Aeronautical Materials;2010-03 |
10 |
YU Kua-hai,YUE Zhu-feng(School of Mechanics,Civil Engineering and Architecture,Northwestern Polytechnical University,Xi'an 710072,China);Parametric modeling and multidisciplinary design optimization for cooling turbine blade[J];Journal of Aerospace Power;2007-08 |
|