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| 1 |
Deng Yangchen 1, 2,Zhan Guang,Gao Tong 1,Zhang Yining 2(1. Sino-French Laboratory of Concurrent Engineering, Department of Aircraft Manufacturing Engineering, Northwestern Polytechnical University,xi′an 710072,China) (2. Shenyang Aircraft Design & Research Institute, Shenyang 110035,China);Analysis and Synthesis Based Aircraft Wing Structural Layout Study[J];Aircraft Design;2004-02 |
| 2 |
Deng Yangchen 1, 2,Xiong Yan 3,Zhang Weihong 1,Zhang Yi’ning 2 (1.Sino-French Laboratory of Concurrent Engineering, Department of Aircraft Manufacturing Engineering,Northwestern Polytechnical University,Xi’an 710072, China) (2.Shenyang Aircraft Design & Research Institute, Shenyang 110035,China) (3.Shenyang Li-Gong University, Shenyang 110168,China);A Design Approach to Fuselage Frames in Aircraft Upgrade Design[J];Aircraft Design;2004-03 |
| 3 |
Deng Yangchen 1,2 ,Liu Xiaoou 2 ,Zhu Jihong 2 (1.Shenyang Aircraft Design & Research Institute,Shenyang 110035,China)(2.Institute of Manufacturing & Electricity Engineering,NorthwesternPolytechnical University,Xi’an 710072,China);An Approach to Structural Topology Optimization about Aircraft Reinforced Frames Design[J];Aircraft Design;2004-04 |
| 4 |
DENG Yang-chen~(1),QIN Zhengqi~(2),XU Qing-hua~(1),ZHANG Jian~(1)(1.Shenyang Aircraft Design & Research Institute,Shenyang 110035,China)(2.Shenyang Institute of Aeronautical Engineering,Shenyang 110031,China);Research of High Aspect Ratio Wing Structural Layout Based on Bionics[J];Aircraft Design;2006-03 |
| 5 |
WANG Wei,CHANG Nan(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China);Multi-Level Optimization in Wing Structural Configuration Design And Future Research Aspects[J];Aircraft Design;2007-05 |
| 6 |
MEI Li1,SUN Zhi-xiao2,JI Peng-bo1,DENG Yang-chen2(1.General Aviation Lab,Shenyang University of Aeronautics and Astronautics, Shenyang 110136,China)(2.Shenyang Aircraft Design & Research Institute,Shenyang 110135,China);The Design Study of the Rib-Like Structure Based on Topology and Size Optimization[J];Aircraft Design;2013-02 |
| 7 |
Xia Tianxiang,Yao Weixing(Key Laboratory of Fundamental Science for National Defense-advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);A Survey of Topology Optimization of Continuum Structure[J];Advances in Aeronautical Science and Engineering;2011-01 |
| 8 |
DENG Yang-chen~1 QIN Zheng-qi~2 (1.Shenyang Aircraft Design & Research Institute,Liaoning Shenyang 110035;2.Shenyang Institute of Aeronautical Engineering,Liaoning Shenyang 110031);Optimal design of airframe on aircraft structure[J];Journal of Shenyang Institute of Aeronautical Engineering;2006-05 |
| 9 |
CHEN Hua~1,DENG Yang-chen~2(1.School of Mechanical and Electronic Engineering,Northwestern Polytechnical University,Xi′an 710072,China;2.Department One,Shenyang Aircraft Design & Research Institute,Shenyang 110035,China);Application of Aircraft Structural Part Conceptual Design Based on Topology Optimization Method[J];Aeronautical Computing Technique;2006-05 |
| 10 |
DENG Yang-chen,CHEN Hua (1.Department One,ShenYang Aircraft Design & Research Institute,Shenyang 110035,China;2.School of Mechanical and Electronic Engineering,Northwestern Polytechnical University,Xi′an 710072,China);Research of High Aspect Ratio Straight Wing Structural Layout Based on Bionics[J];Aeronautical Computing Technique;2007-02 |
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