Structural-Optimization Strategy for Composite Wing Based on Equivalent Finite Element Model-Reference-Cited by-同舟云学术

Structural-Optimization Strategy for Composite Wing Based on Equivalent Finite Element Model

Published:2016-03 Issue:2 Volume:53 Page:351-359
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wang Yu¹,Ouyang Xing¹,Yin Hailian¹,Yu Xiongqing¹

Affiliation:

1. Department of Aerospace Engineering, Key Laboratory of Fundamental Science for National Defense–Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033469

Reference19 articles.

1. Preliminary design of composite wings for buckling, strength and displacement constraints

2. Two-level composite wing structural optimization using response surfaces

3. Optimum Buckling Design for Composite Wing Cover Panels with Manufacturing Constraints

4. Structural Optimization of Composite Wings in an automated Multi-Disciplinary Environment

5. Aeroelastic design of a composite wing with wind tunnel investigation

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