Research on Optimum Design of Composite Plate Wings for Aeroelastic Characteristics Using Lamination Parameters (The First Report)-flutter and Divergence Characteristics of Composite Plate Wings-
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/51/595/51_595_441/_pdf
Reference17 articles.
1. Aeroelastic tailoring - Theory, practice, and promise
2. A Survey of Aeroelastic Tailoring Technology.
3. 3) Housner, J. M. and Stein, M.: Flutter Analysis of Swept-Wing Subsonic Aircraft with Parameter Studies of Composite Wings, NASA TN D-7539, 1974.
4. Control of aeroelastic instabilities through stiffness cross-coupling
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Stacking-Sequence Optimization of Composite Delta Wing to Improve Flutter Limit Using Fractal Branch and Bound Method;JSME International Journal Series A;2005
2. Research on Optimum Design of Composite Plate Wings for Aeroelastic Characteristics Using Lamination Parameters (The Second Report)-Optimum Design of Composite Plate Wings for Flutter and Divergence Characteristics-;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003
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