Shear-driving Force and Critical Shear Angle Analysis of Kevlar/Carbon Fiber Hybrid Composite Skins for a Shear Variable-sweep Wing Based on the Classical Plate Theory-Reference-Cited by-同舟云学术

Shear-driving Force and Critical Shear Angle Analysis of Kevlar/Carbon Fiber Hybrid Composite Skins for a Shear Variable-sweep Wing Based on the Classical Plate Theory

Published:2022-06-29 Issue:5 Volume:29 Page:1871-1887
ISSN:0929-189X
Container-title:Applied Composite Materials
language:en
Short-container-title:Appl Compos Mater

Author:

Yang Guang,Guo Hongwei^ORCID,Xiao Hong,Liu Rongqiang,Shi Chuang

Funder

Postdoctoral Research Foundation of China

National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Ceramics and Composites

Link

https://link.springer.com/content/pdf/10.1007/s10443-022-10044-1.pdf

Reference26 articles.

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3. Anderse, G. R., Cowan, D. L., et al.: Aeroelastic Modeling, Analysis and Testing of a Morphing Wing Structure. In: 48rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Honolulu, Hawaii (2007)

4. Bowman, J., Sanders, B., et al.: Development of Next Generation Morphing Aircraft Structures. In: 48rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Honolulu, Hawaii (2007)

5. Thill, C., Etches, J.A., et al.: Morphing skins. Aeronaut. J. 112(1129), 117–139 (2008)

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