Optimization of Hybrid Laminates with Extension-Shear Coupling

Joint Authors

Cui, Da
Li, Daokui

Source

International Journal of Aerospace Engineering

Issue

Vol. 2018, Issue 2018 (31 Dec. 2018), pp.1-12, 12 p.

Publisher

Hindawi Publishing Corporation

Publication Date

2018-05-27

Country of Publication

Egypt

No. of Pages

12

Abstract EN

The introduction of hybrid composites into the structure with coupling effect can greatly reduce the cost of materials.

The expressions of stiffness coefficient, thermal stress, and thermal moment for hybrid laminates are derived based on the geometrical factors of laminates, and the necessary and sufficient conditions for the hybrid extension-shear-coupled laminates with immunity to hygrothermal shear distortion (HTSD) are further derived.

The extension-shear-coupled effect of hybrid laminates is optimized with improved differential evolution algorithm.

Results are presented for the hybrid laminates that consist of carbon fiber and glass fiber composite materials.

The hygrothermal effect and extension-shear-coupled effect are simulated and verified, meanwhile the robustness of hybrid laminates is analyzed by Monte Carlo method.

American Psychological Association (APA)

Cui, Da& Li, Daokui. 2018. Optimization of Hybrid Laminates with Extension-Shear Coupling. International Journal of Aerospace Engineering،Vol. 2018, no. 2018, pp.1-12.
https://search.emarefa.net/detail/BIM-1168072

Modern Language Association (MLA)

Cui, Da& Li, Daokui. Optimization of Hybrid Laminates with Extension-Shear Coupling. International Journal of Aerospace Engineering No. 2018 (2018), pp.1-12.
https://search.emarefa.net/detail/BIM-1168072

American Medical Association (AMA)

Cui, Da& Li, Daokui. Optimization of Hybrid Laminates with Extension-Shear Coupling. International Journal of Aerospace Engineering. 2018. Vol. 2018, no. 2018, pp.1-12.
https://search.emarefa.net/detail/BIM-1168072

Data Type

Journal Articles

Language

English

Notes

Includes bibliographical references

Record ID

BIM-1168072