Optimization of Hybrid Laminates with Extension-Shear Coupling

المؤلفون المشاركون

Cui, Da
Li, Daokui

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2018، العدد 2018 (31 ديسمبر/كانون الأول 2018)، ص ص. 1-12، 12ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2018-05-27

دولة النشر

مصر

عدد الصفحات

12

الملخص 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.

نمط استشهاد جمعية علماء النفس الأمريكية (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

نمط استشهاد الجمعية الأمريكية للغات الحديثة (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

نمط استشهاد الجمعية الطبية الأمريكية (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

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1168072