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گواهی نمایه سازی مقاله Effect of thickness of the panel on the buckling load of piezoelectric cylindrical composite panels reinforced withcarbon nanotubes

عنوان مقاله: Effect of thickness of the panel on the buckling load of piezoelectric cylindrical composite panels reinforced withcarbon nanotubes
شناسه (COI) مقاله: MINMETALCONF01_085
منتشر شده در کنفرانس بین المللی مهندسی معدن، فلزات و مواد در سال ۱۳۹۴
مشخصات نویسندگان مقاله:

M Eskandari - Department of Mechanical Engineering, Kashan Branch, Islamic Azad University, Kashan, Iran
M Nasihatgozar - Department of Mechanical Engineering, Kashan Branch, Islamic Azad University, Kashan, Iran
V Daghigh - Young Researchers and Elite Club, Jasb Branch, Islamic Azad University, Delijan, Iran

خلاصه مقاله:
This article presents the effect of thickness of the panel on buckling load of piezoelectriccylindrical composite panels reinforced with carbon nano-tubes subjected to axial load isinvestigated. Classical laminated plate theory (CLPT) is employed to reach stress anddisplacement correlations embracing mechanical and magnetic terms. Stress-strainequations for piezoelectric cylindrical panels reinforced with carbon nanotubes are thenwritten by using Mori-Tanaka method. The results suggest that changing the panelthickness changes the buckling load however the changes are completely nonlinear. Inorder to verify the solution approach, motivated by a recent research work published byInterna

کلمات کلیدی:
Thickness of the panel, buckling load, nanocomposite, piezoelectric cylindrical shell, Mori–Tanaka model

صفحه اختصاصی مقاله و دریافت فایل کامل: https://www.civilica.com/Paper-MINMETALCONF01-MINMETALCONF01_085.html