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Comparison of first-order and higher-order basic theories in calculating critical buckling load of marine sandwich panels

عنوان مقاله: Comparison of first-order and higher-order basic theories in calculating critical buckling load of marine sandwich panels
شناسه ملی مقاله: COMPOSIT08_081
منتشر شده در هشتمین کنفرانس بین المللی مواد کامپوزیتی: ساخت، خواص و کاربرد در سال 1401
مشخصات نویسندگان مقاله:

J Orooji - Department of Maritime Engineering, Amirkabir University of Technology, Tehran, Iran
M.S Kiasat - Associate Professor, Department of Maritime Engineering, Amirkabir University of Technology, Tehran, Iran

خلاصه مقاله:
This paper focuses on some of the most widely used theories for global buckling of sandwich panels, (a) Allen's thickface version formula (first-order), (b) High-Order Sandwich Panel Theory (HSAPT) and (c) Extended High-OrderSandwich Panel Theory (EHSAPT). These three theories provide the most accurate and well-known buckling analysismethods for sandwich panels. In order to evaluate the accuracy and correctness of these theories, the bucklingbehavior of some carbon/epoxy PVC core composite sandwich panels are experimentally studied in this work.

کلمات کلیدی:
Carbon/epoxy PVC core sandwich, Buckling test, Higher-order theory

صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/1603235/