Critical buckling load prediction of composite cylinders by usingvarious shell theories and FEM under compressive loading
عنوان مقاله: Critical buckling load prediction of composite cylinders by usingvarious shell theories and FEM under compressive loading
شناسه ملی مقاله: COMPOSIT04_178
منتشر شده در چهارمین کنفرانس بین المللی کامپوزیت در سال 1393
شناسه ملی مقاله: COMPOSIT04_178
منتشر شده در چهارمین کنفرانس بین المللی کامپوزیت در سال 1393
مشخصات نویسندگان مقاله:
Behrooz F. Taheri - Assistant Professor, School of Mechanical Engineering, Iran University of Science and Technology, Tehran, ۱۶۸۴۶-۱۳۱۱۴,Iran
M Omidi - Graduate Student, School of Mechanical Engineering, Iran University of Science and Technology,Tehran, ۱۶۸۴۶-۱۳۱۱۴, Iran
خلاصه مقاله:
Behrooz F. Taheri - Assistant Professor, School of Mechanical Engineering, Iran University of Science and Technology, Tehran, ۱۶۸۴۶-۱۳۱۱۴,Iran
M Omidi - Graduate Student, School of Mechanical Engineering, Iran University of Science and Technology,Tehran, ۱۶۸۴۶-۱۳۱۱۴, Iran
In this manuscript, critical buckling load of thin-walled composite cylinders under axial compressive load are obtained from the Sanders-Koiter and Donnell's shell theories and compared with the finite element results extractedby non-linear arc length incrementation method. Cylinders which are examined had a certain stacking sequence of [± /± / ]s and simply supported boundary conditions with different R/t and L/R ratios.predicted results by various analytical and FE methods do not revealed acceptable consistency for the fiber orientations between 10 to 85 degrees, however for fiber orientations between 0 to 10 and 85 to 90 degrees they showed acceptablecorrelation. In addition, it was shown that increasing R/t ratios to the values more than of 550, resulted in inconsistency reduction of Donnell's theory results with Sanders-Koiter theory and FEM.
کلمات کلیدی: Buckling, Composite cylinder, Sanders-Koiter's theory, Donnell's theory, Finite element method
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/386830/