کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1717663 1520081 2016 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
A new approach for nonlinear dynamic buckling of S-FGM toroidal shell segments with axial and circumferential stiffeners
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
A new approach for nonlinear dynamic buckling of S-FGM toroidal shell segments with axial and circumferential stiffeners
چکیده انگلیسی

This paper presents an analytical approach to study the nonlinear dynamic buckling of sigmoid functionally graded material (S-FGM) toroidal shell segments surrounded by elastic foundations subjected to axial compression. Shells are reinforced by closely spaced rings and stringers. The nonlinear dynamic buckling analysis is based on the classical shell theory with von Kármán–Donnell-type of geometrical nonlinearity. By using the Galerkin method, the closed-form expression of the deflection–time curves is obtained. Numerical solutions are presented in tabular and graphical forms to investigate the deflection–time curves of FGM shells surrounded by elastic foundations. Finally, the influences of geometrical parameters, volume fraction index, elastic foundations, and the effectiveness of stiffeners on the nonlinear dynamic buckling of the S-FGM toroidal shell segments are discussed. The present results are compared with the available data for a special case.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 53, June 2016, Pages 1–9
نویسندگان
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