Nonlinear Finite Element Formulation for The Postbuckling Analysis of Stiffened Composite Panels with Imperfections
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Optimization of Composite, Stiffened, Imperfect Panels under Combined Loads for Service in the Postbuckling Regime
Local buckling and postbuckling of panels stiffened by stringers and rings and subjected to combined in-plane loads is explored with the use of a single module model that consists of one stringer and a width of panel skin equal to the stringer spacing. The cross-section of the skin-stringer module is discretized and the displacement field is assumed to vary trigonometrically in the axial direct...
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The investigation aims at: (i) constructing a modified higher-order shear deformation theory in which Kirchhoff's hypotheses are relaxed, to allow for shear deformations; (ii) validating the present 5-parameter-smeared-laminate theory by comparing the results with exact solutions; and (iii) applying the theory to a specific problem of the postbuckling behavior of a flat stiffened fiber-reinforc...
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For the lightly-loaded structures (200 lbs/in. in compression and 400 lbs/in. in shear), the traditional skin-stiffened structure is more efficient than sandwich structure due to the minimum gage requirements imposed on the sandwich structure. A design for minimum weight and cost Tstiffened panel that was designed for a 120 lbs/in. compression load and 337 lbs./in. shear loading condition is pr...
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It is empirically established that, due to a number of factors involved, a classical (linear) analysis of buckling pressure is impossible. Nonlinear theories of buckling are, therefore, required that involve effective factors such as imperfections and welding effects. In this study, models are developed which are as close to allowable standard deviations as possible. In the next stage, their bu...
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تاریخ انتشار 1998