Thermal postbuckling analysis of laminated cross-ply truncated circular conical shells
TL;DR: In this article, the authors studied the thermoelastic postbuckling behavior of cross-ply laminated composite conical shells under a presumed uniform temperature distribution, and evaluated the minimum temperature parameter that causes the bifurcation of shell deformation from axisymmetric deformation mode to asymmetric one.
About: This article is published in Composite Structures.The article was published on 2005-10-01. It has received 45 citations till now. The article focuses on the topics: Thermoelastic damping & Buckling.
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TL;DR: In this article, the authors investigated linear thermal buckling of a composite conical shell made from a polymeric matrix and reinforced with carbon nanotube fibres, under the assumption of first order shear deformation shell theory, Donnell kinematic assumptions and von Karman type of geometrical nonlinearity.
141 citations
TL;DR: In this article, a review of the static analysis of composite shells is presented, with an emphasis on the analysis performed (static, buckling, postbuckling, and others), complicating effects in both material (e.g. piezoelectric) and structure (i.e. stiffened shells), and various shell geometries (cylindrical, conical, spherical and others).
Abstract: Laminated composite shells are frequently used in various engineering applications including aerospace, mechanical, marine, and automotive engineering. This article reviews the recent literature on the static analysis of composite shells. It follows up with the previous work published by the first author [1-4] and it is a continuation of another recent article that focused on the dynamics of composite shells [3]. This paper reviews most of the research done in recent years (2000-2010) on the static and buckling behavior (including postbuckling) of composite shells. This review is conducted with an emphasis on the analysis performed (static, buckling, postbuckling, and others), complicating effects in both material (e.g. piezoelectric) and structure (e.g. stiffened shells), and the various shell geometries (cylindrical, conical, spherical and others). Attention is also given to the theory being applied (thin, thick, 3D, nonlinear …). However, more details regarding the theories have been described in previous work [1,3].
94 citations
Cites background from "Thermal postbuckling analysis of la..."
...[141,193,194,222], Shevchenko and Babeshko [213,214], Zenkour and Fares [166], Wang and Dai [139], Zhu et al....
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...[193,194], Lee and Lee [217], Rahman and Jansen [131], Li and Lin [34], Panda and Ramachandra [130], and Sai Ram and Sreedhar [218]....
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TL;DR: In this paper, the thermal buckling loads of truncated conical shells of functionally graded material are considered, where the material properties of the shells are assumed to vary continuously through his thickness of the shell, according to a power law distribution of the volume fractions of the constituents.
72 citations
TL;DR: In this article, the authors investigated the bifurcation behavior of a heated conical shell made of a through-the-thickness functionally graded material and obtained properties of the shell based on a power law form across the thickness.
Abstract: Bifurcation behavior of heated conical shell made of a through-the-thickness functionally graded material is investigated in the present research. Properties of the shell are obtained based on a power law form across the thickness. Temperature dependency of the constituents is also taken into account. The heat conduction equation of the shell is solved based on an iterative generalized differential quadrature method (GDQM). General nonlinear equilibrium equations and the associated boundary conditions are obtained using the virtual displacement principle in the Donnell sense. The prebuckling solution of the shell is obtained under the assumption of linear membrane deformations. The stability equations are extracted via the concept of the adjacent equilibrium criterion. A semi-analytical solution employing the GDQM and trigonometric expansion is implemented to solve the stability equations. Numerical results of the present research are compared and validated with the known available data through the open literature. Some parametric studies are conducted to investigate the influences of various involved parameters, such as the cone semi-vertex angle, boundary conditions, power law index of composition rule, length to thickness ratio, and the radius to thickness ratio.
65 citations
Cites background from "Thermal postbuckling analysis of la..."
...[11,12] investigated the linear thermal buckling, nonlinear thermal buckling, and thermal postbuckling of laminated cross-ply conical shells....
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TL;DR: In this article, an analytical approach to investigate the linear buckling of truncated conical panels made of functionally graded materials and subjected to axial compression, external pressure and the combination of these loads is presented.
50 citations
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427 citations
TL;DR: In this article, a review of the literature on composite models, predictor-corrector procedures, the effect of temperature-dependence of material properties on the response, and the sensitivity of the thermomechanical response to variations in material parameters is presented.
Abstract: The focus of this review is on the hierarchy of composite models, predictor-corrector procedures, the effect of temperature-dependence of material properties on the response, and the sensitivity of the thermomechanical response to variations in material parameters. The literature reviewed is devoted to the following eight application areas: heat transfer; thermal stresses; curing, processing and residual stresses; bifurcation buckling; vibrations of heated plates and shells; large deflection and postbuckling problems; and sandwich plates and shells. Extensive numerical results are presented showing the effects of variation in the lamination and geometric parameters of temperature-sensitive angle-ply composite plates on the accuracy of thermal buckling response, and the sensitivity derivatives predicted by nine different modeling approaches (based on two-dimensional theories). The standard of comparison is taken to be the exact three-dimensional thermoelasticity solutions. Some future directions for research on the modeling of high-temperature multilayered composites are outlined. 448 ref., 16 figs., 11 tabs.
232 citations
TL;DR: In this article, the authors present expressions for incremental matrices that remain valid in the equilibrium equations and in the linear incremental equilibrium equations for truss elements, in-plane bending elements, membrane elements, and plate flexural elements.
Abstract: A common technique in geometrically nonlinear finite element analysis is to express the total potential in terms of Lagrangian displacement coordinates, differentiate the potential to obtain the equilibrium equations, and form the differentials of the equilibrium equations to obtain linear incremental equilibrium equations. The geometric nonlinearities in the strain-displacement equations give rise to incremental matrices in the preceding equations. The form of these matrices is not unique in the expression for the total potential. The paper presents expressions for incremental matrices that remain valid in the equilibrium equations and in the linear incremental equilibrium equations. The construction of such matrices is illustrated for truss elements, in-plane bending elements, membrane elements, and plate flexural elements. An examination of some of the recent literature indicates that some investigators have used inappropriate forms of these incremental matrices.
180 citations
TL;DR: A combined experimental-numerical method to evaluate powder thermal properties in laser powder bed fusion MSEC2018 (2018) A simplified and efficient analysis of Morton Effect GT2018(2018) Thermal Transport in Thorium Dioxide IMECE2017 (2017).
Abstract: Topic Collections Related Content Customize your page view by dragging and repositioning the boxes below. Related Journal Articles Filter by Topic > Homogenization of Reticulated Structures Appl. Mech. Rev (July, 2001) Research Advances in the Dynamic Stability Behavior of Plates and Shells: 1987–2005—Part I: Conservative Systems Appl. Mech. Rev (March, 2007) Historical review of Zig-Zag theories for multilayered plates and shells Appl. Mech. Rev (May, 2003) [+] View More Related Proceedings Articles Filter by Topic > A Combined Experimental-Numerical Method to Evaluate Powder Thermal Properties in Laser Powder Bed Fusion MSEC2018 (2018) A Simplified and Efficient Analysis of Morton Effect GT2018 (2018) Thermal Transport in Thorium Dioxide IMECE2017 (2017) [+] View More Related eBook Content Various Structures Design of Plate and Shell Structures> Chapter 12 Axially Loaded Members Design & Analysis of ASME Boiler and Pressure Vessel Components in the Creep Range> Chapter 2 Members in Bending Design & Analysis of ASME Boiler and Pressure Vessel Components in the Creep Range> Chapter 3 [+] View More Sections PDF Email Share Get Citation Get Alerts Some tools below are only available to our subscribers or users with an online account. SEARCH ADVANCED SEARCH Search Applied Mechanics Applied Mechanics Heat Transfer About ASME Digital Collection Email Alerts Library Service Center ASME Membership Contact Us Publications Permissions /Reprints Privacy Policy Terms of Use © 2019 ASME The American Society of Mechanical Engineers Journals Submit a Paper Announcements Call for Papers Title History Conference Proceedings About ASME Conference Publications Conference Proceedings Author Guidelines Conference Publications Toolbox eBooks About ASME eBooks Press Advisory & Oversight Committee Book Proposal Guidelines This site uses cookies. By continuing to use our website, you are agreeing to our privacy policy. | Accept Loading [Contrib]/a11y/accessibility-menu.js
173 citations