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    Hygrothermal Stress Analysis in Composite Laminatesby Perturbation Method

    , M.Sc. Thesis Sharif University of Technology Jenabi, Farhad (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    For studying the hygrothermal deformation of generally laminated composite platesunder uniform temperature change and uniform moisture absorption change, by starting from the reduced form of elasticity displacement field for a long flat laminate, an analytical method is developed in order to accurately calculate the interlaminar stresses near the free edges of the laminate. The constant parameters appearing in the reduced displacement field, describe the global deformation of the laminate and appropriately obtained by employing an improved first-order shear deformation theory.For solving the coupled equilibrium equations of agenerally laminated composite plate, some of the stiffness... 

    Nonlinear Forced Vibrations of Thin Circular and Elliptical Functionally Graded Plates

    , M.Sc. Thesis Sharif University of Technology Ghaheri, Ali (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    Nonlinear forced vibrations of thin functionally graded circular and elliptical plates under classical boundary conditions are investigated based on the classical plate theory. The von Kármán strain-displacement relations is employed to include geometrical nonlinearity caused by large transverse displacements of the plate thickness order, and modal expansion in polar and elliptical coordinate along with the perturbation method of multiple scale is used to solve the governing equations. The material properties are graded through the plate thickness according to a power-law distribution of the volume fraction of the constituents. Transverse forcing is supposed to be harmonic with angular... 

    Inter-Laminar Stress Analysis in Boundary Layer Region of Symmetrically Laminated Plates Under Torsion

    , M.Sc. Thesis Sharif University of Technology Jamalimehr, Amin (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    In the present research an analytical solution is studied for interlaminar stresses in boundary layer region of symmetric composite laminates under torsion. Based on geometrical and physical grounds the existing displacement field in literature is simplified in order to accommodate to torsion of symmetric laminates. Displacement field is divided to global and local parts. The solution procedure consists of combined equivalent single layer theories and layerwise theory of Reddy. ESL theories are more computationally economic while LWTs are considerably accurate in determining local behavior of plate. Further, based on second order shaer deformation theory and Ritz approximate variational... 

    Linear and Nonlinear Thermoelastic Analysis of Functionally Graded Circular Plates and Cylindrical Bending of FG Plates

    , Ph.D. Dissertation Sharif University of Technology Fallah Rajabzadeh, Famida (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    In the present study, analytical solutions within first-order shear deformation plate theory (FSDT), are presented for the linear and nonlinear asymmetric bending of functionally graded circular plates subjected to thermo-mechanical loading and boundary layer phenomenon is also investigated. To this end, cylindrical bending of long rectangular FG plates is also considered to study the perturbation technique which is used here to solve the nonlinear equations. Functionally graded materials are mostly used in high temperature environments and the study of their behavior under thermal and mechanical loadings and in small and large deflection ranges has become very important. Here, the linear... 

    Stress Analysis in Symmetric Composite Laminates Subjected to Shearing Load

    , M.Sc. Thesis Sharif University of Technology Mousanezhad Viyand, Davood (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    In the present study, an analytical solution is developed to calculate the interlaminar stresses in long symmetric laminated composite plates subjected to shearing load. At first, upon the successive integrations of the strain-displacement relations and using the existing patterns in deformation of a long symmetric laminate, the general displacement field is extracted and simplified to the final form. Presented solution is based on a combined method containing the equivalent single-layer (ESL) theories beside the Reddy’s layerwise theory. In this method, the equivalent single-layer theories are utilized because of their simplicity and low computational efforts rather than the layerwise... 

    Stress Analysis of in Cross-ply Laminates in Bending

    , M.Sc. Thesis Sharif University of Technology Yazdani Sarvestani, Hamid Reza (Author) ; Nosier, Asghar (Supervisor)
    Abstract
    In the present study, an analytical solution is developed to calculate the interlaminar stresses in long generally cross-ply laminated composite plates subjected to bending. At first, upon the integration of the strain-displacement relations and using the existing patterns in deformation of the long laminate, the general displacement field is extracted and simplified to the final form. Presented solution is based on a combined method containing the equivalent single-layer (ESL) theories beside the Reddy’s layerwise theory. In this method, the equivalent single-layer theories are utilized because of their simplicity and low computational efforts rather than the layerwise theory in evaluation... 

    Non-linear analysis of functionally graded circular plates under asymmetric transverse loading

    , Article International Journal of Non-Linear Mechanics ; Volume 44, Issue 8 , 2009 , Pages 928-942 ; 00207462 (ISSN) Nosier, A ; Fallah, F ; Sharif University of Technology
    2009
    Abstract
    Based on the first-order shear deformation plate theory with von Karman non-linearity, the non-linear axisymmetric and asymmetric behavior of functionally graded circular plates under transverse mechanical loading are investigated. Introducing a stress function and a potential function, the governing equations are uncoupled to form equations describing the interior and edge-zone problems of FG plates. This uncoupling is then used to conveniently present an analytical solution for the non-linear asymmetric deformation of an FG circular plate. A perturbation technique, in conjunction with Fourier series method to model the problem asymmetries, is used to obtain the solution for various clamped... 

    Interlaminar stresses in antisymmetric angle-ply laminates

    , Article Composite Structures ; Volume 78, Issue 1 , 2007 , Pages 18-33 ; 02638223 (ISSN) Nosier, A ; Bahrami, A ; Sharif University of Technology
    2007
    Abstract
    Based on elasticity theory the reduced form of displacement field is developed for long antisymmertic angle-ply composite laminates subjected to extensional and/or torsional loads. Analytical solutions to the edge-effect problem of such laminates under a uniform axial strain are developed using the first-order shear deformation theory of plates and Reddy's layerwise theory. For a special set of boundary conditions an elasticity solution is presented to verify the validity and accuracy of the layerwise theory. Various numerical results are then developed within the layerwise theory for the interlaminar stresses through the thickness and across the interfaces of antisymmetric angle-ply... 

    Free-edge stresses in general composite laminates

    , Article International Journal of Mechanical Sciences ; Volume 50, Issue 10-11 , 2008 , Pages 1435-1447 ; 00207403 (ISSN) Nosier, A ; Maleki, M ; Sharif University of Technology
    2008
    Abstract
    In the present study, by starting from the reduced form of elasticity displacement field for a long flat laminate, an analytical method is developed in order to accurately calculate the interlaminar stresses near the free edges of generally laminated composite plates under extension. The constant parameter appearing in the reduced displacement field, which describes the global rotational deformation of a laminate, is appropriately obtained by employing an improved first-order shear deformation theory. The accuracy and effectiveness of the proposed first-order theory are verified by means of comparison with the results of Reddy's layerwise theory as a three-dimensional benchmark. Reddy's... 

    Reformulation of Mindlin-Reissner governing equations of functionally graded circular plates

    , Article Acta Mechanica ; Volume 198, Issue 3-4 , 2008 , Pages 209-233 ; 00015970 (ISSN) Nosier, A ; Fallah, F ; Sharif University of Technology
    2008
    Abstract
    The governing equations of the first-order shear deformation plate theory for FG circular plates are reformulated into those describing the interior and edge-zone problems. Analytical solutions are obtained for axisymmetric and asymmetric behavior of functionally graded circular plates with various clamped and simply-supported boundary conditions under mechanical and thermal loadings. The material properties are graded through the plate thickness according to a power-law distribution of the volume fraction of the constituents. The results, which are in closed form and suitable for design purposes, are verified with known results in the literature. It is shown that there are two... 

    Three dimensional analysis of laminated cylindrical panels with piezoelectric layers

    , Article International Journal of Engineering, Transactions B: Applications ; Volume 19, Issue 1 , 2006 , Pages 61-72 ; 1728-144X (ISSN) Nosier, A ; Ruhi, M ; Sharif University of Technology
    Materials and Energy Research Center  2006
    Abstract
    A semi-analytical solution is presented for three dimensional elastic analysis of finitelylong, simply supported, orthotropic, laminated cylindrical panels with piezoelectric layers subjected to outer pressure and electrostatic excitation. Both the direct and inverse piezoelectric effects are investigated. The solution is obtained through reducing the highly coupled partial differential equations (PDE's) of equilibrium to ordinary differential equations (ODE's) with variable coefficients by means of trigonometric function expansion in longitudinal and circumferential directions. The resulting ODE's are solved by dividing the radial domain into some finite subdivisions and imposing necessary... 

    Free-edge stresses in antisymmetric angle-ply laminates in extension and torsion

    , Article International Journal of Solids and Structures ; Volume 43, Issue 22-23 , 2006 , Pages 6800-6816 ; 00207683 (ISSN) Nosier, A ; Bahrami, A ; Sharif University of Technology
    2006
    Abstract
    The first-order shear deformation theory and the layerwise theory of laminated plates are employed to analyze the edge-effect problem of an antisymmetric angle-ply laminate subjected to arbitrary combinations of extensional and torsional loads. The first-order theory is used for predicting the unknown constant parameters appearing in the reduced displacement field of elasticity which, on the other hand, signify the global behavior of the laminate. A layerwise theory is then utilized to determine the local interlaminar stresses within the boundary-layer regions of laminates. In order to closely examine the behavioral characteristics of interlaminar stresses, various numerical examples are... 

    Surface balance laws of linear and angular momenta and Cauchy's stress theorem

    , Article Scientia Iranica ; Volume 11, Issue 1-2 , 2004 , Pages 21-25 ; 10263098 (ISSN) Nosier, A ; Yavari, A ; Sharif University of Technology
    Sharif University of Technology  2004
    Abstract
    Using Helmholtz's decomposition theorem, the laws of balance of linear and angular momenta are restated as surface integrals over the closed surface of an arbitrary subregion in a continuum. Newton's law of action and reaction and Cauchy's theorem for stress and couple-stress are proved as corollaries of these surface balance laws. © Sharif University of Technology  

    Boundary-layer hygrothermal stresses in laminated, composite, circular, cylindrical shell panels

    , Article Archive of Applied Mechanics ; Volume 80, Issue 4 , 2010 , Pages 413-440 ; 09391533 (ISSN) Nosier, A ; Miri, A. K ; Sharif University of Technology
    2010
    Abstract
    Free-edge effects in laminated, circular, cylindrical shell panels subjected to hygrothermal loading are studied by utilizing displacement-based technical theories. Starting from the most general displacement field of elasticity for long, circular, cylindrical shells, appropriate reduced displacement fields are determined for laminated composite shell panels with cross-ply and antisymmetric angle-ply layups. An equivalent single-layer shell theory is used to analytically determine the constant parameters appearing in the reduced displacement fields. A layerwise shell theory is then employed to analytically determine the local displacement functions and the boundary-layer interlaminar... 

    A study of the edge-zone equation of Mindlin-Reissner plate theory in bending of laminated rectangular plates

    , Article Acta Mechanica ; Volume 146, Issue 3-4 , 2001 , Pages 227-238 ; 00015970 (ISSN) Nosier, A ; Yavari, A ; Sarkani, S ; Sharif University of Technology
    2001
    Abstract
    The bending equations of the Mindlin-Reissner theory of plates laminated of transversely isotropic layers are reformulated in terms of the boundary-layer and transverse displacement functions. Analytical expressions are obtained for the primary response quantities of rectangular laminates with various boundary conditions. It is found that various edge conditions have boundary-layer effects on the primary and secondary response quantities that can be characterized as nonexistent, weak, or strong. © Springer-Verlag 2001  

    On a boundary layer phenomenon in Mindlin-Reissner plate theory for laminated circular sector plates

    , Article Acta Mechanica ; Volume 151, Issue 3-4 , 2001 , Pages 149-161 ; 00015970 (ISSN) Nosier, A ; Yavari, A ; Sarkani, S ; Sharif University of Technology
    2001
    Abstract
    In this article, the edge-zone equation of Mindlin-Reissner plate theory, for composite plates laminated of transversely isotropic layers is studied. Analytical solutions are obtained for both circular sector and completely circular plates with various boundary conditions. The boundary-layer function and its effect on the stresses are numerically studied. Effects of plate thickness and boundary conditions are investigated. The results for circular and completely circular plates are exactly the same as those of rectangular plates in our previous work. Therefore, this boundary layer phenomenon seems to be geometry independent. © Springer-Verlag 2000  

    Post-buckling behavior of functionally graded circular plates under asymmetric transverse and in-plane loadings

    , Article Composite Structures ; Volume 125 , 2015 , Pages 477-488 ; 02638223 (ISSN) Fallah, F ; Vahidipoor, M. K ; Nosier, A ; Sharif University of Technology
    Elsevier Ltd  2015
    Abstract
    Based on the first-order nonlinear von Karman theory, the post-buckling analysis of FG circular plates under asymmetric transverse and in-plane loadings are presented. The nonlinear governing equations are reformulated using a stress function and a boundary layer function, and solved by employing a multi-parameter perturbation technique and Fourier series method. The material properties are assumed to vary through the plate thickness according to a power-law distribution of the volume fractions of the constituents. The results are verified with the known results in the literature. The effects of loading, material properties, and boundary conditions on different response quantities are... 

    Stress analysis in symmetric composite laminates subjected to shearing loads

    , Article International Journal of Mechanical Sciences ; Volume 75 , 2013 , Pages 16-25 ; 00207403 (ISSN) Mousanezhad viyand, D ; Yazdani Sarvestani, H ; Nosier, A ; Sharif University of Technology
    2013
    Abstract
    In the present study, an analytical solution is proposed to determine the interlaminar stresses in long symmetric laminated composite plates subjected to shearing loads. An improved first-order shear deformation theory (IFSDT) and a simplified IFSDT (SIFSDT) are utilized to calculate the unknown constants appearing in the reduced elasticity displacement field which actually demonstrate the global deformations of the plate. Then the numerical values of the interlaminar normal and shear stresses are established through the laminates by using Reddy's layerwise theory. Finally, several numerical examples are presented to study the interlaminar stresses in the interfaces of the layers and through... 

    Analysis of Interlaminar Stresses in Boundary Layer of Circumferentially Closed Laminated Cylinders

    , M.Sc. Thesis Sharif University of Technology Lotfalian, Reza (Author) ; Noseir, Asghar (Supervisor)
    Abstract
    In this study, using Reddy's layer-wise theory, thermal and rotational inter-laminar stress distribution within cylindrical composite shells with different boundary conditions is analytically studied. Convergence of the layer-wise theory is also studied and the numbers of sub-layers are determined so that efficient and accurate results can be achieved by this method. In order to assess the validity of layer-wise theory, results of this method are compared with results obtained by elasticity theory, for two sets of boundary conditions. It is observed that depending on the shell layer stacking, loading and boundary condition type, each of inter-laminar stresses may be the critical stress... 

    Nonlinear Analysis of FG Rectangular Plates under Mechanical and Thermo-Mechanical Loads using the Extended Kantorovich Method

    , M.Sc. Thesis Sharif University of Technology Moradkhani, Behrooz (Author) ; Nasier, Asghar (Supervisor)
    Abstract
    The purpose of this research is to provide an analytical solution using first order shear deformation theory for nonlinear bending of rectangular FG plate under mechanical and thermal loads with different boundary conditions. To achieve this goal, extended Kantorovich method have been used. This method has a high convergence rate and is more accurate than other approximate methods, such as the Ritz and Galerkin methods, because the partially differential equations are converted to ordinary differential equations. In order to solving nonlinear odes the perturbation method is used. Material of the plate is a mixture of ceramic and metal and is modeled as an isotropic and non-homogeneous...