Angle-Ply Laminate

14,000,000 Leading Edge Experts on the ideXlab platform

Scan Science and Technology

Contact Leading Edge Experts & Companies

Scan Science and Technology

Contact Leading Edge Experts & Companies

The Experts below are selected from a list of 8658 Experts worldwide ranked by ideXlab platform

Yoshinobu Tanigawa - One of the best experts on this subject based on the ideXlab platform.

  • Control of transient thermoelastic displacement of an Angle-Ply Laminated cylindrical panel bonded to a piezoelectric layer
    Applied Mathematics and Computation, 2004
    Co-Authors: Yoshihiro Ootao, Yoshinobu Tanigawa
    Abstract:

    In this study, the theoretical analysis of a control of transient thermoelastic displacement is developed for an Angle-Ply Laminated cylindrical panel bonded to a piezoelectric layer due to nonuniform heat supply. By using the exact solutions for Angle-Ply Laminate and piezoelectric layer of crystal class mm2, the theoretical analysis of a transient piezothermoelasticity is developed for a simply supported cylindrical composite panel under the state of generalized plane deformation. Analysis of a piezothermoelastic problem leads to an appropriate electric potential applied to the piezoelectric layer which suppresses the induced thermoelastic displacement in the radial direction at the midpoint on the free surface of the Angle-Ply Laminate. Some numerical results for the temperature change, the displacement, the stress in a transient state when the transient thermoelastic displacement is controlled are shown in figures.

  • analysis of transient thermal stress and thermal deformation of an angle ply Laminated rectangular plate due to nonuniform heat supply based on higher order shear deformation theory
    JSME international journal. Series A mechanics and material engineering, 1996
    Co-Authors: Yoshinobu Tanigawa, Kazuki Nagayama, Ryuusuke Kawamura
    Abstract:

    This article concerns a theoretical analysis of heat conduction in a transient state and the associated thermoelastic behavior for a multilayered anisotropic Laminated plate subjected to nonuniform heat supply. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal stack of layers having orthotropic material properties, i.e., an Angle-Ply Laminate. The three-dimensional temperature solution in a transient state and the associated thermoelastic behavior of the plate with simply supported edge conditions are formulated using the functional approach based on the variational principle. For the analysis of the thermoelastic field, the higher-order shear deformation theory of the plate is used to evaluate the shear stress components. As an example, numerical calculations are carried out for a 2 layered Angle-Ply Laminate, and the numerical results for temperature distribution, out-of-plane deflection, normal and shear stress distributions are discussed in detail.

  • transient thermal stress and thermal deformation of an angle ply Laminated rectangular plate due to nonuniform heat supply based on higher order shear deformation theory
    Transactions of the Japan Society of Mechanical Engineers. A, 1995
    Co-Authors: Yoshinobu Tanigawa, Kazuki Nagayama, Ryuusuke Kawamura
    Abstract:

    This paper is concerned with a theoretical treatment of thermal stress and thermal bending problems for a multi-layered anisotropic Laminated plate due to partially distributed heat supply. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal pile of layers having orthotropic material properties, i. e. an Angle-Ply Laminate. We obtain the three-dimensional temperature in a transient state and thermal deformation of a simply supported plate using the higher-order shear deformation theory. As an example, numerical calculations are carried out for a 2-layered Angle-Ply Laminate, and the numerical results are examined precisely.

  • analysis of thermal stress and deformation due to nonuniform heat supply in an angle ply Laminated rectangular plate
    Transactions of the Japan Society of Mechanical Engineers. A, 1995
    Co-Authors: Yoshinobu Tanigawa, Ryuusuke Kawamura, Tomohiro Takahara, Kazuki Nagayama
    Abstract:

    This paper describes theoretical treatment of problems of thermal stress and thermal bending due to partially distributed heat supply for a multilayered anisotropic Laminated plate. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal stack of layers having orthotropic material properties, i. e. an Angle-Ply Laminate. Introducing the Rayleigh-Ritz method based on the variational principle, a three-dimensional temperature solution for a transient state is given. Moreover, for the thermoelastic problems, the components of displacements are analyzed using the Rayleigh-Ritz method, and the characteristic behaviors of thermal stress and thermal deformation for a simply supported plate are determined. As an example, calculations are carried out for a 2-layered Angle-Ply Laminate, and the results are examined precisely.

Ryuusuke Kawamura - One of the best experts on this subject based on the ideXlab platform.

  • analysis of transient thermal stress and thermal deformation of an angle ply Laminated rectangular plate due to nonuniform heat supply based on higher order shear deformation theory
    JSME international journal. Series A mechanics and material engineering, 1996
    Co-Authors: Yoshinobu Tanigawa, Kazuki Nagayama, Ryuusuke Kawamura
    Abstract:

    This article concerns a theoretical analysis of heat conduction in a transient state and the associated thermoelastic behavior for a multilayered anisotropic Laminated plate subjected to nonuniform heat supply. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal stack of layers having orthotropic material properties, i.e., an Angle-Ply Laminate. The three-dimensional temperature solution in a transient state and the associated thermoelastic behavior of the plate with simply supported edge conditions are formulated using the functional approach based on the variational principle. For the analysis of the thermoelastic field, the higher-order shear deformation theory of the plate is used to evaluate the shear stress components. As an example, numerical calculations are carried out for a 2 layered Angle-Ply Laminate, and the numerical results for temperature distribution, out-of-plane deflection, normal and shear stress distributions are discussed in detail.

  • transient thermal stress and thermal deformation of an angle ply Laminated rectangular plate due to nonuniform heat supply based on higher order shear deformation theory
    Transactions of the Japan Society of Mechanical Engineers. A, 1995
    Co-Authors: Yoshinobu Tanigawa, Kazuki Nagayama, Ryuusuke Kawamura
    Abstract:

    This paper is concerned with a theoretical treatment of thermal stress and thermal bending problems for a multi-layered anisotropic Laminated plate due to partially distributed heat supply. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal pile of layers having orthotropic material properties, i. e. an Angle-Ply Laminate. We obtain the three-dimensional temperature in a transient state and thermal deformation of a simply supported plate using the higher-order shear deformation theory. As an example, numerical calculations are carried out for a 2-layered Angle-Ply Laminate, and the numerical results are examined precisely.

  • analysis of thermal stress and deformation due to nonuniform heat supply in an angle ply Laminated rectangular plate
    Transactions of the Japan Society of Mechanical Engineers. A, 1995
    Co-Authors: Yoshinobu Tanigawa, Ryuusuke Kawamura, Tomohiro Takahara, Kazuki Nagayama
    Abstract:

    This paper describes theoretical treatment of problems of thermal stress and thermal bending due to partially distributed heat supply for a multilayered anisotropic Laminated plate. As an analytical model, we consider a Laminated rectangular plate consisting of a diagonal stack of layers having orthotropic material properties, i. e. an Angle-Ply Laminate. Introducing the Rayleigh-Ritz method based on the variational principle, a three-dimensional temperature solution for a transient state is given. Moreover, for the thermoelastic problems, the components of displacements are analyzed using the Rayleigh-Ritz method, and the characteristic behaviors of thermal stress and thermal deformation for a simply supported plate are determined. As an example, calculations are carried out for a 2-layered Angle-Ply Laminate, and the results are examined precisely.

Venu N Kumar - One of the best experts on this subject based on the ideXlab platform.

  • stiffness degradation resulting from 90 ply cracking in angle ply composite Laminates
    Composites Science and Technology, 1999
    Co-Authors: B. Pradhan, Venu N Kumar
    Abstract:

    Abstract Stiffness degradation resulting from 90° ply cracking in [±θn/90m]s Angle-Ply composite Laminates has been evaluated by a 3D finite-element method. A control volume having a single simulated transverse crack in 90° ply/plies and intact ±θ outer layers is used for the analysis. The stiffness degradation as a transverse crack extends in the width direction for glass/epoxy Angle-Ply Laminates is calculated for different crack lengths and different fibre orientation angles θ of the outer layers. Effects of the number of 90° layers and number of ±θ layers on the Laminate stiffness have also been studied. It has been observed that the available stiffness of the cracked Angle-Ply Laminate largely depends on the fibre orientation angle of the outer layers, the number of cracked cross-ply layers and the number of uncracked outer ±θ layers in the Laminate.

Arash Bahrami - One of the best experts on this subject based on the ideXlab platform.

  • Free-edge stresses in antisymmetric Angle-Ply Laminates in extension and torsion
    International Journal of Solids and Structures, 2006
    Co-Authors: Asghar Nosier, Arash Bahrami
    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 presented for different antisymmetric Angle-Ply Laminates under an axial force and a torque.

B. Pradhan - One of the best experts on this subject based on the ideXlab platform.

  • stiffness degradation resulting from 90 ply cracking in angle ply composite Laminates
    Composites Science and Technology, 1999
    Co-Authors: B. Pradhan, Venu N Kumar
    Abstract:

    Abstract Stiffness degradation resulting from 90° ply cracking in [±θn/90m]s Angle-Ply composite Laminates has been evaluated by a 3D finite-element method. A control volume having a single simulated transverse crack in 90° ply/plies and intact ±θ outer layers is used for the analysis. The stiffness degradation as a transverse crack extends in the width direction for glass/epoxy Angle-Ply Laminates is calculated for different crack lengths and different fibre orientation angles θ of the outer layers. Effects of the number of 90° layers and number of ±θ layers on the Laminate stiffness have also been studied. It has been observed that the available stiffness of the cracked Angle-Ply Laminate largely depends on the fibre orientation angle of the outer layers, the number of cracked cross-ply layers and the number of uncracked outer ±θ layers in the Laminate.

  • Stiffness degradation resulting from 90° ply cracking in Angle-Ply composite Laminates
    Composites Science and Technology, 1999
    Co-Authors: B. Pradhan, N Venu Kumar
    Abstract:

    Abstract Stiffness degradation resulting from 90° ply cracking in [±θn/90m]s Angle-Ply composite Laminates has been evaluated by a 3D finite-element method. A control volume having a single simulated transverse crack in 90° ply/plies and intact ±θ outer layers is used for the analysis. The stiffness degradation as a transverse crack extends in the width direction for glass/epoxy Angle-Ply Laminates is calculated for different crack lengths and different fibre orientation angles θ of the outer layers. Effects of the number of 90° layers and number of ±θ layers on the Laminate stiffness have also been studied. It has been observed that the available stiffness of the cracked Angle-Ply Laminate largely depends on the fibre orientation angle of the outer layers, the number of cracked cross-ply layers and the number of uncracked outer ±θ layers in the Laminate.