Authors :
Bertram, D. I.; Onwuka, D.O.; Ibearugbulem, O.M; Okere, C.E.
Volume/Issue :
Volume 9 - 2024, Issue 6 - June
Google Scholar :
https://tinyurl.com/4m9rtthb
Scribd :
https://tinyurl.com/bp5nw7v2
DOI :
https://doi.org/10.38124/ijisrt/IJISRT24JUN1201
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Abstract :
This work investigated the application of the
Alternative II refined plate theory in the analysis of an
anisotropic plate subjected to in-plane and lateral loads.
The kinematic equations developed from the Alternative
II Refined plate theory were used together with a
complete three-dimensional constitutive relation to obtain
the total potential energy of an anisotropic plate under
lateral and in-plane loads. General variation of the total
potential energy was done, a governing equation and two
compatibility equations were obtained. A polynomial
displacement function was obtained by solving the
governing and compatibility equations. This was used to
obtain peculiar displacement functions by satisfying the
boundary conditions of any plate. The stiffness
coefficients were obtained using the displacement
function. With the displacement functions and the
stiffness coefficients, the equations for the in-plane
normal and shear stresses as well as the transverse normal
and shear stresses were determined for any applied
lateral load when the applied in-plane load is a fraction of
the buckling load. Also, the equations for the
displacements of the plate were determined. Numerical
values of the stresses and displacement parameters were
determined for span to thickness ratios of 5, 10, 20 and
100 at angle of fiber orientations of 0 and aspect ratios of
1, 1.5 and 2.0 when the ratio of applied in-plane load to
buckling load are 0, 0.25 and 0.5. Using simple percentage
difference, the results from this work were compared with
the works of previous researchers.
Keywords :
Alternative II Theory, Anisotropic, In-plane and Lateral Loads, Rectangular Plate.
References :
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- Ibearugbulem O.M, Onwuegbuchulem U.C and Ibearugbulem C. N (2021). Analytical Three-Dimensional Bending Analyses of Simply Supported Thick Rectangular Plate. International Journal of Engineering Advanced Research (IJEAR) eISSN: 2710-7167 [Vol. 3 No. 1 March 2021] Journal website: http://myjms.mohe.gov.my/index.php/ijear.
- Ibearugbulem, O.M., Ezeh, J.C., Ettu, L.O, Gwarah, L.S. (2018). Bending Analysis of Rectangular Thick Plate Using Polynomial Shear Deformation Theory. IOSR Journal of Engineering (IOSRJEN) Vol. 08, Issue 9, ||V (III) || pp. 53-61
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- Sarvestani, H.Y, Naghashpour, A. and Heidari-Rarani, M., (2015). Bending analysis of a general cross-ply laminate using 3D elasticity solution and layer wise theory. Int J Adv Struct Eng, 7:329–340b DOI 10.1007/s40091-014-0073-2.
- Sayyad, A. S and Ghugal, Y. M. (2012). Bending and free vibration analysis of thick isotropic plates by using exponential shear deformation theory. Applied and Computational Mechanics 6, pp. 65–82
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This work investigated the application of the
Alternative II refined plate theory in the analysis of an
anisotropic plate subjected to in-plane and lateral loads.
The kinematic equations developed from the Alternative
II Refined plate theory were used together with a
complete three-dimensional constitutive relation to obtain
the total potential energy of an anisotropic plate under
lateral and in-plane loads. General variation of the total
potential energy was done, a governing equation and two
compatibility equations were obtained. A polynomial
displacement function was obtained by solving the
governing and compatibility equations. This was used to
obtain peculiar displacement functions by satisfying the
boundary conditions of any plate. The stiffness
coefficients were obtained using the displacement
function. With the displacement functions and the
stiffness coefficients, the equations for the in-plane
normal and shear stresses as well as the transverse normal
and shear stresses were determined for any applied
lateral load when the applied in-plane load is a fraction of
the buckling load. Also, the equations for the
displacements of the plate were determined. Numerical
values of the stresses and displacement parameters were
determined for span to thickness ratios of 5, 10, 20 and
100 at angle of fiber orientations of 0 and aspect ratios of
1, 1.5 and 2.0 when the ratio of applied in-plane load to
buckling load are 0, 0.25 and 0.5. Using simple percentage
difference, the results from this work were compared with
the works of previous researchers.
Keywords :
Alternative II Theory, Anisotropic, In-plane and Lateral Loads, Rectangular Plate.