Free Vibration Study of Anti-Symmetric Angle-Ply Laminated Plates under Clamped Boundary Conditions

K.K. Viswanathan; K. Karthik; Y.V.S.S. Sanyasiraju; Z.A. Aziz

Curved and Layered Structures (2016)

  • Volume: 3, Issue: 1
  • ISSN: 2353-7396

Abstract

top
Two type of numerical approach namely, Radial Basis Function and Spline approximation, used to analyse the free vibration of anti-symmetric angle-ply laminated plates under clamped boundary conditions. The equations of motion are derived using YNS theory under first order shear deformation. By assuming the solution in separable form, coupled differential equations obtained in term of mid-plane displacement and rotational functions. The coupled differential is then approximated using Spline function and radial basis function to obtain the generalize eigenvalue problem and parametric studies are made to investigate the effect of aspect ratio, length-to-thickness ratio, number of layers, fibre orientation and material properties with respect to the frequency parameter. Some results are compared with the existing literature and other new results are given in tables and graphs.

How to cite

top

K.K. Viswanathan, et al. "Free Vibration Study of Anti-Symmetric Angle-Ply Laminated Plates under Clamped Boundary Conditions." Curved and Layered Structures 3.1 (2016): null. <http://eudml.org/doc/287117>.

@article{K2016,
abstract = {Two type of numerical approach namely, Radial Basis Function and Spline approximation, used to analyse the free vibration of anti-symmetric angle-ply laminated plates under clamped boundary conditions. The equations of motion are derived using YNS theory under first order shear deformation. By assuming the solution in separable form, coupled differential equations obtained in term of mid-plane displacement and rotational functions. The coupled differential is then approximated using Spline function and radial basis function to obtain the generalize eigenvalue problem and parametric studies are made to investigate the effect of aspect ratio, length-to-thickness ratio, number of layers, fibre orientation and material properties with respect to the frequency parameter. Some results are compared with the existing literature and other new results are given in tables and graphs.},
author = {K.K. Viswanathan, K. Karthik, Y.V.S.S. Sanyasiraju, Z.A. Aziz},
journal = {Curved and Layered Structures},
keywords = {Free vibration; laminated plate; antisymmetric; angle-ply; splines; radial basis function},
language = {eng},
number = {1},
pages = {null},
title = {Free Vibration Study of Anti-Symmetric Angle-Ply Laminated Plates under Clamped Boundary Conditions},
url = {http://eudml.org/doc/287117},
volume = {3},
year = {2016},
}

TY - JOUR
AU - K.K. Viswanathan
AU - K. Karthik
AU - Y.V.S.S. Sanyasiraju
AU - Z.A. Aziz
TI - Free Vibration Study of Anti-Symmetric Angle-Ply Laminated Plates under Clamped Boundary Conditions
JO - Curved and Layered Structures
PY - 2016
VL - 3
IS - 1
SP - null
AB - Two type of numerical approach namely, Radial Basis Function and Spline approximation, used to analyse the free vibration of anti-symmetric angle-ply laminated plates under clamped boundary conditions. The equations of motion are derived using YNS theory under first order shear deformation. By assuming the solution in separable form, coupled differential equations obtained in term of mid-plane displacement and rotational functions. The coupled differential is then approximated using Spline function and radial basis function to obtain the generalize eigenvalue problem and parametric studies are made to investigate the effect of aspect ratio, length-to-thickness ratio, number of layers, fibre orientation and material properties with respect to the frequency parameter. Some results are compared with the existing literature and other new results are given in tables and graphs.
LA - eng
KW - Free vibration; laminated plate; antisymmetric; angle-ply; splines; radial basis function
UR - http://eudml.org/doc/287117
ER -

NotesEmbed ?

top

You must be logged in to post comments.

To embed these notes on your page include the following JavaScript code on your page where you want the notes to appear.

Only the controls for the widget will be shown in your chosen language. Notes will be shown in their authored language.

Tells the widget how many notes to show per page. You can cycle through additional notes using the next and previous controls.

    
                

Note: Best practice suggests putting the JavaScript code just before the closing </body> tag.