SimCafe

Space shortcuts

Child pages
  • ANSYS - Orthotropic plate with a hole - Problem Specification

Versions Compared

Old Version 24

changes.mady.by.user user-87699

Saved on

compared with

New Version Current

changes.mady.by.user user-0108f

Saved on

Key

  • This line was added.
  • This line was removed.
  • Formatting was changed.
Comment: Migrated to Confluence 5.3
Panel
Wiki Markup
{alias:plate2} {panel}

Author:

Oswaldo

Rodriguez,

Cornell

University {color:#cc0000}{*}Problem Specification{*}{color} [1. Create Command Log file|ANSYS - Orthotropic plate with a hole - Step 1] [2. Modify Log file - part1|ANSYS - Orthotropic plate with a hole - Step 2] [3. Modify Log file - part2|ANSYS - Orthotropic plate with a hole - Step 3] [4. Solve|ANSYS - Orthotropic plate with a hole - Step 4] [5. Postprocess the results|ANSYS - Orthotropic plate with a hole - Step 5] {panel} h2. Problem Specification Consider the square plate of uniform thickness with a circular hole with dimensions shown in the figure below. The plate is uniaxially loaded with a uniform pressure _p_=1 MPa. In addition, the plate is made of a Glass/Epoxy composite material with the fibers oriented in same direction as the applied load. The material properties are as follows: Young's modulus in the fiber direction Ex = 59.3 GPa Young's modulus in the transverse direction Ey = 22 GPa In-plane shear modulus Gxy = 8.96 GPa Major Poisson's ratio n{~}xy~ = 0.26 Minor Poisson's ratio n{~}yx~= 0.047 The circumferential stress concentration on the boundary of the hole is to be determined using ANSYS. !Composite_probspec.jpg! Go to [Step 1: Create Command Log file|ANSYS - Orthotropic plate with a hole - Step 1] Go to [all ANSYS Learning Modules|ANSYS Learning Modules]

University

Problem Specification
1. Create Command Log file
2. Modify Log file - part1
3. Modify Log file - part2
4. Solve
5. Postprocess the results

Problem Specification

Consider the square plate of uniform thickness with a circular hole with dimensions shown in the figure below. The plate is uniaxially loaded with a uniform pressure p=1 MPa. In addition, the plate is made of a Glass/Epoxy composite material with the fibers oriented in same direction as the applied load. The material properties are as follows:

Young's modulus in the fiber direction Ex = 59.3 GPa
Young's modulus in the transverse direction Ey = 22 GPa
In-plane shear modulus Gxy = 8.96 GPa
Major Poisson's ratio nxy = 0.26
Minor Poisson's ratio nyx= 0.047

The circumferential stress concentration on the boundary of the hole is to be determined using ANSYS.

Image Added

Go to Step 1: Create Command Log file

Go to all ANSYS Learning Modules