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# FEA Simulations PowerPoint PPT Presentation

FEA Simulations. Usually based on energy minimum or virtual work Component of interest is divided into small parts 1D elements for beam or truss structures 2D elements for plate or shell structures 3D elements for solids Boundary conditions are applied

FEA Simulations

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### FEA Simulations

• Usually based on energy minimum or virtual work

• Component of interest is divided into small parts

• 1D elements for beam or truss structures

• 2D elements for plate or shell structures

• 3D elements for solids

• Boundary conditions are applied

• Force or stress (i.e., pressure or shear)

• Displacement

• Multi-point constraints

### FEA Simulations (Contintued)

• Solution of governing equations

• Static: solution of simulataneous equations

• Vibrations: eigenvalue analysis

• Transient: Numerically step through time

• Nonlinear: includes buckling uses an iterative solution

• Evaluation of stress and strain

• Post-processing: e.g., contour or history plots

### Principal of Virtual Work

Change in energy for a “virtual” displacement, , in

the structure of volume, V , with surface, S, is

where

is the energy change

is the virtual displacement

is the internal stress

is the virtual strain due to

are the body forces (e.g., gravity, centrifugal)

are surface tractions(e.g., pressure, friction)

### Principal of Virtual Work (continued)

The principal of virtual work must hold for all possible

virtual displacements. We must convert at the nodes

to in the elements.

For example if we have a beam we can take

and

or

is the strain displacement matrix.

### Energy Minimization

Let where U is the internal energy and Vis

the potential energy due to the loads and are given by

and .

Recall then and

and the variation becomes

.

Since , and

,

is the same as virtual work.

### Finite Elements

• Assume displacements inside

an element is a linear (or quadratic)

function of the displacements of

the nodes of each element.

• Assume the function outside

each element is zero.

• Add the displacements of each

element to get the displacements

of all nodes.

For example:

For element 1:

For element 2:

Hence

### Interpolation Function

• Isoparametric elements have

same function displacements

as the coordinates

• Transform to an element with

coordinates at nodes

### Interpolation Function (continued)

• 2D isoparametric element

• 1D isoparametric element

• 3D isoparametric element in a similar manner

### Volume Integration

• For the parallelepiped the

the shaded area is

• The volume is

- i.e. a determinant

• For a rectangular

parallelepiped

• The volume is

### Volume Integration (continued)

• Using the isoparametric coordinates

• Use similar expressions for

• The volume becomes

• Numerical integration is more efficient if both the multiplying factor and the location of the integration points are specified by the integration rule.

• The rule for integration along x can be expanded to include y and z.

• For example, in one dimension, let

• Transform to isoparametric coordinates

and

### Gaussian Quadrature (continued)

• Then the integral becomes

• We can write the integral as

### Governing Equations

• Use virtual work or energy minimization

• Sum over each element since each element has no influence outside its boundary

• Let where is the vector of nodal displacements for element k

• Then the strains are

• Then

• Let

• And

• Hence

### Boundary Conditions

• Surface forces have been included

• So far the FE model is not restrained from rigid body motion

• Hence displacement boundary conditions are needed

• Recall

• Let the displacement constraints be

• Develop an augmented energy

### Boundary Conditions (continued)

• The energy minimum

### Summary

• The governing equations are based on virtual work or the minimization of energy.

• Displacement functions are zero outside elements.

• Isoparametric elements use the same function for the coordinates and displacements inside elements

• A Jacobian is required to complete integrations over the internal coordinates.

• Gaussian quadrature is typically used for integrations. Hence stresses and strains are calculated at integration points.

• Enforced displacements can be included through the use of Lagrange multipliers.