me 475 computer aided design of structures finite element analysis of trusses – part 2

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ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part 2 Ron Averill Michigan State University

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ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part 2. Ron Averill Michigan State University. Learning Objectives. Describe why a truss element has multiple DOFs per node Develop the 2D vector transformation equations - PowerPoint PPT Presentation

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Page 1: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

ME 475Computer Aided Design of Structures

Finite Element Analysis of Trusses – Part 2

Ron AverillMichigan State University

Page 2: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Learning Objectives1. Describe why a truss element has multiple DOFs per node

2. Develop the 2D vector transformation equations

3. Use the 2D vector transformation equations to develop the finite element equations of a plane truss element

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Page 3: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Plane Truss Element DOFsThe nodes of a plane truss element can displace in both the x and y directions, even though each element elongates (strains) in only the local x-direction. The element rotation is a rigid body motion.

blue – undeformed

red – deformed

F3

Page 4: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Plane Truss Element DOFsIn order to describe the motion in two dimensions, we need two components of displacement, or two degrees of freedom (DOFs), per node.

We define two local DOFs at each node:

is the x-component of displacement at the ith node (i = 1,2)

is the y-component of displacement at the ith node (i = 1,2)

Similarly, there will be two components of force at each node.

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Page 5: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Plane Truss Elements – DOFs Plane truss elements have two DOFs per node:

Y x y

e 2

1 X

5

θ

Page 6: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Plane Truss Elements – Forces Plane truss elements have two internal force components per node:

Y x y

e 2

1 X

6

θ

Page 7: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Expanded Bar Finite Element EquationsTo accommodate the extra DOFs and forces, we expand the 1D bar finite element equations as follows:

Note the order of the local DOFs and forces. Displacements and forces at the same node are clustered together.

These equations are equivalent to the 1D bar equations, and they are still written with respect to local coordinates.

So we can express these equations as:

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Page 8: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Need for a Common Coordinate SystemTo simplify the enforcement of displacement continuity at nodes, we need to express all local DOFs in a common coordinate system. 1

1 Y 2 2 3

3 X8

The boolean array is:

45°

45°

Page 9: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Vector TransformationsOur common coordinate system will be the global XY system.

Y

y x

X

We can transform the nodal displacements as follows:

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θ

Page 10: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Vector TransformationsLet’s define and

Then we can write the transformation equations in matrix form as:

Inverting:

Note that transformations occur at a point – a node in this case. So we will apply these transformations at each node.

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Page 11: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Transformation of Planar Truss DOFsIn terms of the nodal DOFs, we have:

Or:

Where is called the transformation matrix.

Because is orthogonal, it has the special property:

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Page 12: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

Transformation of Planar Truss ForcesSimilarly for forces, we have:

Or:

Where is the same transformation matrix as before.

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Page 13: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Planar Truss FE EquationsRecall the expanded 4x4 system of bar equations from page 5:

Introducing the transformations just developed:

Premultiply both sides by

Simplifying:

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Page 14: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Planar Truss FE EquationsDefine:

So we have the final form:

These are the local (element level) finite element equations in terms of the global coordinate system. Just as before:

is the stiffness matrix of an element

is the element displacement vector

is the vector of internal element forces

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Page 15: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

2D Planar Truss FE EquationsWe can expand the equations

as:

These equations describe the behavior of an arbitrary 2D planar linear truss element in terms of the global coordinate system.

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Page 16: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

ExerciseDetermine the element stiffness matrix for each of the truss elements shown below.

2 3 Y 1 2

1 3 4 P = 10,000 lbs X

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45°45°

Elements 1 and 3 have length 10 ft. For all elements, E=30E6 psi and A = 2 in2.

The boolean array is:

Page 17: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

SolutionFirst we determine the orientation of each element, based on the direction of local x as defined in the boolean array.

2 3 Y 1 2

1 3 4 P = 10,000 lbs X

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45°45°

So the orientations are:

Element θ

1 90°

2 45°

3 0°

Page 18: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

SolutionIn general, recall that:

Element 1: E = 30E6 psi, A = 2 in2, h = 120 in, θ = 90°

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Page 19: ME 475 Computer Aided Design of Structures Finite Element Analysis of Trusses – Part  2

SolutionElement 2: E = 30E6 psi, A = 2 in2, h = 120 in, θ = 45°

Element 3: E = 30E6 psi, A = 2 in2, h = 120 in, θ = 0°

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