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1

Finite Element Method

FEM FOR PLATES &

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CONTENTS

 INTRODUCTION

 PLATE ELEMENTS

– Shape functions

– Element matrices

 SHELL ELEMENTS

– Elements in local coordinate system

– Elements in global coordinate system

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3

INTRODUCTION

 FE equations based on Mindlin plate theory will be developed.

 FE equations of shells will be formulated by

superimposing matrices of plates and those of 2D solids.

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PLATE ELEMENTS

 Geometrically similar to 2D plane stress solids except that it carries only transverse loads. Leads to bending.

2D equilvalent of the beam element.

 Rectangular plate elements based on Mindlin plate theory will be developed – conforming element.

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5

PLATE ELEMENTS

 Consider a plate structure:

x y

z, w

h

fz Middle plane

Middle plane

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PLATE ELEMENTS

 Mindlin plate theory:

( , , ) ( , )

In-plane strain:

Middle plane

χ (Curvature)

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7

PLATE ELEMENTS

Off-plane shear strain:

Potential (strain) energy:

z

In-plane stress & strain

Off-plane shear stress & strain

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PLATE ELEMENTS

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9

PLATE ELEMENTS

3 3

2 2

2

1 1

( )d ( )d

2 e 12 12 2 e

T

e x y

A A

h h

T

hw     A

d I d A

x

y w

 

          

d

3

3

0 0

0 0

12

0 0

12

h

h

h

 

 

 

 

  

 

 

 

 

I

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Shape functions

 Note that rotation is independent of deflection w

,

,

4

1 4

1 4

1

i y i i

y i

x i i

x i

i i

N N

w N

w

 

 

 

) 1

)( 1

(

4

1    

i i

i

N   

where (Same as rectangular

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11

Shape functions

h

displacement at node 1

displacement at node 2

displacement at node 3

displacement at node 4

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Element matrices

Substitute

h

x e

y

w

 

 

     

   

d Nd into

e e T

e e

T dm d

2 1

1

( )d

2 e

T e

A

T

d I d A

where T d

e

e

A A

m N I N

Recall that:

3

3

0 0

0 0

12

0 0

12

h

h

h

 

 

 

 

  

 

 

 

 

I

(Can be evaluated

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13

Element matrices

A

Substitute

h

d Nd into potential energy function

from which we obtain

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Element matrices

analytically but practically solved using Gauss

integration)

A

For uniformly distributed load,

1 0 0 1 0 0 1 0 0 1 0 0

z T

eabf

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15

SHELL ELEMENTS

 Loads in all directions

 Bending, twisting and in-plane deformation

 Combination of 2D solid elements (membrane effects) and plate elements (bending effect).

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Elements in local coordinate system

Consider a flat shell element

4 node

3 node

2 node

1 node

4

rotation about -axis rotation about -axis rotation about -axis

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17

Elements in local coordinate system

Membrane stiffness (2D solid element):

4 node

3 node

2 node

1 node node4

node3

node2

node1

Bending stiffness (plate element):

4 node

3 node

2 node

1 node node4

node3

node2

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Elements in local coordinate system

4 node

3 node

2 node

1 node

0 node

node

node

node

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19

Elements in local coordinate system

Membrane mass matrix (2D solid element):

13

Bending mass matrix (plate element):

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Elements in local coordinate system

4 node

3 node

2 node

1 node

0 node

node

node

node

Components related to the DOF z, are zeros in local coordinate system.

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21

Elements in global coordinate system

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Remarks

 The membrane effects are assumed to be

uncoupled with the bending effects in the element level.

This implies that the membrane forces will not

result in any bending deformation, and vice versa.

 For shell structure in space, membrane and

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23

CASE STUDY

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CASE

STUDY

Mode

Natural Frequencies (MHz)

768 triangular elements with

480 nodes

384 quadrilateral elements with

480 nodes

1280 quadrilateral elements with

1472 nodes

1 7.67 5.08 4.86

2 7.67 5.08 4.86

3 7.87 7.44 7.41

4 10.58 8.52 8.30

5 10.58 8.52 8.30

6 13.84 11.69 11.44

7 13.84 11.69 11.44

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25

CASE STUDY

Mode 1:

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CASE STUDY

Mode 3:

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27

CASE STUDY

Mode 5:

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CASE STUDY

Mode 7:

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29

CASE STUDY

 Transient analysis of micro-motor

F F F

x x

Node 210

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31

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