Title: ECIV 720 A Advanced Structural Mechanics and Analysis
1ECIV 720 A Advanced Structural Mechanics and
Analysis
- Lecture 12
- Isoparametric CST
- Area Coordinates
- Shape Functions
- Strain-Displacement Matrix
- Rayleigh-Ritz Formulation
- Galerkin Formulation
2FEM Solution Area Triangulation
Area is Discretized into Triangular Shapes
3FEM Solution Area Triangulation
One Source of Approximation
4FEM Solution Nodes and Elements
Points where corners of triangles meet Define
NODES
5Non-Acceptable Triangulation
Nodes should be defined on corners of ALL
adjacent triangles
6FEM Solution Nodes and Elements
7FEM Solution Objective
- Use Finite Elements to Compute Approximate
Solution At Nodes
- Interpolate u and v at any point from Nodal
values q1,q2,q6
8Intrinsic Coordinate System
2 (0,1)
3 (0,0)
1 (1,0)
Parent
9Area Coordinates
Location of P can be defined uniquely
Area Coordinates
10Area Coordinates and Shape Functions
Area Coordinates are linear functions of x and h
Are equal to 1 at nodes they correspond to
Are equal to 0 at all other nodes
Natural Choice for Shape Functions
11Shape Functions
12Geometry from Nodal Values
13Intrinsic Coordinate System
14Displacement Field from Nodal Values
15Strain Tensor from Nodal Values of Displacements
Need Derivatives
Strain Tensor
u and v functions of x and h
16Jacobian of Transformation
J
Jacobian of Transformation
J
17Jacobian of Transformation Physical Significance
18Jacobian of Transformation Physical Significance
19Jacobian of Transformation Physical Significance
20Jacobian of Transformation
21Strain Tensor from Nodal Values of Displacements
22Strain Tensor from Nodal Values of Displacements
23Strain Tensor from Nodal Values of Displacements
e B q
Looks Familiar?
24Strain-Displacement Matrix
Is constant within each element - CST
25Stresses
e B q
26Element Stiffness Matrix ke
e B q
s D B qe
ke
27Formulation of Stiffness Equations
t
Assume Plane Stress
28Total Potential Approach
Total Potential
29Total Potential Approach
30Total Potential Approach
31Total Potential Approach
Work Potential of Body Forces
32WP of Body Forces
33WP of Body Forces
34WP of Body Forces
35WP of Body Forces
36Total Potential Approach
Work Potential of Tractions
37WP of Traction
Distributed Load acting on EDGE of element
38WP of Traction
39WP of Traction
Components
40WP of Traction
41WP of Traction
2
3
1
42WP of Traction
43Total Potential Approach
Work Potential of Concentrated Loads
44WP of Concentrated Loads
Indicates that at location of point loads a node
must be defined
45In Summary
46After Superposition
Minimizing wrt Q
47Galerkin Approach
Galerkin
48Galerkin Approach
49Galerkin Approach
Introduce Virtual Displacement Field f
50Galerkin Approach
51Element Stiffness Matrix ke
52Galerkin Approach
Virtual Work Potential of Body Forces
53dWP of Body Forces
As we have already seen
54dWP of Body Forces
55Galerkin Approach
Virtual Work Potential of Traction
56dWP of Traction
57dWP of Traction
58Galerkin Approach
Virtual Work Potential of Point Loads
59dWP of Concentrated Loads
Indicates that at location of point loads a node
must be defined
60In Summary
61After Superposition
Y is arbitrary and thus
62Stress Calculations
ee Be qe
63Stress Calculations
Constant
64Summary of Procedure
Tt (force/length)
Nodes should be placed at
65Summary of Procedure
For Every Element Compute
- Strain-Displacement Matrix B
66Summary of Procedure
67Summary of Procedure
- Node Equivalent Traction Vector
For ALL loaded sides
68Summary of Procedure
Collect ALL Point Loads in Nodal Load Vector
69Summary of Procedure
Form Stiffness Equations
70Summary of Procedure
Apply Boundary Conditions
For Every Element Compute Stress
71Example
Tt200 lb/in
(0,2)
(3,2)
fx0
fy60 lb/in2
(0,0)
(3,0)
72ANSYS Solution Coarse Mesh
73(No Transcript)
74(No Transcript)
75(No Transcript)
76(No Transcript)
77(No Transcript)
78(No Transcript)
79(No Transcript)
802-D Constant Stress Triangle
Comments
- First Element for Stress Analysis
- Does not work very well
- When in Bending under-predicts displacements
- Slow convergence for fine mesh
- For in plane strain conditions Mesh Locks
- No Deformations
81Element Defects
82Element Defects
Constant Stress Triangles
Y-Deflection X-Stress about ¼ of actual
83Element Defects
x10, y10 x2a, y20 x30, y3a
?
Spurious Shear Strain Absorbs Energy Larger
Force Required
84Element Defects
Rubber Like Material n0.5
Mesh Lock