introduction to finite element method - faculty...
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Introduction to
Finite Element Method
Wong Foek Tjong, Ph.D.
Petra Christian University
Surabaya
Guest Lecture in Prodi Teknik Sipil
2 2014/6/7
Lecture Outline
1. Overview of the FEM
2. Computational steps of the FEM
3. Learning the direct stiffness method using ta29.petra.ac.id
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Behavior of a
Real Structure
Experiment
Replicate conditions of the
structure (possibly on a
smaller scale) and observe
the behavior of the model
Simulation
Simplifications and
assumptions of the
real structure
Mathematical
Model Physical
Model
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An example of the FEM
applications
Real experiment FE simulation It is often expensive or
dangerous
It replicates conditions of
the real experiment
Source: W.J. Barry (2003), “FEM Lecture Slides”, AIT Thailand
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Mathematical
Models
Analytical Solution
Techniques
Numerical Solution
Techniques
Closed-form
Solutions
Only possible for
simple geometries and
boundary conditions
•Finite difference methods
•Finite element methods
•Boundary element methods
•Mesh-free methods
•etc.
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It is a computational technique used to obtain approximate solutions of engineering problems.
The results are generally not exact.
However, the accuracy of the results can be improved either using finer mesh (h-refinement) or higher degree elements (p-refinement)
What is FEM?
Solution refinements in FEM
h-refinement
h=1/4
h=1/2
h=1
Solution refinements in FEM
(cont’d)
p-refinement
h=1 h=1/2 u=a+bx+cy+
dx 2+exy+fy 2
u=a+bx+cy
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In the context of structural analyzes, it may be regarded as a generalized matrix method of structural analysis.
It is originated as a method of structural analysis but is now widely used in various disciplines such as heat transfer, fluid flow, seepage, electricity and magnetism, and others.
Finite element method (1)
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Modern FEM were first developed and applied by
aeronautical engineers, i.e. M.J. Turner et al., at Boeing
company in the period 1950s.
1956: The first engineering FEM paper
Finite element method (2)
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The name “finite element method” was
coined by R.W. Clough in 1960. It is
called “finite” in order to distinguish with
“infinitesimal element” in Calculus.
1967: First FEM book by O.C.
Zienkiewicz
Finite element method (3)
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For General purposes:
NASTRAN, ANSYS, ADINA, ABAQUS, etc.
For structural analysis, particularly in Civil Engineering:
SANS, SAP2000, STAAD, GT STRUDL, MIDAS, DIANA, STRAND 7, etc.
For building structures:
ETABS, BATS etc.
Examples of FEM software
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Example of applications in
structural engineering
Source: MidasGen project apllications
http://en.midasuser.com/products/gallery.asp
Beijing National Stadium in China
(Bird’s Nest Stadium)
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Example of applications in
structural engineering (cont’d)
Source: http://gid.cimne.upc.es/gidinpractice/gp01.html
The structural analysis
of an F-16 aircraft The analysis of the Cathedral of
Barcelona using 3D solid elements.
(courtesy of Barcelona Cathedral)
Simulation of Wave Propagation
Passing a Solid Barrier
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Source: G. B. Wijaya (2005), a Petra-AIT Thesis
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Lecture Outline
1. Overview of the FEM
2. Computational steps of the FEM
3. Learning the direct stiffness method using ta29.petra.ac.id
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Fundamental concept is discretization, i.e.
dividing a continuum (continuous body,
structural system) into a finite number of smaller
and simple elements whose union approximates
the geometry of the continuum.
Discretization
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Some basic element shapes
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Examples of discretization (3)
Cooling Tower– Nuclear Power Plant (taken from a FEM Course Project of Doddy and Andre, Dec 2008)
150 m
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Structural Model and Its Example
of the Analysis Results
The structure is divided into smaller parts called “element”
Membrane force contour in the circumferential direction
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The FE Model with
a Finer Mesh
The structure is modeled with a finer mesh
The result is now better
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Discretize the structure (problem domain)
Divide the structure or continuum into finite elements
Once the structure has been discretized, the
computational steps faithfully follow the steps in the
direct stiffness method.
The direct stiffness method:
The global stiffness matrix of the discrete structure are obtained
by superimposing (assembling) the stiffness matrices of the
element in a direct manner.
Computational steps of the FEM-
the direct stiffness method
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Generate element stiffness matrix and element
force matrix for each element.
Assemble the element matrices to obtain the
global stiffness equation of the structure.
Apply the known nodal loads.
Specify how the structure is supported:
Set several nodal displacements to known values.
Computational steps… (cont’d)
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Solve simultaneous linear algebraic
equation.
The nodal parameters (displacements)
are obtained.
Calculate element stresses or stress
resultants (internal forces).
General steps of the FEM (cont’d)
x2
D1
D2
D3
CONTINUOUS MODEL
DISCRETE MODEL
p1
p2
p3 Joint
= Free DOF
{D} = Joint Degree-of-freedom
= Locked DOF
Discretization of Plane Frame Structures
D4
D5
D6
D7
D8
D9
D10
D11
D12
Source: ACECOMS, AIT-Thailand
Plane Frame Element
The stiffness equation for the plane frame
element can be obtained by superposing
the bar and beam equations.
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1
2
3
4
5
6
x
y
z Local
coordinate
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1
2
3
4
5
6
The discretized equation:
kd=f
𝐝 =
𝑑1
𝑑2
𝑑3
𝑑4
𝑑5
𝑑6
=
𝑢1
𝑣1
𝜃1𝑢2
𝑣2
𝜃2
; 𝐟 =
𝑓1
𝑓2
𝑓3
𝑓4
𝑓5
𝑓6
=
𝑁1
𝑉1
𝑀1
𝑁2
𝑉2
𝑀2
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1
2
3
4
5
6
The stiffness matrix:
𝐶1 =𝐸𝐴
𝐿 ; 𝐶𝟐 =
𝐸𝐼𝑧
𝐿3 (1+𝜑𝑦) ; 𝜑𝑦 =
12𝐸𝐼𝑧
𝐴s𝐺𝐿2
𝐤 =
𝐶1 0 0 −𝐶1 0 00 12𝐶2 6𝐶2𝐿 0 −12𝐶2 6𝐶2𝐿
0 6𝐶2𝐿 (4 + 𝜑)𝐶2𝐿2 0 −6𝐶2𝐿 2 − 𝜑 𝐶2𝐿2
−𝐶1 0 0 𝐶1 0 00 −12𝐶2 −6𝐶2𝐿 0 12𝐶2 −6𝐶2𝐿
0 6𝐶2𝐿 (2 − 𝜑)𝐶2𝐿2 0 −6𝐶2𝐿 (4 + 𝜑)𝐶2𝐿2
1
2
3
4
5
6
7
8
9 10
11
12
=
1 2 3 4 5 6 7 8
9 10 11 12
Source: ACECOMS, AIT-Thailand
1
2
3
4
5
6
7
8
9 10
11
12
=
1 2 3 4 5 6 7 8
9 10 11 12
Source: ACECOMS, AIT-Thailand
1
2
3
4
5
6
7
8
9 10
11
12
=
1 2 3 4 5 6 7 8
9 10 11 12
Source: ACECOMS, AIT-Thailand
1
2
3
4
5
6
7
8
9 10
11
12
=
1 2 3 4 5 6 7 8
9 10 11 12
Source: ACECOMS, AIT-Thailand
1
2
3
4
5
6
7
8
9 10
11
12
r2 = r2
=
1 2 3 4 5 6 7 8
9 10 11 12
-
1
2
3
4
5
6
7
8
9 10
11
12
r2 = r2
=
1 2 3 4 5 6 7 8
9 10 11 12
-
Final System
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Lecture Outline
1. Overview of the FEM
2. Computational steps of the FEM
3. Learning the direct stiffness method using ta29.petra.ac.id
Example (SAP2000 Verification
Manual, 2007)
Find the internal forces, support reactions and the
deflection at the middle of the beam (node 5)
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