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2.8.08 INTRODUCTION
Chapter 1
INTRODUCTION
Zahit Mecitoğlu
FINITE ELEMENT ANALYSIS
IN STRUCTURES
© 2008 İstanbul Technical University
INTRODUCTION
2.8.08
WHAT IS FINITE ELEMENT
ANALYSIS?
„ Finite Element Analysis (FEA) is a method for numerical
solution of field problems.
Examples for field problems
The distribution of temperature in a turbine blade
The distribution of displacements and
stresses in an helicopter rotor blade.
„ A field problem is described by differential equations or
by an integral expression and either description may be
used to formulate finite elements.
INTRODUCTION
2.8.08
WHAT DOES “STRUCTURE” MEAN ?
„ Here the word “structures” implies any solids that are
subjected to loads or other influences.
„ Such influences cause deformations (or strains) through
out the continuum, accompanied by internal stresses
and reactions at restrained points.
„ The primary objectives of analysis by finite elements are
to calculate approximately the stresses and deflections
in a structure.
INTRODUCTION
2.8.08
HOW DOES THE FEM ORIJINATE ?
„ The finite element method is originally developed to
study the stresses in complex aircraft structures.
„ Then, it is applied to other fields of continuum
mechanics, such as heat transfer, fluid mechanics,
electromagnetics, geomechanics, biomechanics.
„ However, this course is devoted solely to the topic of
finite elements for the analysis of structures.
INTRODUCTION
2.8.08
WHY FEM IS NECESSARY ?
„ Analytical solutions to the engineering problems are
possible only if the geometry, loading and boundary
conditions of the problem are simple.
„ Otherwise it is necessary to use an approximate
numerical solution such as FEM.
INTRODUCTION
2.8.08
WHY FEA IS USED IN INDUSTRY?
„ To reduce the amount of prototype testing
Computer simulation allows multiple “what-if” scenarios to be
tested quickly and effectively.
„ To simulate designs that are not suitable for
prototype testing
Example: Surgical implants, such as an artificial knee
„ The bottom line:
Cost savings
Time savings… reduce time to market!
Create more reliable, better-quality designs
INTRODUCTION
2.8.08
APPLICATION AREAS
„ FEA software packages are used by engineers worldwide
in virtually all fields of engineering:
Structural
Thermal
Fluid (CFD, Acoustics, and other fluid analyses)
Low- and High-Frequency Electromagnetics
„ A partial list of industries in which FEA is used:
Aerospace
Automotive
Biomedical
Bridges & Buildings
Electronics & Appliances
Heavy Equipment & Machinery
MEMS
Sporting Goods
INTRODUCTION
2.8.08
DESIGN PROCESS AND FEA
Yes
No
Recognation of need
Definition of problem
Structural design
Analysis
Evaluation
Presentation
Experiment
Design modifications
Does design
satisfy all design
constraints
Determination of design
constraints problem
INTRODUCTION
2.8.08
EXPERIMENT OR ANALYSIS?
EXPERIMENT
„ Trial-error approach
„ Expensive for the large systems
„ Failure during the experiment may be dangerous
ANALYSIS
„ No need for actual structure
„ Assumptions and approximations affects adequacy of the results.
Analysis and experiment are dispensable in the design process.
INTRODUCTION
2.8.08
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Y
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EXPERIMENT AND ANALYSIS EXAMPLES
EXPERIMENTS
ANALYSES
INTRODUCTION
2.8.08
MODELING
„ An analysis method is applied to a model problem rather
than to an actual physical problem.
„ Even laboratory experiments use models unless the actual
physical structure is tested.
INTRODUCTION
2.8.08
...MODELING
aproximations
!
!
Engineering
problem
mathematical
model
solution
methods
results
Experimental
model
measurements
aproximations
!
aproximations
aproximations
!
INTRODUCTION
2.8.08
SOLUTION METHODS
Analytical Solution Methods
„ They provide closed form exact solutions
to the mathematical model of engineering problems.
„ They can be used only if the geometry, loading and
boundary conditions of the problem are simple.
INTRODUCTION
2.8.08
…SOLUTION METHODS
Approximate Solution Methods
„ They provide closed form approximate solutions to the
mathematical model of engineering problems.
„ They can be used only if the geometry, loading and
boundary conditions of the problem are simple.
INTRODUCTION
2.8.08
…SOLUTION METHODS
Numerical Solution Methods
„ They provide discrete form approximate solution to the
mathematical model of engineering problems.
„ They can be used to solve the problems with relatively
complex geometry, loading and boundary conditions.
In particular finite elements can represent structures of arbitrarily
complex geometry.
INTRODUCTION
2.8.08
...Example
Consider a beam with length L as shown in the Figure. The
modulus of elasticity of beam is E, and the moment of inertia
is I. When a vertical distributed load P is applied, the beam
deforms by w from the original horizontal line. Mathematical
model of the beam in differential equation form is
P
L EI
INTRODUCTION
2.8.08
Example
4
4
d w
EI P
dx
=
with the boundary conditions for the clamped end
0 at x = 0
dw
w
dx
= =
and for the free end
2 3
2 3
0 at x = L
d w d w
dx dx
= =
(1.1)
INTRODUCTION
2.8.08
...Example
We can express the Eq. (1.1) in variational form as follows
2
2
2
0 0
2
L L
EI d w
dx Pwdx
dx
⎛ ⎞
Π = −
⎜ ⎟
⎜ ⎟
⎝ ⎠
∫ ∫
Here P is the mechanical potential energy of the beam
with deflection w under applied distributed force P. A
solution of this problem statement can be obtained by
minimizing the potential energy.
INTRODUCTION
2.8.08
Solution
(i) Analytical Solution: Application of the integration
method to Eq. (1.1) as an analytical solution method.
3
1
3
2
2
1 2
2
1
1
2
d w
Px C
EI
dx
d w
Px C x C
EI
dx
= +
= + +
3 2
1 2 3
4 3 2
1 2 3 4
1
6
1
24
dw
Px C x C x C
dx EI
w Px C x C x C x C
EI
= + + +
= + + + +
INTRODUCTION
2.8.08
...Solution
The integration constants are obtained by applying the
B.C.’s and the exact solution is found as follows
( )
2
2 2
4 6
24
Px
w x Lx L
EI
= − − +
INTRODUCTION
2.8.08
...Solution
(ii) Approximate Solution: Application of the Ritz method
to Eq. (1.2) as a approximate solution method. A trial
function can be chosen as
2 2
1 2 3
( ) ( )
w x x a a x a x
= + + +L
If we take only two terms, and substitute the approximate
solution into the potential energy expression Eq. (1.2) we
obtain
( ) ( )
2 2 3
1 2 1 2
0 0
2 6
2
L L
EI
a a x dx P a x a x dx
Π = + − +
∫ ∫
INTRODUCTION
2.8.08
...Solution
The potential energy is minimized by equating to zero its
first derivatives with respect to unknown constants. After
performing the integrations, the following equations are
obtained.
2
1 2
1
2
1 2
2
0 2 3
6
0 2
24
PL
a La
a EI
PL
a La
a EI
∂Π
= ⇒ + =
∂
∂Π
= ⇒ + =
∂
INTRODUCTION
2.8.08
...Solution
Solving the equations, the constants are determined as
2 2
1 2
5
24 12
PL PL
a a
EI EIL
= = −
and the approximate solution is obtained as
( )
2 3
( ) 5 2
24
PL
w x x L x
EI
= − −
INTRODUCTION
2.8.08
...Solution
(iii) Numerical Solution: Application of the FEA as a
numerical solution method. We discretize the beam with
two beam elements, Fig. 1.5. The unknown nodal
parameters are the deflections and the slopes.
After the application of the FE procedure we reduce the
problem to the following linear algebraic equation system
θ2
w3
2
1
w1 w2
P
L/2 L/2
L
1
2
3
θ1
θ3
INTRODUCTION
2.8.08
...Solution
2
2 2
1
2 2
3
3
2 2
1 3
2
24 0 12 3 12
0 2 3 0
8
12 3 12 3 6
24
3 3
L w
L L L
EI PL
w
L L
L
L
L L L L
θ
θ
−
⎡ ⎤ ⎧ ⎫ ⎧ ⎫
⎢ ⎥ ⎪ ⎪ ⎪ ⎪
−
⎢ ⎥ ⎪ ⎪ ⎪ ⎪
=
⎨ ⎬ ⎨ ⎬
⎢ ⎥
− − − ⎪ ⎪ ⎪ ⎪
⎢ ⎥
⎪ ⎪ ⎪ ⎪
⎢ ⎥ −
⎩ ⎭
⎩ ⎭
−
⎣ ⎦
Then, the nodal displacement are obtained
2
3
2
3
3
0.044271
0.14583
0.125
1.666667
w L
PL
w L
EI
θ
θ
−
⎧ ⎫ ⎧ ⎫
⎪ ⎪ ⎪ ⎪
−
⎪ ⎪ ⎪ ⎪
=
⎨ ⎬ ⎨ ⎬
−
⎪ ⎪ ⎪ ⎪
⎪ ⎪ ⎪ ⎪
−
⎩ ⎭
⎩ ⎭
INTRODUCTION
2.8.08
...Solution
Solution Techniques w2 (PL4/EI) w3 (PL4/EI)
Analytical -0.044271 -0.125
Approximate -0.041667 -0.125
Numerical -0.044271 -0.125
INTRODUCTION
2.8.08
ADVANTAGES OF FEA
„ Versatility: FEA is applicable to any field problem, such as
heat transfer, stress analysis, magnetic fields and so on.
„ There is no geometric restriction (The body or region may
have any shape).
„ Boundary conditions and loading are not restricted
(boundary conditions and loads may be applied to any
portion)
INTRODUCTION
2.8.08
…ADVANTAGES OF FEA
„ Material properties may be change from one element to
another (even within an element) and the material
anisotropy is allowed)
„ Different elements (behavior and mathematical
descriptions) can be combined in a single FE model.
„ A FE structure closely resembles the actual body or region
to be analyzed.
„ The approximation is easily improved by grading the mesh
(mesh refinement)
INTRODUCTION
2.8.08
STEPS OF FEA
1. Learning about the problem
2. Modeling the problem
3. Preliminary Analysis
4. Discretizing the model
5. Formulating the solution
6. Obtaining Linear Algebraic Equations (LEAs)
7. Solving the equations
8. Checking the results
INTRODUCTION
2.8.08
1. Learning about the problem
It is important to understand the physics or nature of the problem and classify it.
PROBLEM IDENTIFICATION
„ What are the more important physical phenomena
involved?
„ Is the problem time-independent or time-dependent? (static
or dynamic?)
„ Is nonlinearity involved? (Is iterative solution necessary or
not?)
„ What results are sought from analysis?
„ What accuracy is required?
„ Is the problem interdisciplinary?
INTRODUCTION
2.8.08
…Learning about the problem
From answers
i) necessary information to carry out an analysis
ii) how the problem is modeled
iii) what method of solution is adopted
„ You must decide to do a nonlinear analysis if stresses are
high enough to produce yielding.
„ You must decide to perform a buckling analysis if the thin
sections carry compressive load.
INTRODUCTION
2.8.08
…Learning about the problem
Cautions:
„ Without this step a proper model cannot be devised.
„ At present, software does not automatically decide what
solution procedure must apply to the problem.
„ Software has limitations and almost contains errors.
„ Yet the engineer, not to software provider, is legally
responsible for results obtained.
INTRODUCTION
2.8.08
2. Modeling the problem
„ FEA is simulation, not reality.
„ FEA is also applied to the mathematical model.
„ If the model is inappropriate or inadequate,
even very accurate FEA may show
some disagreements with physical reality.
INTRODUCTION
2.8.08
...Modeling the problem
STEPS
„ Understand the physical nature of the problem.
„ Exclude superfluous detail but include all essential features.
(Unnecessary detail can be omitted)
„ Make necessary assumptions for geometry, material, and
loading. (i.e. fixed support, concentrated load, linear elastic
material assumptions)
„ Devise a model problem for the analysis.
„ Write down the differential equations and boundary
conditions, or integral statement.
INTRODUCTION
2.8.08
...Modeling the problem
MODEL SELECTION
„ What theory or mathematical formulation describes
behavior?
„ Depending on the dimensions, loading, and boundary
conditions of this idealization
we may decide that behavior is described by
beam theory
plate-bending theory
equations of plane elasticity
or some other analysis theory.
INTRODUCTION
2.8.08
...Modeling the problem
SELECTION FACTORS
Modeling decisions are influenced by
„ what information is sought
„ what accuracy is required
„ the anticipated expense of FEA
„ its capabilities and limitations.
INTRODUCTION
2.8.08
...Modeling the problem
Actual structure Finite Element Model, (Beam)
INTRODUCTION
2.8.08
3. Preliminary analysis
„ Before going from a mathematical model to FEA, at least
one preliminary solution should be obtained.
„ We may use whatever means are conveniently available.
simple analytical calculations,
handbook formulas,
trusted previous solutions,
or experiment.
„ Evaluation of the preliminary analysis results may require
a better mathematical model.
INTRODUCTION
2.8.08
4. Discretizating the model
„ A mathematical model is discretized by dividing it into a
mesh of finite elements.
„ Thus a fully continuous field is represented by a
piecewise continuous field.
„ A continuum problem is one with an infinite number of
unknowns.
„ The FE discretization procedures reduce the problem to
one of finite number of unknowns.
INTRODUCTION
2.8.08
...Discretizating the model
ERRORS
„ Discretization introduces another approximation. Relative to
reality, two sources of error have now been introduced:
§ modeling error
§ discretization error
„ To reduce the errors
improve model
use more elements
„ Numerical error is due to finite precision to represent data
and the results manipulation.
INTRODUCTION
2.8.08
...Discretizating the model
ELEMENTS AND NODES
By means of this method,
„ Solution region is divided into a finite number of
subregions (elements) of simple geometry
(triangles, rectangles …)
„ Key points are selected on the elements to serve as
nodes.
8-Node Hex 9-Node Pyramid 10-Node Tet
INTRODUCTION
2.8.08
...Discretizating the model
„ The nodes usually lie on the element boundaries,
„ Some elements have also a few interior nodes.
„ The nodes share values of the field quantity
„ They may also share its one or more derivatives.
„ The nodal values are called as the degrees of freedom
(d.o.f).
„ The nodes are also locations where loads are applied and
boundary conditions are imposed.
INTRODUCTION
2.8.08
...Discretizating the model
INTERPOLATION FUNCTIONS
„ The FEA is an approximation based on piecewise
interpolation of field quantity.
„ The interpolation functions approximate (represent) the
field variable in terms of the d.o.f. over a finite element.
„ In this way, the problem is stated in terms of these
nodal values as new unknowns.
INTRODUCTION
2.8.08
...Discretizating the model
„ Polynomials are usually chosen as interpolation functions
because differentiation and integration is easy with
polynomials.
„ The degree of polynomial depends on the number of
unknowns at each node and certain compatibility and
continuity requirements.
„ Often functions are chosen so that the field variable and its
derivatives are continuous across adjoining element
boundaries.
INTRODUCTION
2.8.08
5. Formulating the solution
„ Now, we can formulate the solution for individual
elements.
„ There are four different approaches to formulate the
properties of individual elements.
Direct approach
Variational approach
Weighted residuals approach
Energy balance approach
„ Stiffness and equivalent nodal loads for a typical
element are determined using the mentioned above.
INTRODUCTION
2.8.08
6-7. Obtaining LEAs and solution
„ The element properties are assembled to obtain the
system equations.
„ The equations are modified to account for the boundary
conditions of the problem.
„ The nodal displacements are obtained solving this
simultaneous linear algebraic equation system.
„ Support reactions are determined at restrained nodes.
INTRODUCTION
2.8.08
...Obtaining LEAs and solution
„ The strains and stresses are obtained from the element
formulations using the nodal displacements.
„ Once the nodal values (unknowns) are found, the
interpolation functions define the field variable through
the assemblage of elements.
„ The nature of solution and the degree of approximation
depend on the size and number of elements, and
interpolation functions.
INTRODUCTION
2.8.08
FINITE ELEMENT ANALYSIS
PREPROCESSING
NUMERICAL ANALYSIS
POSTPROCESSING
INTRODUCTION
2.8.08
PREPROCESSING
„ Input data describes geometry, material properties, loads,
and boundary conditions.
„ Software can automatically prepare much of the FE mesh,
but must be given direction as to the type of element and
mesh density desired.
„ Review the data for correctness before proceeding.
INTRODUCTION
2.8.08
Solid Model of a Tramcar
INTRODUCTION
2.8.08
Solid Model of a Bogie
INTRODUCTION
2.8.08
FE Model of the Tramcar
INTRODUCTION
2.8.08
FE Model of the Bogie
INTRODUCTION
2.8.08
FE Model of an Aircraft
INTRODUCTION
2.8.08
FE Model of a Wing
INTRODUCTION
2.8.08
Loading Scenarios
F = 300 KN F = 300 KN
F = 300 KN F = 300 KN
INTRODUCTION
2.8.08
NUMERICAL ANALYSIS
„ Software automatically generates matrices that describe
the behavior of each element,
„ and combines these matrices into a large matrix equation
that represents the FE structure,
„ solves this equation to determine values of field quantities
at nodes and additional calculations for nonlinear or time-
dependent behavior.
INTRODUCTION
2.8.08
POSTPROCESSING
The FEA solution and quantities derived from it are listed or
graphically displayed.
„ Deformed shape (with exaggeration)
„ Animation
„ Stress of various types on various planes.
INTRODUCTION
2.8.08
Deformed Shapes
INTRODUCTION
2.8.08
The von Mises Stresses on the Bogie
INTRODUCTION
2.8.08
Animation
INTRODUCTION
2.8.08
Animation
INTRODUCTION
2.8.08
CHECK RESULTS
Cautions:
„ Software has limitations and almost contains errors.
„ Yet the engineer, not to software provider, is legally
responsible for results obtained.
Examine results qualitatively
„ Are the boundary conditions applied correctly?
„ Are the symmetries seen on the results?
Compare FEA results with solutions from preliminary analysis and
with any other useful information that may be available.
INTRODUCTION
2.8.08
…CHECK RESULTS
Expect to revise:
Rarely is the first FE analysis satisfactory.
Obvious blunders must be corrected.
Either physical understanding or the FE model, or
both, may be at fault.
Disagreements must be satisfactorily resolved by
repair of the mathematical model and/or the FE
model.
INTRODUCTION
2.8.08
LEARNING AND USING FEA
Why study the theory of FEA?
An inept user can obtain result using a software.
However, reliable results are obtained only when the
analyst understand the problem,
how to model it
behavior of finite elements
assumptions and limitations built in the software
input data formats
and when the analyst checks for errors at all stages.
INTRODUCTION
2.8.08
…LEARNING AND USING FEA
It is not realistic to demand that analyst understand
details of all elements and procedures, but misuse of
FEA can be avoided only by those who understand
fundamentals.

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presentation1.pdf

  • 1. 2.8.08 INTRODUCTION Chapter 1 INTRODUCTION Zahit Mecitoğlu FINITE ELEMENT ANALYSIS IN STRUCTURES © 2008 İstanbul Technical University
  • 2. INTRODUCTION 2.8.08 WHAT IS FINITE ELEMENT ANALYSIS? „ Finite Element Analysis (FEA) is a method for numerical solution of field problems. Examples for field problems The distribution of temperature in a turbine blade The distribution of displacements and stresses in an helicopter rotor blade. „ A field problem is described by differential equations or by an integral expression and either description may be used to formulate finite elements.
  • 3. INTRODUCTION 2.8.08 WHAT DOES “STRUCTURE” MEAN ? „ Here the word “structures” implies any solids that are subjected to loads or other influences. „ Such influences cause deformations (or strains) through out the continuum, accompanied by internal stresses and reactions at restrained points. „ The primary objectives of analysis by finite elements are to calculate approximately the stresses and deflections in a structure.
  • 4. INTRODUCTION 2.8.08 HOW DOES THE FEM ORIJINATE ? „ The finite element method is originally developed to study the stresses in complex aircraft structures. „ Then, it is applied to other fields of continuum mechanics, such as heat transfer, fluid mechanics, electromagnetics, geomechanics, biomechanics. „ However, this course is devoted solely to the topic of finite elements for the analysis of structures.
  • 5. INTRODUCTION 2.8.08 WHY FEM IS NECESSARY ? „ Analytical solutions to the engineering problems are possible only if the geometry, loading and boundary conditions of the problem are simple. „ Otherwise it is necessary to use an approximate numerical solution such as FEM.
  • 6. INTRODUCTION 2.8.08 WHY FEA IS USED IN INDUSTRY? „ To reduce the amount of prototype testing Computer simulation allows multiple “what-if” scenarios to be tested quickly and effectively. „ To simulate designs that are not suitable for prototype testing Example: Surgical implants, such as an artificial knee „ The bottom line: Cost savings Time savings… reduce time to market! Create more reliable, better-quality designs
  • 7. INTRODUCTION 2.8.08 APPLICATION AREAS „ FEA software packages are used by engineers worldwide in virtually all fields of engineering: Structural Thermal Fluid (CFD, Acoustics, and other fluid analyses) Low- and High-Frequency Electromagnetics „ A partial list of industries in which FEA is used: Aerospace Automotive Biomedical Bridges & Buildings Electronics & Appliances Heavy Equipment & Machinery MEMS Sporting Goods
  • 8. INTRODUCTION 2.8.08 DESIGN PROCESS AND FEA Yes No Recognation of need Definition of problem Structural design Analysis Evaluation Presentation Experiment Design modifications Does design satisfy all design constraints Determination of design constraints problem
  • 9. INTRODUCTION 2.8.08 EXPERIMENT OR ANALYSIS? EXPERIMENT „ Trial-error approach „ Expensive for the large systems „ Failure during the experiment may be dangerous ANALYSIS „ No need for actual structure „ Assumptions and approximations affects adequacy of the results. Analysis and experiment are dispensable in the design process.
  • 10. INTRODUCTION 2.8.08 -4,00E +03 -3,00E +03 -2,00E +03 -1,00E +03 0,00E +00 1,00E +03 2,00E +03 3,00E +03 0,0 0,1 0,2 0,3 0,4 0,5 zaman, s μ s D E N E Y AN SYSSÖ N Ü M LÜ EXPERIMENT AND ANALYSIS EXAMPLES EXPERIMENTS ANALYSES
  • 11. INTRODUCTION 2.8.08 MODELING „ An analysis method is applied to a model problem rather than to an actual physical problem. „ Even laboratory experiments use models unless the actual physical structure is tested.
  • 13. INTRODUCTION 2.8.08 SOLUTION METHODS Analytical Solution Methods „ They provide closed form exact solutions to the mathematical model of engineering problems. „ They can be used only if the geometry, loading and boundary conditions of the problem are simple.
  • 14. INTRODUCTION 2.8.08 …SOLUTION METHODS Approximate Solution Methods „ They provide closed form approximate solutions to the mathematical model of engineering problems. „ They can be used only if the geometry, loading and boundary conditions of the problem are simple.
  • 15. INTRODUCTION 2.8.08 …SOLUTION METHODS Numerical Solution Methods „ They provide discrete form approximate solution to the mathematical model of engineering problems. „ They can be used to solve the problems with relatively complex geometry, loading and boundary conditions. In particular finite elements can represent structures of arbitrarily complex geometry.
  • 16. INTRODUCTION 2.8.08 ...Example Consider a beam with length L as shown in the Figure. The modulus of elasticity of beam is E, and the moment of inertia is I. When a vertical distributed load P is applied, the beam deforms by w from the original horizontal line. Mathematical model of the beam in differential equation form is P L EI
  • 17. INTRODUCTION 2.8.08 Example 4 4 d w EI P dx = with the boundary conditions for the clamped end 0 at x = 0 dw w dx = = and for the free end 2 3 2 3 0 at x = L d w d w dx dx = = (1.1)
  • 18. INTRODUCTION 2.8.08 ...Example We can express the Eq. (1.1) in variational form as follows 2 2 2 0 0 2 L L EI d w dx Pwdx dx ⎛ ⎞ Π = − ⎜ ⎟ ⎜ ⎟ ⎝ ⎠ ∫ ∫ Here P is the mechanical potential energy of the beam with deflection w under applied distributed force P. A solution of this problem statement can be obtained by minimizing the potential energy.
  • 19. INTRODUCTION 2.8.08 Solution (i) Analytical Solution: Application of the integration method to Eq. (1.1) as an analytical solution method. 3 1 3 2 2 1 2 2 1 1 2 d w Px C EI dx d w Px C x C EI dx = + = + + 3 2 1 2 3 4 3 2 1 2 3 4 1 6 1 24 dw Px C x C x C dx EI w Px C x C x C x C EI = + + + = + + + +
  • 20. INTRODUCTION 2.8.08 ...Solution The integration constants are obtained by applying the B.C.’s and the exact solution is found as follows ( ) 2 2 2 4 6 24 Px w x Lx L EI = − − +
  • 21. INTRODUCTION 2.8.08 ...Solution (ii) Approximate Solution: Application of the Ritz method to Eq. (1.2) as a approximate solution method. A trial function can be chosen as 2 2 1 2 3 ( ) ( ) w x x a a x a x = + + +L If we take only two terms, and substitute the approximate solution into the potential energy expression Eq. (1.2) we obtain ( ) ( ) 2 2 3 1 2 1 2 0 0 2 6 2 L L EI a a x dx P a x a x dx Π = + − + ∫ ∫
  • 22. INTRODUCTION 2.8.08 ...Solution The potential energy is minimized by equating to zero its first derivatives with respect to unknown constants. After performing the integrations, the following equations are obtained. 2 1 2 1 2 1 2 2 0 2 3 6 0 2 24 PL a La a EI PL a La a EI ∂Π = ⇒ + = ∂ ∂Π = ⇒ + = ∂
  • 23. INTRODUCTION 2.8.08 ...Solution Solving the equations, the constants are determined as 2 2 1 2 5 24 12 PL PL a a EI EIL = = − and the approximate solution is obtained as ( ) 2 3 ( ) 5 2 24 PL w x x L x EI = − −
  • 24. INTRODUCTION 2.8.08 ...Solution (iii) Numerical Solution: Application of the FEA as a numerical solution method. We discretize the beam with two beam elements, Fig. 1.5. The unknown nodal parameters are the deflections and the slopes. After the application of the FE procedure we reduce the problem to the following linear algebraic equation system θ2 w3 2 1 w1 w2 P L/2 L/2 L 1 2 3 θ1 θ3
  • 25. INTRODUCTION 2.8.08 ...Solution 2 2 2 1 2 2 3 3 2 2 1 3 2 24 0 12 3 12 0 2 3 0 8 12 3 12 3 6 24 3 3 L w L L L EI PL w L L L L L L L L θ θ − ⎡ ⎤ ⎧ ⎫ ⎧ ⎫ ⎢ ⎥ ⎪ ⎪ ⎪ ⎪ − ⎢ ⎥ ⎪ ⎪ ⎪ ⎪ = ⎨ ⎬ ⎨ ⎬ ⎢ ⎥ − − − ⎪ ⎪ ⎪ ⎪ ⎢ ⎥ ⎪ ⎪ ⎪ ⎪ ⎢ ⎥ − ⎩ ⎭ ⎩ ⎭ − ⎣ ⎦ Then, the nodal displacement are obtained 2 3 2 3 3 0.044271 0.14583 0.125 1.666667 w L PL w L EI θ θ − ⎧ ⎫ ⎧ ⎫ ⎪ ⎪ ⎪ ⎪ − ⎪ ⎪ ⎪ ⎪ = ⎨ ⎬ ⎨ ⎬ − ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ − ⎩ ⎭ ⎩ ⎭
  • 26. INTRODUCTION 2.8.08 ...Solution Solution Techniques w2 (PL4/EI) w3 (PL4/EI) Analytical -0.044271 -0.125 Approximate -0.041667 -0.125 Numerical -0.044271 -0.125
  • 27. INTRODUCTION 2.8.08 ADVANTAGES OF FEA „ Versatility: FEA is applicable to any field problem, such as heat transfer, stress analysis, magnetic fields and so on. „ There is no geometric restriction (The body or region may have any shape). „ Boundary conditions and loading are not restricted (boundary conditions and loads may be applied to any portion)
  • 28. INTRODUCTION 2.8.08 …ADVANTAGES OF FEA „ Material properties may be change from one element to another (even within an element) and the material anisotropy is allowed) „ Different elements (behavior and mathematical descriptions) can be combined in a single FE model. „ A FE structure closely resembles the actual body or region to be analyzed. „ The approximation is easily improved by grading the mesh (mesh refinement)
  • 29. INTRODUCTION 2.8.08 STEPS OF FEA 1. Learning about the problem 2. Modeling the problem 3. Preliminary Analysis 4. Discretizing the model 5. Formulating the solution 6. Obtaining Linear Algebraic Equations (LEAs) 7. Solving the equations 8. Checking the results
  • 30. INTRODUCTION 2.8.08 1. Learning about the problem It is important to understand the physics or nature of the problem and classify it. PROBLEM IDENTIFICATION „ What are the more important physical phenomena involved? „ Is the problem time-independent or time-dependent? (static or dynamic?) „ Is nonlinearity involved? (Is iterative solution necessary or not?) „ What results are sought from analysis? „ What accuracy is required? „ Is the problem interdisciplinary?
  • 31. INTRODUCTION 2.8.08 …Learning about the problem From answers i) necessary information to carry out an analysis ii) how the problem is modeled iii) what method of solution is adopted „ You must decide to do a nonlinear analysis if stresses are high enough to produce yielding. „ You must decide to perform a buckling analysis if the thin sections carry compressive load.
  • 32. INTRODUCTION 2.8.08 …Learning about the problem Cautions: „ Without this step a proper model cannot be devised. „ At present, software does not automatically decide what solution procedure must apply to the problem. „ Software has limitations and almost contains errors. „ Yet the engineer, not to software provider, is legally responsible for results obtained.
  • 33. INTRODUCTION 2.8.08 2. Modeling the problem „ FEA is simulation, not reality. „ FEA is also applied to the mathematical model. „ If the model is inappropriate or inadequate, even very accurate FEA may show some disagreements with physical reality.
  • 34. INTRODUCTION 2.8.08 ...Modeling the problem STEPS „ Understand the physical nature of the problem. „ Exclude superfluous detail but include all essential features. (Unnecessary detail can be omitted) „ Make necessary assumptions for geometry, material, and loading. (i.e. fixed support, concentrated load, linear elastic material assumptions) „ Devise a model problem for the analysis. „ Write down the differential equations and boundary conditions, or integral statement.
  • 35. INTRODUCTION 2.8.08 ...Modeling the problem MODEL SELECTION „ What theory or mathematical formulation describes behavior? „ Depending on the dimensions, loading, and boundary conditions of this idealization we may decide that behavior is described by beam theory plate-bending theory equations of plane elasticity or some other analysis theory.
  • 36. INTRODUCTION 2.8.08 ...Modeling the problem SELECTION FACTORS Modeling decisions are influenced by „ what information is sought „ what accuracy is required „ the anticipated expense of FEA „ its capabilities and limitations.
  • 37. INTRODUCTION 2.8.08 ...Modeling the problem Actual structure Finite Element Model, (Beam)
  • 38. INTRODUCTION 2.8.08 3. Preliminary analysis „ Before going from a mathematical model to FEA, at least one preliminary solution should be obtained. „ We may use whatever means are conveniently available. simple analytical calculations, handbook formulas, trusted previous solutions, or experiment. „ Evaluation of the preliminary analysis results may require a better mathematical model.
  • 39. INTRODUCTION 2.8.08 4. Discretizating the model „ A mathematical model is discretized by dividing it into a mesh of finite elements. „ Thus a fully continuous field is represented by a piecewise continuous field. „ A continuum problem is one with an infinite number of unknowns. „ The FE discretization procedures reduce the problem to one of finite number of unknowns.
  • 40. INTRODUCTION 2.8.08 ...Discretizating the model ERRORS „ Discretization introduces another approximation. Relative to reality, two sources of error have now been introduced: § modeling error § discretization error „ To reduce the errors improve model use more elements „ Numerical error is due to finite precision to represent data and the results manipulation.
  • 41. INTRODUCTION 2.8.08 ...Discretizating the model ELEMENTS AND NODES By means of this method, „ Solution region is divided into a finite number of subregions (elements) of simple geometry (triangles, rectangles …) „ Key points are selected on the elements to serve as nodes. 8-Node Hex 9-Node Pyramid 10-Node Tet
  • 42. INTRODUCTION 2.8.08 ...Discretizating the model „ The nodes usually lie on the element boundaries, „ Some elements have also a few interior nodes. „ The nodes share values of the field quantity „ They may also share its one or more derivatives. „ The nodal values are called as the degrees of freedom (d.o.f). „ The nodes are also locations where loads are applied and boundary conditions are imposed.
  • 43. INTRODUCTION 2.8.08 ...Discretizating the model INTERPOLATION FUNCTIONS „ The FEA is an approximation based on piecewise interpolation of field quantity. „ The interpolation functions approximate (represent) the field variable in terms of the d.o.f. over a finite element. „ In this way, the problem is stated in terms of these nodal values as new unknowns.
  • 44. INTRODUCTION 2.8.08 ...Discretizating the model „ Polynomials are usually chosen as interpolation functions because differentiation and integration is easy with polynomials. „ The degree of polynomial depends on the number of unknowns at each node and certain compatibility and continuity requirements. „ Often functions are chosen so that the field variable and its derivatives are continuous across adjoining element boundaries.
  • 45. INTRODUCTION 2.8.08 5. Formulating the solution „ Now, we can formulate the solution for individual elements. „ There are four different approaches to formulate the properties of individual elements. Direct approach Variational approach Weighted residuals approach Energy balance approach „ Stiffness and equivalent nodal loads for a typical element are determined using the mentioned above.
  • 46. INTRODUCTION 2.8.08 6-7. Obtaining LEAs and solution „ The element properties are assembled to obtain the system equations. „ The equations are modified to account for the boundary conditions of the problem. „ The nodal displacements are obtained solving this simultaneous linear algebraic equation system. „ Support reactions are determined at restrained nodes.
  • 47. INTRODUCTION 2.8.08 ...Obtaining LEAs and solution „ The strains and stresses are obtained from the element formulations using the nodal displacements. „ Once the nodal values (unknowns) are found, the interpolation functions define the field variable through the assemblage of elements. „ The nature of solution and the degree of approximation depend on the size and number of elements, and interpolation functions.
  • 49. INTRODUCTION 2.8.08 PREPROCESSING „ Input data describes geometry, material properties, loads, and boundary conditions. „ Software can automatically prepare much of the FE mesh, but must be given direction as to the type of element and mesh density desired. „ Review the data for correctness before proceeding.
  • 56. INTRODUCTION 2.8.08 Loading Scenarios F = 300 KN F = 300 KN F = 300 KN F = 300 KN
  • 57. INTRODUCTION 2.8.08 NUMERICAL ANALYSIS „ Software automatically generates matrices that describe the behavior of each element, „ and combines these matrices into a large matrix equation that represents the FE structure, „ solves this equation to determine values of field quantities at nodes and additional calculations for nonlinear or time- dependent behavior.
  • 58. INTRODUCTION 2.8.08 POSTPROCESSING The FEA solution and quantities derived from it are listed or graphically displayed. „ Deformed shape (with exaggeration) „ Animation „ Stress of various types on various planes.
  • 60. INTRODUCTION 2.8.08 The von Mises Stresses on the Bogie
  • 63. INTRODUCTION 2.8.08 CHECK RESULTS Cautions: „ Software has limitations and almost contains errors. „ Yet the engineer, not to software provider, is legally responsible for results obtained. Examine results qualitatively „ Are the boundary conditions applied correctly? „ Are the symmetries seen on the results? Compare FEA results with solutions from preliminary analysis and with any other useful information that may be available.
  • 64. INTRODUCTION 2.8.08 …CHECK RESULTS Expect to revise: Rarely is the first FE analysis satisfactory. Obvious blunders must be corrected. Either physical understanding or the FE model, or both, may be at fault. Disagreements must be satisfactorily resolved by repair of the mathematical model and/or the FE model.
  • 65. INTRODUCTION 2.8.08 LEARNING AND USING FEA Why study the theory of FEA? An inept user can obtain result using a software. However, reliable results are obtained only when the analyst understand the problem, how to model it behavior of finite elements assumptions and limitations built in the software input data formats and when the analyst checks for errors at all stages.
  • 66. INTRODUCTION 2.8.08 …LEARNING AND USING FEA It is not realistic to demand that analyst understand details of all elements and procedures, but misuse of FEA can be avoided only by those who understand fundamentals.