- •Copyright Notice
- •Table of Contents
- •Chapter 1. Introduction
- •I. Basic Concepts
- •Examples:
- •Why Finite Element Method?
- •Applications of FEM in Engineering
- •Examples:
- •A Brief History of the FEM
- •FEM in Structural Analysis (The Procedure)
- •Example:
- •Available Commercial FEM Software Packages
- •Objectives of This FEM Course
- •II. Review of Matrix Algebra
- •Linear System of Algebraic Equations
- •Matrix Addition and Subtraction
- •Scalar Multiplication
- •Matrix Multiplication
- •Transpose of a Matrix
- •Symmetric Matrix
- •Unit (Identity) Matrix
- •Determinant of a Matrix
- •Singular Matrix
- •Matrix Inversion
- •Examples:
- •Solution Techniques for Linear Systems of Equations
- •Positive Definite Matrix
- •Differentiation and Integration of a Matrix
- •Types of Finite Elements
- •III. Spring Element
- •One Spring Element
- •Spring System
- •Checking the Results
- •Notes About the Spring Elements
- •Example 1.1
- •Chapter 2. Bar and Beam Elements
- •I. Linear Static Analysis
- •II. Bar Element
- •Stiffness Matrix --- Direct Method
- •Stiffness Matrix --- A Formal Approach
- •Example 2.1
- •Example 2.2
- •Distributed Load
- •Bar Elements in 2-D and 3-D Space
- •2-D Case
- •Transformation
- •Stiffness Matrix in the 2-D Space
- •Element Stress
- •Example 2.3
- •Example 2.4 (Multipoint Constraint)
- •3-D Case
- •III. Beam Element
- •Simple Plane Beam Element
- •Direct Method
- •Formal Approach
- •3-D Beam Element
- •Example 2.5
- •Equivalent Nodal Loads of Distributed Transverse Load
- •Example 2.6
- •Example 2.7
- •FE Analysis of Frame Structures
- •Example 2.8
- •Chapter 3. Two-Dimensional Problems
- •I. Review of the Basic Theory
- •Plane (2-D) Problems
- •Stress-Strain-Temperature (Constitutive) Relations
- •Strain and Displacement Relations
- •Equilibrium Equations
- •Exact Elasticity Solution
- •Example 3.1
- •II. Finite Elements for 2-D Problems
- •A General Formula for the Stiffness Matrix
- •Constant Strain Triangle (CST or T3)
- •Linear Strain Triangle (LST or T6)
- •Linear Quadrilateral Element (Q4)
- •Quadratic Quadrilateral Element (Q8)
- •Example 3.2
- •Transformation of Loads
- •Stress Calculation
- •I. Symmetry
- •Types of Symmetry:
- •Examples:
- •Applications of the symmetry properties:
- •Examples:
- •Cautions:
- •II. Substructures (Superelements)
- •Physical Meaning:
- •Mathematical Meaning:
- •Advantages of Using Substructures/Superelements:
- •Disadvantages:
- •III. Equation Solving
- •Direct Methods (Gauss Elimination):
- •Iterative Methods:
- •Gauss Elimination - Example:
- •Iterative Method - Example:
- •IV. Nature of Finite Element Solutions
- •Stiffening Effect:
- •V. Numerical Error
- •VI. Convergence of FE Solutions
- •Type of Refinements:
- •Examples:
- •VII. Adaptivity (h-, p-, and hp-Methods)
- •Error Indicators:
- •Examples:
- •Chapter 5. Plate and Shell Elements
- •Applications:
- •Forces and Moments Acting on the Plate:
- •Stresses:
- •Relations Between Forces and Stresses
- •Thin Plate Theory ( Kirchhoff Plate Theory)
- •Examples:
- •Under uniform load q
- •Thick Plate Theory (Mindlin Plate Theory)
- •II. Plate Elements
- •Kirchhoff Plate Elements:
- •Mindlin Plate Elements:
- •Discrete Kirchhoff Element:
- •Test Problem:
- •Mesh
- •III. Shells and Shell Elements
- •Example: A Cylindrical Container.
- •Shell Theory:
- •Shell Elements:
- •Curved shell elements:
- •Test Cases:
- •Chapter 6. Solid Elements for 3-D Problems
- •I. 3-D Elasticity Theory
- •Stress State:
- •Strains:
- •Stress-strain relation:
- •Displacement:
- •Strain-Displacement Relation:
- •Equilibrium Equations:
- •Stress Analysis:
- •II. Finite Element Formulation
- •Displacement Field:
- •Stiffness Matrix:
- •III. Typical 3-D Solid Elements
- •Tetrahedron:
- •Hexahedron (brick):
- •Penta:
- •Element Formulation:
- •Solids of Revolution (Axisymmetric Solids)
- •Axisymmetric Elements
- •Applications
- •Chapter 7. Structural Vibration and Dynamics
- •I. Basic Equations
- •A. Single DOF System
- •B. Multiple DOF System
- •Example
- •II. Free Vibration
- •III. Damping
- •IV. Modal Equations
- •V. Frequency Response Analysis
- •VI. Transient Response Analysis
- •B. Modal Method
- •Cautions in Dynamic Analysis
- •Examples
- •Chapter 8. Thermal Analysis
- •Further Reading
Lecture Notes: Introduction to Finite Element Method |
Chapter 2. Bar and Beam Elements |
Equivalent Nodal Loads of Distributed Transverse Load
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q |
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x L |
j |
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qL/2 |
qL/2 |
qL2/12 |
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qL2/12 |
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This can be verified by considering the work done by the distributed load q.
q
L L
qL qL/2
qL2/12
L L
© 1997-2002 Yijun Liu, University of Cincinnati |
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Lecture Notes: Introduction to Finite Element Method |
Chapter 2. Bar and Beam Elements |
Example 2.6
y |
p |
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E,I |
2 |
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L |
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Given: A cantilever beam with distributed lateral load p as shown above.
Find: The deflection and rotation at the right end, the reaction force and moment at the left end.
Solution: The work-equivalent nodal loads are shown below,
y |
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f |
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m |
1 |
E,I |
2 |
x |
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L |
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where
f = pL / 2, |
m = pL2 / 12 |
Applying the FE equation, we have
© 1997-2002 Yijun Liu, University of Cincinnati |
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Lecture Notes: Introduction to Finite Element Method Chapter 2. Bar and Beam Elements
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12 |
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6L −12 6L v1 |
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F1Y |
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EI |
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6L |
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4L |
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−6L |
2L |
θ1 = |
M1 |
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L3 |
−12 |
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−6L 12 −6L v2 |
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F2Y |
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6L |
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−6L |
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2L |
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4L |
θ |
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Load and constraints (BC’s) are, |
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F2Y = − f , |
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M2 = m |
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v1 =θ1 = 0 |
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Reduced equation is, |
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EI |
12 |
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−6L v2 |
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− f |
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L3 |
−6L |
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4L2 θ |
= m |
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Solving this, we obtain, |
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v2 |
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= |
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−2L2 f |
+ |
3Lm |
− pL4 |
/ 8EI |
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−3Lf |
+ |
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= |
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(A) |
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θ2 |
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6EI |
6m |
− pL3 |
/ 6EI |
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These nodal values are the same as the exact solution. Note that the deflection v(x) (for 0 < x< 0) in the beam by the FEM is, however, different from that by the exact solution. The exact solution by the simple beam theory is a 4th order polynomial of x, while the FE solution of v is only a 3rd order polynomial of x.
If the equivalent moment m is ignored, we have,
v2 |
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= |
L |
−2L2 |
f |
− pL4 |
/ 6EI |
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−3Lf |
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= |
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θ2 |
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6EI |
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− pL3 |
/ 4EI |
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The errors in (B) will decrease if more elements are used. The
© 1997-2002 Yijun Liu, University of Cincinnati |
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Lecture Notes: Introduction to Finite Element Method |
Chapter 2. Bar and Beam Elements |
equivalent moment m is often ignored in the FEM applications. The FE solutions still converge as more elements are applied.
From the FE equation, we can calculate the reaction force and moment as,
F1Y |
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= |
L3 −12 |
6L v2 |
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pL / 2 |
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M |
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−6L 2L2 θ |
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= 5pL2 / 12 |
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1 |
EI |
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2 |
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where the result in (A) is used. This force vector gives the total effective nodal forces which include the equivalent nodal forces for the distributed lateral load p given by,
− pL / 2− pL2 / 12
The correct reaction forces can be obtained as follows,
F |
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pL |
/ 2 |
− pL / 2 |
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pL |
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1Y |
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= |
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− |
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= |
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M1 |
5pL2 |
/ 12 |
− pL2 / 12 |
pL2 |
/ 2 |
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Check the results!
© 1997-2002 Yijun Liu, University of Cincinnati |
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