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Finite Element Method
(FEM)
By,
Mr. M. Sasi Kumar
Assistant Professor
Department of Aeronautical Engineering
Kalaignarkarunanidhi Institute of Technology
08-11-2021 1
M.SASI KUMAR, AP/AERO
Syllabus
08-11-2021 2
M.SASI KUMAR, AP/AERO
Text Books & References
08-11-2021 3
M.SASI KUMAR, AP/AERO
Overview
• Objectives
• Methods of Engineering Analysis
• Methods under Numerical solutions
• What is FEM?
• Historical background
• General steps of the Finite Element Analysis
• Advantage, Disadvantage and Application of FEM/FEA
08-11-2021 4
M.SASI KUMAR, AP/AERO
Objectives
08-11-2021 5
M.SASI KUMAR, AP/AERO
Methods of Engineering analysis
Engineering analysis
Classical Methods Numerical methods
Experimental Analytical Energy
Boundary
Element
(BVM)
Finite
Difference
(FDM)
Finite
Element
(FEM)
08-11-2021 6
M.SASI KUMAR, AP/AERO
CONDITIONS EXPERIMENTAL ANALYTICAL NUMERICAL
Applicable
If physical prototype is
available
For simple problems like
cantilever, simply
supported beams, etc.
For Real life complex
problems
Result Accuracy
Cannot be believed blindly
and a minimum of 3 to 5
prototypes must be tested
100% Accurate results
Approximate but
acceptable solutions
Time consuming High High Low
Process cost
Expensive man power and
materials
Medium Low
Example
Strain gauge
measurements, Vibration
measurement, etc.
Theory of bending FEM, FDM, FVM, BEM
08-11-2021 7
M.SASI KUMAR, AP/AERO
Methods under Numerical solutions
1. Functional approximation :
• Rayleigh-Ritz methods (Variational approach) and Galerkin methods (Weighted
residual methods) are based on functional approximation but vary in their
procedure.
• Rayleigh-Ritz method is useful for solving complex structural problems.
• Weighted residual methods is useful for solving non-structural problems.
1. Functional approximation
2. Finite Difference Method (FDM)
3. Finite Element Method (FEM)
08-11-2021 8
M.SASI KUMAR, AP/AERO
2. Finite Difference Method:
• It is numerical method for solving differential equations by approximating
derivatives with finite differences.
• It is useful for solving heat transfer fluid mechanics and structural mechanic
problems.
• It is applicable to any phenomenon for which differential equation along with
the boundary conditions are available.
3. Finite Element Method (FEM) or Finite Element Analysis
(FEA):
• In finite element method, instead of solving the problem for the entire body,
in one operation, we formulate the equations for each finite element and
combine them into the solution of the whole body.
08-11-2021 9
M.SASI KUMAR, AP/AERO
What is FEM?
• The finite element method is the most widely used method for solving problems of
engineering and mathematical models.
• It is a numerical method used to calculate approximate solutions to differential equation.
• In this method, a body or a structure is subdivided into smaller elements of finite
dimensional called finite elements. Then the body is considered as an assemblage of these
elements connected at a finite number of joints called ‘Nodes’. The properties of each type of
finite element is obtained and assembled together and solved as a whole to get solution.
08-11-2021 10
M.SASI KUMAR, AP/AERO
• FEM can be applied to both Structural and Non Structural problems
1. Structural problems:
In this type, displacements at each nodal point is obtained. By using this
Stress and strain in each element can be calculated
2. Non structural problems:
In this type, temperature or fluid pressure at each nodal point is obtained.
By using these values, properties such as heat flow, fluid flow etc., for each element
Can be obtained.
08-11-2021 11
M.SASI KUMAR, AP/AERO
Historical background
• 1940 - Basic idea of FEA were developed by aircraft engineers.
They used matrix methods
• 1945 - Hrennikoff - Field of structural engineering
• 1947 - Levy - Introduce force method
• 1953 - Levy – Stiffness method for analysis aircraft
structures
• 1954 - Argyris & Kelsey – Matrix structural analysis
08-11-2021 12
M.SASI KUMAR, AP/AERO
• 1960 - Clough - Introduced the term ‘finite element’ in plane stress
analysis.
• 1961 - Turner - Large deflection and thermal analysis
problem.
• 1962 - Gallagher - Material non-linearity problems.
• 1968 - Zinkiewicz - Visco elasticity problems.
• 1969 - Szabo, Lee - Weighted Residual Method for structural analysis
08-11-2021 13
M.SASI KUMAR, AP/AERO
• 1970 - Zinkiewicz, Parekh - Weighted Residual method for transient
field problems.
• 1970s - Applications extended to shell
bending, plate bending, heat
transfer analysis, fluid flow
analysis, etc.
• 1967 - Zinkiewicz - First FEM book -
“The Finite Element Method”.
08-11-2021 14
M.SASI KUMAR, AP/AERO
General Steps of the FEM/FEA
• STEP 1 : Discretization of Structure
• STEP 2 : Numbering of Nodes & Elements
• STEP 3 : Selection of Displacement Function
• STEP 4 : Define the Material Behavior
• STEP 5 : Derivation of Element stiffness matrix
• STEP 6 : Derivation of Global stiffness matrix
• STEP 7 : Applying Boundary Condition
• STEP 8 : Solution for the unknown displacements
• STEP 9 : Computation of the element strains and stresses
• STEP 10: Interpret the Results
08-11-2021 15
M.SASI KUMAR, AP/AERO
STEP 1 : Discretization of Structure
08-11-2021 16
M.SASI KUMAR, AP/AERO
STEP 1 : Discretization of Structure
08-11-2021 17
M.SASI KUMAR, AP/AERO
STEP 2 : Numbering of Nodes & Elements
08-11-2021 18
M.SASI KUMAR, AP/AERO
STEP 3 : Selection of Displacement Function
08-11-2021 19
M.SASI KUMAR, AP/AERO
STEP 4 : Define the Material Behavior
08-11-2021 20
M.SASI KUMAR, AP/AERO
STEP 5 : Derivation of Element stiffness matrix
08-11-2021 21
M.SASI KUMAR, AP/AERO
STEP 6 : Derivation of Global stiffness matrix
08-11-2021 22
M.SASI KUMAR, AP/AERO
STEP 7 : Applying Boundary Condition
From the global stiffness matrix [K] is a singular matrix because its determinant is
Equal to zero. In order to remove this singularity problem, certain boundary
Conditions are applied.
STEP 8 : Solution for the unknown displacements
These equations can be solved and unknown displacements {u} are calculated
by using Gaussian Elimination method or Gauss Seidal method
08-11-2021 23
M.SASI KUMAR, AP/AERO
• From the solution of displacement vector {u}, stress and strain value can be calculated.
STEP 9 : Computation of the element strains and stresses
STEP 10: Interpret the Results
08-11-2021 24
M.SASI KUMAR, AP/AERO
Advantages of FEM :
• FEM can handle irregular geometry in a convenient manner.
• It handles general load conditions without difficulty.
• Non-homogeneous materials can be handled easily.
• All the various types of boundary conditions are handled.
• Higher order elements may be implemented.
08-11-2021 25
M.SASI KUMAR, AP/AERO
Disadvantages of FEM :
• It requires a digital computer and fairly extensive software.
• It requires longer execution time compared with finite difference
method.
• Output result will vary considerably, when the body is modeled
with fine mesh when compared to body modeled with course
mesh.
08-11-2021 26
M.SASI KUMAR, AP/AERO
Applications of FEM :
08-11-2021 27
M.SASI KUMAR, AP/AERO
08-11-2021 M.SASI KUMAR, AP/AERO 28
THANK YOU
08-11-2021 M.SASI KUMAR, AP/AERO 29

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Finite element method introduction

  • 1. Finite Element Method (FEM) By, Mr. M. Sasi Kumar Assistant Professor Department of Aeronautical Engineering Kalaignarkarunanidhi Institute of Technology 08-11-2021 1 M.SASI KUMAR, AP/AERO
  • 3. Text Books & References 08-11-2021 3 M.SASI KUMAR, AP/AERO
  • 4. Overview • Objectives • Methods of Engineering Analysis • Methods under Numerical solutions • What is FEM? • Historical background • General steps of the Finite Element Analysis • Advantage, Disadvantage and Application of FEM/FEA 08-11-2021 4 M.SASI KUMAR, AP/AERO
  • 6. Methods of Engineering analysis Engineering analysis Classical Methods Numerical methods Experimental Analytical Energy Boundary Element (BVM) Finite Difference (FDM) Finite Element (FEM) 08-11-2021 6 M.SASI KUMAR, AP/AERO
  • 7. CONDITIONS EXPERIMENTAL ANALYTICAL NUMERICAL Applicable If physical prototype is available For simple problems like cantilever, simply supported beams, etc. For Real life complex problems Result Accuracy Cannot be believed blindly and a minimum of 3 to 5 prototypes must be tested 100% Accurate results Approximate but acceptable solutions Time consuming High High Low Process cost Expensive man power and materials Medium Low Example Strain gauge measurements, Vibration measurement, etc. Theory of bending FEM, FDM, FVM, BEM 08-11-2021 7 M.SASI KUMAR, AP/AERO
  • 8. Methods under Numerical solutions 1. Functional approximation : • Rayleigh-Ritz methods (Variational approach) and Galerkin methods (Weighted residual methods) are based on functional approximation but vary in their procedure. • Rayleigh-Ritz method is useful for solving complex structural problems. • Weighted residual methods is useful for solving non-structural problems. 1. Functional approximation 2. Finite Difference Method (FDM) 3. Finite Element Method (FEM) 08-11-2021 8 M.SASI KUMAR, AP/AERO
  • 9. 2. Finite Difference Method: • It is numerical method for solving differential equations by approximating derivatives with finite differences. • It is useful for solving heat transfer fluid mechanics and structural mechanic problems. • It is applicable to any phenomenon for which differential equation along with the boundary conditions are available. 3. Finite Element Method (FEM) or Finite Element Analysis (FEA): • In finite element method, instead of solving the problem for the entire body, in one operation, we formulate the equations for each finite element and combine them into the solution of the whole body. 08-11-2021 9 M.SASI KUMAR, AP/AERO
  • 10. What is FEM? • The finite element method is the most widely used method for solving problems of engineering and mathematical models. • It is a numerical method used to calculate approximate solutions to differential equation. • In this method, a body or a structure is subdivided into smaller elements of finite dimensional called finite elements. Then the body is considered as an assemblage of these elements connected at a finite number of joints called ‘Nodes’. The properties of each type of finite element is obtained and assembled together and solved as a whole to get solution. 08-11-2021 10 M.SASI KUMAR, AP/AERO
  • 11. • FEM can be applied to both Structural and Non Structural problems 1. Structural problems: In this type, displacements at each nodal point is obtained. By using this Stress and strain in each element can be calculated 2. Non structural problems: In this type, temperature or fluid pressure at each nodal point is obtained. By using these values, properties such as heat flow, fluid flow etc., for each element Can be obtained. 08-11-2021 11 M.SASI KUMAR, AP/AERO
  • 12. Historical background • 1940 - Basic idea of FEA were developed by aircraft engineers. They used matrix methods • 1945 - Hrennikoff - Field of structural engineering • 1947 - Levy - Introduce force method • 1953 - Levy – Stiffness method for analysis aircraft structures • 1954 - Argyris & Kelsey – Matrix structural analysis 08-11-2021 12 M.SASI KUMAR, AP/AERO
  • 13. • 1960 - Clough - Introduced the term ‘finite element’ in plane stress analysis. • 1961 - Turner - Large deflection and thermal analysis problem. • 1962 - Gallagher - Material non-linearity problems. • 1968 - Zinkiewicz - Visco elasticity problems. • 1969 - Szabo, Lee - Weighted Residual Method for structural analysis 08-11-2021 13 M.SASI KUMAR, AP/AERO
  • 14. • 1970 - Zinkiewicz, Parekh - Weighted Residual method for transient field problems. • 1970s - Applications extended to shell bending, plate bending, heat transfer analysis, fluid flow analysis, etc. • 1967 - Zinkiewicz - First FEM book - “The Finite Element Method”. 08-11-2021 14 M.SASI KUMAR, AP/AERO
  • 15. General Steps of the FEM/FEA • STEP 1 : Discretization of Structure • STEP 2 : Numbering of Nodes & Elements • STEP 3 : Selection of Displacement Function • STEP 4 : Define the Material Behavior • STEP 5 : Derivation of Element stiffness matrix • STEP 6 : Derivation of Global stiffness matrix • STEP 7 : Applying Boundary Condition • STEP 8 : Solution for the unknown displacements • STEP 9 : Computation of the element strains and stresses • STEP 10: Interpret the Results 08-11-2021 15 M.SASI KUMAR, AP/AERO
  • 16. STEP 1 : Discretization of Structure 08-11-2021 16 M.SASI KUMAR, AP/AERO
  • 17. STEP 1 : Discretization of Structure 08-11-2021 17 M.SASI KUMAR, AP/AERO
  • 18. STEP 2 : Numbering of Nodes & Elements 08-11-2021 18 M.SASI KUMAR, AP/AERO
  • 19. STEP 3 : Selection of Displacement Function 08-11-2021 19 M.SASI KUMAR, AP/AERO
  • 20. STEP 4 : Define the Material Behavior 08-11-2021 20 M.SASI KUMAR, AP/AERO
  • 21. STEP 5 : Derivation of Element stiffness matrix 08-11-2021 21 M.SASI KUMAR, AP/AERO
  • 22. STEP 6 : Derivation of Global stiffness matrix 08-11-2021 22 M.SASI KUMAR, AP/AERO
  • 23. STEP 7 : Applying Boundary Condition From the global stiffness matrix [K] is a singular matrix because its determinant is Equal to zero. In order to remove this singularity problem, certain boundary Conditions are applied. STEP 8 : Solution for the unknown displacements These equations can be solved and unknown displacements {u} are calculated by using Gaussian Elimination method or Gauss Seidal method 08-11-2021 23 M.SASI KUMAR, AP/AERO
  • 24. • From the solution of displacement vector {u}, stress and strain value can be calculated. STEP 9 : Computation of the element strains and stresses STEP 10: Interpret the Results 08-11-2021 24 M.SASI KUMAR, AP/AERO
  • 25. Advantages of FEM : • FEM can handle irregular geometry in a convenient manner. • It handles general load conditions without difficulty. • Non-homogeneous materials can be handled easily. • All the various types of boundary conditions are handled. • Higher order elements may be implemented. 08-11-2021 25 M.SASI KUMAR, AP/AERO
  • 26. Disadvantages of FEM : • It requires a digital computer and fairly extensive software. • It requires longer execution time compared with finite difference method. • Output result will vary considerably, when the body is modeled with fine mesh when compared to body modeled with course mesh. 08-11-2021 26 M.SASI KUMAR, AP/AERO
  • 27. Applications of FEM : 08-11-2021 27 M.SASI KUMAR, AP/AERO
  • 29. THANK YOU 08-11-2021 M.SASI KUMAR, AP/AERO 29