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Government Engineering College, Bhavnagar.
Civil Engineering Department
METHODS TO SOLVE INDETERMINATE PROBLEM
2
Displacement methods
Force method
Small degree
of statical
indeterminacy
Large degree
of statical
indeterminacy
Displacement method
in matrix formulation
Numerical methods
Disadvantages:
• bulky calculations (not for hand calculations);
• structural members should have some certain
number of unknown nodal forces and nodal
displacements; for complex members such as curved
beams and arbitrary solids this requires some
discretization, so no analytical solution is possible.
ADVANTAGES AND DISADVANTAGES OF MATRIX
METHODS
3
Advantages:
• very formalized and computer-friendly;
• versatile, suitable for large problems;
• applicable for both statically determinate and
indeterminate problems.
FLOWCHART OF MATRIX METHOD
4
Classification
of members
Stiffness matrices
for members
Transformed
stiffness matrices
Stiffness matrices are
composed according to
member models
Stiffness matrices are
transformed from local to global
coordinates
Final equation
F = K · Z
Stress-strain state
of structure
Unknown displacements and
reaction forces are calculated
Stiffness matrices of separate
members are assembled into a
single stiffness matrix K
STIFFNESS MATRIX OF STRUCTURAL MEMBER
5
Stiffness matrix (K) gives the relation between vectors
of nodal forces (F) and nodal displacements (Z):
EXAMPLE OF MEMBER STIFFNESS MATRIX
6
Stiffness relation for a rod:
Stiffness matrix:
( )i j i
EA
F x x
L
= − ⋅ −
ASSEMBLY OF STIFFNESS MATRICES
7
To assemble stiffness matrices of separate members
into a single matrix for the whole structure, we should
simply add terms for corresponding displacements.
Physically, this procedure represent the usage of
compatibility and equilibrium equations.
Let’s consider a system of two rods:
ASSEMBLY OF STIFFNESS MATRICES - EXAMPLE
8
SOLUTION USING MATRIX METHOD - EXAMPLE
9
SOLUTION USING MATRIX METHOD - EXAMPLE
10
i j
1 0
k
SOLUTION USING MATRIX METHOD - EXAMPLE
11
i j
1 0
k
TRANSFORMATION MATRIX
12
Transformation matrix is used to transform nodal
displacements and forces from local to global
coordinate system (CS) and vice versa:
Transformation matrix is always orthogonal, thus, the
inverse matrix is equal to transposed matrix:
1 M
T T−
=
F T F Z T Z= ⋅ = ⋅
The transformation from local CS to global CS:
T T
F T F Z T Z= ⋅ = ⋅
For simplest member (rod) we get:
TRANSFORMATION MATRIX EXAMPLE
13
i
i
j
j
x
y
Z
x
y
 
 
 =
 
 
 
i
i
j
j
x
y
Z
x
y
 
 
 =
 
 
  Z T Z= ×
TRANSFORMATION MATRIX
14
To transform the stiffness matrix from local CS to
global CS, the following formula is used:
EXAMPLE FOR A TRUSS
15
The truss has three members, thus 6 degrees of
freedom. The stiffness matrix will be 6x6.
EXAMPLE FOR A TRUSS
16
EXAMPLE FOR A TRUSS
17
EXAMPLE FOR A TRUSS
18
EXAMPLE FOR A TRUSS
19
EXAMPLE FOR A TRUSS
20
EXAMPLE FOR A TRUSS
21
EXAMPLE FOR A TRUSS
22
EXAMPLE FOR A TRUSS
23
THREE BASIC EQUATIONS
Equilibrium
equations
Constitutive
equations
Compatibility
equations
Taken into account when global
stiffness matrix is assembled from
member matrices
Through member stiffness
matrices
Taken into account when global
stiffness matrix is assembled from
member matrices
How are they implemented in matrix method
24

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Matrix methods

  • 1. Government Engineering College, Bhavnagar. Civil Engineering Department
  • 2. METHODS TO SOLVE INDETERMINATE PROBLEM 2 Displacement methods Force method Small degree of statical indeterminacy Large degree of statical indeterminacy Displacement method in matrix formulation Numerical methods
  • 3. Disadvantages: • bulky calculations (not for hand calculations); • structural members should have some certain number of unknown nodal forces and nodal displacements; for complex members such as curved beams and arbitrary solids this requires some discretization, so no analytical solution is possible. ADVANTAGES AND DISADVANTAGES OF MATRIX METHODS 3 Advantages: • very formalized and computer-friendly; • versatile, suitable for large problems; • applicable for both statically determinate and indeterminate problems.
  • 4. FLOWCHART OF MATRIX METHOD 4 Classification of members Stiffness matrices for members Transformed stiffness matrices Stiffness matrices are composed according to member models Stiffness matrices are transformed from local to global coordinates Final equation F = K · Z Stress-strain state of structure Unknown displacements and reaction forces are calculated Stiffness matrices of separate members are assembled into a single stiffness matrix K
  • 5. STIFFNESS MATRIX OF STRUCTURAL MEMBER 5 Stiffness matrix (K) gives the relation between vectors of nodal forces (F) and nodal displacements (Z):
  • 6. EXAMPLE OF MEMBER STIFFNESS MATRIX 6 Stiffness relation for a rod: Stiffness matrix: ( )i j i EA F x x L = − ⋅ −
  • 7. ASSEMBLY OF STIFFNESS MATRICES 7 To assemble stiffness matrices of separate members into a single matrix for the whole structure, we should simply add terms for corresponding displacements. Physically, this procedure represent the usage of compatibility and equilibrium equations.
  • 8. Let’s consider a system of two rods: ASSEMBLY OF STIFFNESS MATRICES - EXAMPLE 8
  • 9. SOLUTION USING MATRIX METHOD - EXAMPLE 9
  • 10. SOLUTION USING MATRIX METHOD - EXAMPLE 10 i j 1 0 k
  • 11. SOLUTION USING MATRIX METHOD - EXAMPLE 11 i j 1 0 k
  • 12. TRANSFORMATION MATRIX 12 Transformation matrix is used to transform nodal displacements and forces from local to global coordinate system (CS) and vice versa: Transformation matrix is always orthogonal, thus, the inverse matrix is equal to transposed matrix: 1 M T T− = F T F Z T Z= ⋅ = ⋅ The transformation from local CS to global CS: T T F T F Z T Z= ⋅ = ⋅
  • 13. For simplest member (rod) we get: TRANSFORMATION MATRIX EXAMPLE 13 i i j j x y Z x y      =       i i j j x y Z x y      =       Z T Z= ×
  • 14. TRANSFORMATION MATRIX 14 To transform the stiffness matrix from local CS to global CS, the following formula is used:
  • 15. EXAMPLE FOR A TRUSS 15 The truss has three members, thus 6 degrees of freedom. The stiffness matrix will be 6x6.
  • 16. EXAMPLE FOR A TRUSS 16
  • 17. EXAMPLE FOR A TRUSS 17
  • 18. EXAMPLE FOR A TRUSS 18
  • 19. EXAMPLE FOR A TRUSS 19
  • 20. EXAMPLE FOR A TRUSS 20
  • 21. EXAMPLE FOR A TRUSS 21
  • 22. EXAMPLE FOR A TRUSS 22
  • 23. EXAMPLE FOR A TRUSS 23
  • 24. THREE BASIC EQUATIONS Equilibrium equations Constitutive equations Compatibility equations Taken into account when global stiffness matrix is assembled from member matrices Through member stiffness matrices Taken into account when global stiffness matrix is assembled from member matrices How are they implemented in matrix method 24