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Problem-1
Consider a member of a truss A, B which is making an angle theeta with respect
horizontal axis. Let 1,2,3 and 4 be the coordinates for displacement and the forces
acting at the jointsto of the member, let L,A,E be the properties of the member.
under consideration
A 1
E 1
L 1
theeta degrees
1 2 3 4
1 0 -1 0 1
[k]= 0 0 0 0 2 * 1
-1 0 1 0 3
0 0 0 0 4
1 0 -1 0
[k]= 0 0 0 0
-1 0 1 0
0 0 0 0
Development of Stiffness Matrix for Truss Element
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2
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1
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2
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2
2
2
2
2
2
2
2
1
1
sin
sin
cos
sin
sin
cos
sin
cos
cos
sin
cos
cos
sin
sin
cos
sin
sin
cos
sin
cos
cos
sin
cos
cos
v
u
v
u
L
AE
F
F
F
F
y
x
y
x
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Problem-2
Develop stiffness matrix for truss element shown in the figure by direct stifness
method take AE/L =1
The number of displacement at a joint in a truss is equal to 2, in the given problem
there are 4 joints. The total degree of freedom was supposed to be 8. But
the joint B,C, and D are supported with a hinge due toi this the displacement
(both vertical and horizontal will be equal to zero at B,C and D)
The actual degree of freedom or DOF = 2
. L (m) AE/L Theeta Cos theeta sin theeta
AB 5 1 126.87 -0.600001 0.7999989
AC 4 1 90 0 1
AD 5.65 1 45 0.7071068 0.7071068
1 2 3 4
0.3600017 -0.480001 -0.360002 0.4800005 1
[K]AB= -0.480001 0.6399983 0.4800005 0.6399983 2
-0.360002 0.4800005 0.3600017 -0.480001 3 *
0.4800005 0.6399983 -0.480001 0.6399983 4
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2
2
1
1
2
2
2
2
2
2
2
2
2
2
1
1
sin
sin
cos
sin
sin
cos
sin
cos
cos
sin
cos
cos
sin
sin
cos
sin
sin
cos
sin
cos
cos
sin
cos
cos
v
u
v
u
L
AE
F
F
F
F
y
x
y
x
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1 2 5 6
[K]AC= 0 0 0 0 1
0 1 0 1 2
0 0 0 0 5
0 1 0 1 6
1 2 7 8
[K]AD= 0.5 0.5 -0.5 -0.5 1
0.5 0.5 -0.5 0.5 2
0 -0.5 0.5 0.5 7
-0.5 0.5 0.5 0.5 8
The co- ordinates 3,4, 5,6,7 and 8 are restrained due to this there are only
displacement in the direction of co- ordinate 1 and 2
1 2
[k]= 0.8600017 0.0199995 1
0.0199995 2.1399983 2

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Introduction to Multiple Access Protocol.pptx
 

Stifness matrix 2

  • 1. Problem-1 Consider a member of a truss A, B which is making an angle theeta with respect horizontal axis. Let 1,2,3 and 4 be the coordinates for displacement and the forces acting at the jointsto of the member, let L,A,E be the properties of the member. under consideration A 1 E 1 L 1 theeta degrees 1 2 3 4 1 0 -1 0 1 [k]= 0 0 0 0 2 * 1 -1 0 1 0 3 0 0 0 0 4 1 0 -1 0 [k]= 0 0 0 0 -1 0 1 0 0 0 0 0 Development of Stiffness Matrix for Truss Element                             − − − − − − =               2 2 1 1 2 2 2 2 2 2 2 2 2 2 1 1 sin sin cos sin sin cos sin cos cos sin cos cos sin sin cos sin sin cos sin cos cos sin cos cos v u v u L AE F F F F y x y x                        
  • 2. Problem-2 Develop stiffness matrix for truss element shown in the figure by direct stifness method take AE/L =1 The number of displacement at a joint in a truss is equal to 2, in the given problem there are 4 joints. The total degree of freedom was supposed to be 8. But the joint B,C, and D are supported with a hinge due toi this the displacement (both vertical and horizontal will be equal to zero at B,C and D) The actual degree of freedom or DOF = 2 . L (m) AE/L Theeta Cos theeta sin theeta AB 5 1 126.87 -0.600001 0.7999989 AC 4 1 90 0 1 AD 5.65 1 45 0.7071068 0.7071068 1 2 3 4 0.3600017 -0.480001 -0.360002 0.4800005 1 [K]AB= -0.480001 0.6399983 0.4800005 0.6399983 2 -0.360002 0.4800005 0.3600017 -0.480001 3 * 0.4800005 0.6399983 -0.480001 0.6399983 4                             − − − − − − =               2 2 1 1 2 2 2 2 2 2 2 2 2 2 1 1 sin sin cos sin sin cos sin cos cos sin cos cos sin sin cos sin sin cos sin cos cos sin cos cos v u v u L AE F F F F y x y x                        
  • 3. 1 2 5 6 [K]AC= 0 0 0 0 1 0 1 0 1 2 0 0 0 0 5 0 1 0 1 6 1 2 7 8 [K]AD= 0.5 0.5 -0.5 -0.5 1 0.5 0.5 -0.5 0.5 2 0 -0.5 0.5 0.5 7 -0.5 0.5 0.5 0.5 8 The co- ordinates 3,4, 5,6,7 and 8 are restrained due to this there are only displacement in the direction of co- ordinate 1 and 2 1 2 [k]= 0.8600017 0.0199995 1 0.0199995 2.1399983 2