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Displacement Method of Analysis Moment Distribution Method
Chapter 12
– In this method, joint rotations & displacements are used as unknowns in carrying out the analysis.
– Unlike the slope deflection method, the moment-distribution method does not require the solution of simultaneous equations, instead answers are obtained by a procedure of successive approximations (iteration technique).
– From the slope deflection equations it is evident that the moments acting on the ends of a member in a frame consist of several distinct parts;• The fixed-end moments, which are the moments caused by the
load acting on the member, with the ends of the member assumed to be fixed.
• The moment due to the rotations that actually take at the ends of the member.
• The moments caused by the translation of one end of the member relative to the other
Introduction
General Principles
• Sign convention– Same sign as slope deflection equations; clockwise moments are
considered positive & counterclockwise moments are negative.
• Member stiffness factor– If the beam is pinned at one end & fixed at the other
2 2 3 ( )AB A B AB
IM E FEM
L L
2
2 0 0 0AB A
EIM
L
4AB A
EIM
L
For unit A = 1
4AB
EIK
L
It is referred to as the stiffness factor at A and can be
defined as as the amount of moment M required to rotate
the end A of the beam A = 1 radian
General PrinciplesJoint Stiffness Factor
The total stiffness factor for joint A is
equal to the summation of the stiffness
factor of each member.
A AB AD ACK K K K
1000 4000 5000 10000AK
That means a moment of 10000 needed to
rotate joint A (1 radian)
Distribution Factor (DF)
If a moment M is applied to joint A, that will rotate joint A an amount of
then each member connected to that joint will rotate by this same amount
M
1 i nM M M M 1 i n iK K K K
The distribution factor for ith member is
i ii
i
M KDF
M K
K
DFK
General Principles• Example; Fined the moment at each side of joint A (MAB, MAD & MAC).
M=2000N.m
The total stiffness factor of joint A
1000 4000 5000 10000K The distribution factors for each members
at joint A
40000.4
10000ABDF
50000.5
10000ACDF
10000.1
10000ADDF
The moment of each member at the joint
0.4 2000 800 .ABM N m
0.5 2000 1000 .ACM N m
0.1 2000 200 .ADM N m
General Principles
• Member relative-stiffness
– As in the most cases, the frame or the beam, will be made from the same material, same modulus of elasticity, then the 4E is same for all members.
1 1
1 1
1 1
1 1
4
4 4 4i n i n
i n i n
EI I
K L LDF
EI EI EI I I IK
L L L L L L
R
IK
L
General Principles
• Carry-Over Factor
– The applied moment M at A cause A to rotate A.
– Applying slope deflection;
2 42 3AB A B AB A
EI EIM FEM
L L L
2 22 3BA B A BA A
EI EIM FEM
L L L
1
2BA ABM M
That means that, the moment M at the pin induces a moment 0.5 M at the
fixed end. In this case the carry over factor is +0.5.
The carry-over represent the fraction of M that is carried over from the
pin to the wall.
Problem 1• Determine the internal moment at each support of the beam
1. Calculate the distribution factors at all
joints that are free to rotate 4 (300)
4 (20)15
BA
EK E
4 (600)4 (30)
20BC
EK E
Joint B 4 (20)
0.44 (20) 4 (30)
BA
EDF
E E
4 (30)0.6
4 (20) 4 (30)BC
EDF
E E
For joint A & C the distribution factors = 0. 4 (20)
0.4 (20)
AB
EDF
E
4 (30)0.
4 (30)CB
EDF
E
2. Calculate the fixed end moment
assuming all joints to be locked
0.AB BAFEM FEM
2240(20)8000 .
12BCFEM lb ft 8000 .CBFEM lb ft
3. Begin the actual moment distribution process
0.60.40. 0.D.F.
80000.0. 8000F.E.M.
480032000. 0.Balancing Joint B
1600 2400Carry over moment
Final Ms 320032001600 10400
Problem 1
Example 12-1• Draw the bending moment diagram.
1. The distribution factors
4
12AB
EIK
4
12BC
EIK
Joint B 4 /12
0.54 /12 4 /12
BA
EIDF
EI EI
4 /120.5
4 /12 4 /12BC
EIDF
EI EI
Joint C 4 /12
0.44 / 8 4 /12
CB
EIDF
EI EI
4 / 80.6
4 / 8 4 /12CD
EIDF
EI EI
4
8CD
EIK
2. Fixed end moment
0.AB BAFEM FEM
220(12)240 .
12BCFEM kN m 240 .CBFEM kN m
250(8)250 .
8CDFEM kN m 250 .DCFEM kN m
1 36
6 0.3
0.05 1.8
6120
Example 12-1
D.F.
2400.0. 250F.E.M.
120Balancing
60 3C.O.M
Final Ms 125.3125.362.5 234.3
0.50.50. 0.0.60.4
250240
4
281.5281.5
2 60
1Balancing
0.5 18C.O.M
24
12 0.5
6Balancing
3 0.15C.O.M
0.2
0.1 3
0.05Balancing
0.02 0.9C.O.M
1.2
0.6 0.02
Balancing 0.30.3 0.010.01
3. Begin the actual moment distribution process
Example 12-1
Problem 2• Determine the internal moment at each support.
1. The distribution factors
4
6AB
EIK
8
6BC
EIK
Joint B 4 / 6 1
4 / 6 8 / 6 3BA
EIDF
EI EI
8 / 6 2
4 / 6 8 / 6 3BC
EIDF
EI EI
Joint C 8 / 6
18 / 6
CB
EIDF
EI
2. Fixed end moment23(6)
9 .12
BCFEM t m 9 .CBFEM t m
8(6)6 .
8ABFEM t m 6 .BAFEM t m
A3t/m8t
B C2II
3m 3m 6m
3. Begin the actual moment distribution process
9
1
1.5
0.17
3
0.34
0.5
2
D.F.
966 9F.E.M.
1Balancing
0.5 1C.O.M
Final Ms 8.938.934.54 0.
2 / 31/ 30. 1.
4.5
1.5Balancing
0.75 1.5C.O.M 0.5
0.16Balancing
0.08 0.17C.O.M 0.75
0.25Balancing
0.12 0.25C.O.M 0.08Balancing 0.060.02 0.25
0.
0.
0.
0.
0.
Problem 2
Example 12-2
Example 12-2
Example 12-2
Stiffness-Factor Modification• Member pin supported at far end.
– Using slop-deflection equations
22 3AB A B AB
EIM FEM
L L
22 3BA B A BA
EIM FEM
L L
0.BAM
2 32 0 0
2
AAB A A
EI EIM
L L
The stiffness factor for this beam is;
3EIK
L
2
0. 2 0 0B A
EI
L
2
AB
To model the case of having the far end pinned or
roller supported
Problem 3• Back to Problem 3- Solution A
1. The distribution factors
4
6AB
EIK
6
6BC
EIK
Joint B 4
0.44 6
BADF
60.6
4 6BCDF
Joint C 8 / 6
18 / 6
CB
EIDF
EI
2. Fixed end moment23(6)
13.5 .8
BCFEM t m
8(6)6 .
8ABFEM t m 6 .BAFEM t m
A3t/m8t
B C2II
3m 3m 6m
4.5
D.F.
13.566F.E.M.
3Balancing
1.5C.O.M
Final Ms 994.5 0.
0.60.40.
0.
1.
Balancing 0. 0. 0.
• Determine the internal moment at each support.1t/m9t.m
A
B C
12m4m2m4m 2m
D9t.m1. The distribution factors
4
6AB
EIK
4
12BC
EIK
Joint B 4 / 6 2
4 / 6 4 /12 3BA
EIDF
EI EI
4 /12 1
4 / 6 4 /12 3BC
EIDF
EI EI
2. Fixed end moment21(12)
12 .12
BCFEM t m 12 .CBFEM t m
2
9 2(2 4 2)3 .
6ABFEM t m
4
6CD
EIK
Joint C 4 / 6 2
4 / 6 4 /12 3CD
EIDF
EI EI
4 /12 1
4 / 6 4 /12 3CB
EIDF
EI EI
2
9 4(2 2 4)0. .
6BAFEM t m
2
9 2(2 4 2)3 .
6DCFEM t m
2
9 4(2 2 4)0. .
6CDFEM t m
Problem 4
Problem 41t/m9t.m
A
B C
D9t.m
3. Begin the actual moment distribution process
0.67 1.33
0.11 0.22
0.02 0.04
84
D.F.
120.3 3F.E.M.
8Balancing
4 4C.O.M
Final Ms 9.599.591.8 1.8
1/ 32 / 30. 0.2 / 31/ 3
0.12
4
9.599.59
2 2
1.33Balancing
0.67 0.67C.O.M
0.67
0.33 0.33
0.22Balancing
0.11 0.11C.O.M
0.11
0.06 0.06
0.04Balancing
0.02 0.02C.O.M
0.02
Stiffness-Factor Modification
22 3BC B C BC
EIM FEM
L L
2AB B
EIM
L
The stiffness factor is;
2EIK
L
2
2 0 0BC B B
EIM
L
For the center span of Symmetric beam & load
From symmetry of load C = -B
Symmetric beam & loading.– Using slop-deflection equations
Stiffness-Factor Modification
22 3BC B C BC
EIM FEM
L L
6AB B
EIM
L
The stiffness factor is;
6EIK
L
2
2 0 0BC B B
EIM
L
For the center span of Symmetric beam & load
From symmetry of load C = B
Symmetric beam with Anti-symmetric Loading.– Using slop-deflection equations
Problem 5• Back to Problem 4
1t/m9t.mA
B C
12m4m2m4m 2m
D9t.m
1. The distribution factors
4
6AB
EIK
2
12BC
EIK
Joint B 4 / 6
0.84 / 6 2 /12
BA
EIDF
EI EI
2 /120.2
4 / 6 2 /12BC
EIDF
EI EI
2. Fixed end moment
12 .
12 .
3 .
0 .
BC
CB
AB
BA
FEM t m
FEM t m
FEM t m
FEM t m
2.4
D.F.
120.3F.E.M.
9.6Balancing
4.8C.O.M
Final Ms 9.69.61.8 1.8
0.20.80.
9.69.6
Example 12-3
Determine the internal moment at the supports for the beam shown. EI is constant
Example 12-4
Determine the internal moment at the supports for the beam shown. E is constant
Example 12-4
• Determine the internal moment at each support when support B sinks by 10mm. EI = 200t.m2
1. The distribution factors4
3AB
EIK
3
6BC
EIK
Joint B 4 / 3
0.734 / 3 3 / 6
BA
EIDF
EI EI
3 / 60.27
4 / 3 3 / 6BC
EIDF
EI EI
Joint C 4 / 6
14 / 6
CB
EIDF
EI
2. Fixed end moment
22(6) /8 9 .BCFEM t m
6(3) / 8 2.25 .ABFEM t m
2.25 .BAFEM t m
1.5m
A2t/m6t
B C
3m 6m
2t
Moment developed by the settlements Member AB
2 2
6 6 200 0.01
3AB BA
EIFEM FEM
L
1.33 .AB BAFEM FEM t m
Member BC
2 2
3 3 200 0.01
6BC
EIFEM
L
0.165 .BCFEM t m
Cantilevers moment2 1.5 3 .CM t m
Problem 6
3. Begin the actual moment distribution process
7.34
1.74
0.165
D.F.
92.252.25F.E.M.
1.33FEM due to
Final Ms 5.65.61.24 3
0.270.730. 1.
0.92
4.68Balancing
2.34C.O.M
1.33
3.58
0.
3
A
B C
3
Total Modified F.E.M.
Problem 6
Balancing joint C 3
1.5C.O.M
Balancing 0.0.
0.
0
Problem 7: Frame with No Sway
• Determine the internal moment at each support. EI constant
4t
C
3t/m
8m3m
3m
A
B
C
A
B 0.5 0.
16 16
5.75
10.25
2.875
18.875
1. The distribution factors
3
6AB
EIK
4
8BC
EIK
Joint B 1/ 2
0.51/ 2 1/ 2
BADF
1/ 20.5
1/ 2 1/ 2BCDF
2. Fixed end moment
23(8) /12 16 .BCFEM t m
16 .CBFEM t m
3
(4) 6 4.5 .16
BAFEM t m
38.4 13.3326.6757.6
0.
0.
0 013.147.89
-9.9
0
• Determine the internal moment at each support. EI constant
1. The distribution factors
4
5AB
EIK
4
3BC
EIK
Joint B 4 / 5
0.2554 / 5 4 / 3 1
BADF
4 / 30.425
4 / 5 4 / 3 1BCDF
2. Fixed end moment
26.67 .BCFEM kN m
13.33 .CBFEM kN m
38.4 .ABFEM kN m
57.6 .BAFEM kN m
1m 2m
C
60kN
4m
A B
3m 2m
D
80kN
4
4BD
EIK
10.32
4 / 5 4 / 3 1BDDF
0BD DBFEM FEM
0.255 0.425
0.3
2
0. 0.
0.
-4.9
5
3.945 6.57
-4.9
5
42.345 6.7639.8149.71
-9.9
Problem 8
Example 12-5
Determine the internal moment at the joints for the frame shown.
There is a pin support at E and D and a fixed support at A. EI is constant
Example 12-5
Frames with Sway
Example 12-6• Determine the moment at each joint. EI is constant
(C) (B)(A)
Moment at A is equal to the moment at B plus the moment at C
0.32 0.08
0.3
20
.
0.
-0.0
8
Example 12-6• Structure B
DFBA= 0.5
Distribution factors
Joint B
Joint C
Fixed end moment
DFBC= 0.5
DFCB= 0.5
DFCD= 0.5
FEMBC= -10.24 kN.m
FEMCB= 2.56 kN.m
10.24 2.56
0.
0.
0.
0.0.5
0.5
0.5
0.
0.
0.5
5.12 1.28
5.1
20
.
0.
-1.2
8
2.8
8
5.76 2.64
5.7
6
-2.6
4-1
.322
.56
0.
0.64 2.56
-0.6
4
0.
0.32 1.28
0.3
20
.
0.
-1.2
80.64 0.16
0.1
6
-0.6
4
0.
0.
0.1
6
-0.0
4
Example 12-6
R = HA + HD
Determine the joint resistance RFx = 0.
By taking the moment at C we get
HD = -0.79
B
HA
5.76
2.88A
C
HD
-2.64
-1.32D
R
By taking the moment at B we get
HD = 1.73
R = 1.73 – 0.79 = 0.94 kN
• Structure C0.94
kN
2
6EIModified Fixed End Moment FEM
L
6
25AB BA CD DC
EIMFEM MFEM MFEM MFEM
Assuming all the joints are locked, the
produced by the load R caused a moment M
As is equal in column AB & CD & FEM = 0.
0.BC CBMFEM MFEM
0.19 0.19
0.1
90.
0.
0.1
9
Example 12-6The final moment produced by the R = 0.94 kN can be determined by;
Take EI = 25 and then fined out the moment on the frame
0. 0.
-6-6
-6-60.5
0.5
0.5
0.
0.
0.5
3 3
30.
0.
3
-4.8
3.6 3.6
-3.6
-3.6
-4.8
1.5
0.
1.5 1.5
1.5
0.
0.75 0.75
-0.7
50.
0.
-0.7
5
0.375 0.375
-0.3
75 -0
.375
0.
0.
0.1
0
0.1
06AB BA CD DCMFEM MFEM MFEM MFEM
0.BC CBMFEM MFEM
Example 12-6
R’ = H’A + H’D
Determine the joint resistance R’ that produced EI = 25Fx = 0.
By taking the moment at C we get
H’D = 1.68
H’A
B
-3.6
-4.8AH’
D
C
-3.6
-4.8D
R’
By taking the moment at B we get
HA = 1.68
R’ = 1.68 + 1.68 = 3.36 kN
0.94 25
0.94
3.36R EIM M
The moment produced by the reaction R = 0.94 kN would be
1.01 1.01
-1.0
1-1
.34 -1
.34
-1.0
1
Example 12-6
The final moment would be the moment of B plus the moment of C
5.76 1.01 4.75 .BCM kN m
2.64 1.01 3.65 .CBM kN m
2.88 1.34 1.54 .ABM kN m
5.76 1.01 4.75 .BAM kN m
2.64 1.01 3.65 .CDM kN m
1.32 1.34 2.66 .DCM kN m
3.125 3.125
3.1
25
0.
0.
3.1
25
Example 12-6 Solution B
0. 0.
-10
0-1
00
-100
-10
0
0.5
0.5
0.5
0.
0.
0.5
50 50
50
0.
0.
50
-80
1.56
0.195
-60
0.1
95
-80
25
0.
25 25
25
0.
12.5 12.5
-12.5
0.
0.
-12.5
6.25 6.25
-6.5
-6.2
50.
0.
1.5
6
1.5
6
100AB BA CD DCMFEM MFEM MFEM MFEM
0.BC CBMFEM MFEM
1.56
-0.7
8-0
.39
0.
0. 0.
0.780.78
0.39
60
0.39
0.195
60
0.
-60
0.
-0.7
80.
0.1
95
-0.3
9
Example 12-6 Solution B
R’ = H’A + H’D
Determine the joint resistance R’ that produced MFEM=100
Fx = 0.
By taking the moment at C we get
H’D = 28 kN
H’A
B
-60
-80AH’
D
C
-60
-80D
R’
By taking the moment at B we get
HB = 28 kN
R’ = 28 + 28 = 56.0 kN
0.94
0.94100
56.0RM MFEM
The moment produced by the reaction R = 0.94 kN would be
1.01 1.01
-1.0
1-1
.34 -1
.34
-1.0
1
Example 12-6
The final moment would be the moment of B plus the moment of C
5.76 1.01 4.75 .BCM kN m
2.64 1.01 3.65 .CBM kN m
2.88 1.34 1.54 .ABM kN m
5.76 1.01 4.75 .BAM kN m
2.64 1.01 3.65 .CDM kN m
1.32 1.34 2.66 .DCM kN m
Example 12-7Determine the moment at each joint of the frame shown. E is constant
Example 12-7
Example 12-7
Example 12-7
Problem 9• Determine the moment at each joint. EI is constant
(C)(B)(A)
• Structure BDistribution factors
Joint B (symmetry)
Fixed end momentFEMBC = -16.33 kN.m
FEMCB = 16.33 kN.m
4
8,6BA
EIK
2
7BC
EIK
4 / 8.60.62
4 / 8.6 2 / 7BA
EIDF
EI EI
2 / 70.38
4 / 8.6 2 / 7BC
EIDF
EI EI
0.38
16.33
6.21
10.12
0.
Determine the joint resistance R
R = 6 kN (symmetry HA = HD)
Problem 9
• Structure C
2
6
8.6AB BA CD DC
EIMFEM MFEM MFEM MFEM
Assuming all the joints are locked, the
produced by the load R caused a moment M
2
6 6.98( 1.163 )
7 49BC CB
EI EIMFEM MFEM
6 kN
A
B
D
C
AB
BC
CD
B1
2
2
6EIMFEM FEM
L
0.
take AB =
BC = 2(AB cos) = 2 5/8.6 = 1.163
CD = AB =
Take EI = 8.62 and then fined out the moment on the frame
6AB BA CD DCMFEM MFEM MFEM MFEM
10.53BC CBMFEM MFEM
Problem 9
0.190.19
10.5310.532.492.49
7.67.6
1.251.25
0.690.69
0.350.35
0.550.55
The joint resistance R’ that produced EI = 8.62
R’ = H’A + H’D
Fx = 0.
Problem 9
Free body diagram for column AB & taking the moment at B = 0.
A
B
H’A
6.8
7.6
5m
7m
VA
' 7 6.8 7.6 5 0A AH V
Free body diagram for Beam BC& taking the moment at C = 0.
7 7.6 7.6 0BV
' 3.6AH
2.17A BV V
VB
C
7.1B
7.1
VC
C
H’D
6.6
6.8
5m
7m
D
VD
Free body diagram for column CD & taking the moment at C = 0.
' 7 6.8 7.6 5 0D DH V
7 7.6 7.6 0CV
' 3.6DH
2.17D CV V
Free body diagram for Beam BC& taking the moment at B = 0.
Problem 9
R’ = 3.6 + 3.6= 7.2 kN
26 8.6
6
7.2R EI
M M
The moment produced by the reaction R = 6 kN would be
The final moment would be the moment of B plus the moment of C
10.12 6.26 3.79 .BCM kN m
10.12 6.33 16.45 .CBM kN m
5.06 5.67 0.61 .ABM kN m
10.12 6.33 3.79 .BAM kN m
10.12 6.33 16.45 .CDM kN m
5.06 5.67 10.73 .DCM kN m
6.336.33
Problem 9
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