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A B C D EF
GH
Influence Line for Girder
• Forces Apply to the Girder
(b/L)P1 (a/L)P1 P2
P1
a b
P2
L
A B
P1
D
P2
A
B C D
F
GH
61
A F
GH
• Reaction
1
0.5 0.5
RGRH
RH
1
62
A F
GH
RG
1
0.5 0.5
RG
11
RH
63
A F
GH
• Shear
L
a b b b
1
0.5 0.5
1
1
VC
VC
VC
x
2b/L
-(a+b)/L
1
C
64
A F
GH
L
VCD
VCD
1
0.5 0.5
1
0.5 0.5
VCD x
-a/L
b/L
a b
65
A
C
F
GH
• Bending Moment
L
a b
ab/L
1
0.5 0.5
MC
x
1
1
MC
MC
C
66
A
B C D E
F
GH
L
MF
x
1
0.5 0.5
1
0.5 0.5
MF
MF
a b
ab/L
67
Example 6-5
Draw the influence for
- the Reaction RG and RF
- Shear VCD
- the moment MC and MH
1.5 m 1.5 m
A
C D
H
F
3 m 3 m 3 m 3 m
G
68
1
RG
x
RG
1.333
0.667
0.333
1.5 m 1.5 m
A H
F
3 m 3 m 3 m 3 m
G
69
RF
x
RF
1
0.667
0.333
-0.333
1.5 m 1.5 m
A H
F
3 m 3 m 3 m 3 m
G
70
1.5 m 1.5 m
A H
F
3 m 3 m 3 m 3 m
G
VCD
x
VCD
VCD
1
0.5 0.5
4.5/9
-4.5/9
0.333
-0.333
0.333
C D
71
1.5 m 1.5 m
A H
F
3 m 3 m 3 m 3 m
G
MC
MC
1
1
MC
x
(3)(6)/9 = 2
-2
1
C
72
MH
MH
1
0.5 0.5
MH
x
(4.5)(4.5)/9 = 2.25
1.51.5
-1.5
1.5 m 1.5 m
A H
F
3 m 3 m 3 m 3 m
G
73
Example 6-6
Draw the influence line diagrams of girder for
- the reaction at C and G,
- shear at E and H,
- bending moment at H.
2 m
A
GB
6 @ 4 m = 24 m
C D E FH
74
SOLUTION
RC
RC
1
0.75
0.50
0.25
1.25
A
GB
6 @ 4 m = 24 m
C D E FH
2 m
75
A
GB
6 @ 4 m = 24 m
C D E FH
2 m
RG
RG
1
1
1
0.25
0.50
0.75
-0.25
76
A
GB
6 @ 4 m = 24 m
C D E FH
2 m
VE
1
1
1
1
VE
VE
8/16 = 0.5
-8/16 = 0.5-0.25
0.250.25
8 m 8 m
77
A
GB
6 @ 4 m = 24 m
C D E FH
2 m
6/16 = 0.375
-10/16 = 0.625
VH
1
1
VH
VH
1
0.5 0.5
-0.25
0.250.25
-0.50
10 m 6 m
78
A
GB
6 @ 4 m = 24 m
C D E FH
2 m
MH
1
1
1
0.5 0.5
MH
MH
(10)(6)/16 = 3.75
1.50
2.50
-1.50
3
10 m 6 m
79
Draw the influence for
- the Reaction RG and RH
- Shear VC and VCD
- the moment MC, MD, and MF
and determine the maximum for
- the Reaction (RG)max and (RH)max
- Shear (VCD)max
due to
- a uniform dead load 2 kN/m
- a uniform live load 5 kN/m
- a concentrated live load 50 kN
Example 6-7
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
80
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
RG
1
0.5 0.5
10/14
6/14
2/14
1/14
RG
11
RH
81
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
E
F
GH
1
0.5 0.5
RGRH
RH
1 12/14
8/14
4/146/14
82
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
VC
VC
1
0.5 0.5
VC
x
8/14
-6/14
1
1
1
-2/14
4/14
-1/14
83
-8/14
6/14
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
VF
VF
1
0.5 0.5
1
0.5 0.5
VCD x
-1/14 -2/14
-6/14
4/14
84
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
(6)(8)/14 = 3.43
1
0.5 0.5
MC
x
(4/8)(3.43)
(2/6)(3.43)
1
1
MC
MC
85
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
E
F
GH
1
0.5 0.5
1
1
MD x
(10)(4)/14 = 2.86(6/10)(2.86)
(2/10)(2.86)
MD
MD
86
(8)(6)/14=3.428
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D
F
GH
MF
x
1
0.5 0.5
1
0.5 0.5
2.285
2.571
0.857
0.429
MF
MF
87
[0.5×4 (2/14)] + [(0.5)(2/14 + 1)(12) = 7.143
RG
1
10/14
6/14
2/14
1/14
Maximum Reaction
2 kN/m
5 kN/m
50 kN
(RG)max = (2)(7.143) + (5)(7.143) + (50)(1)
= 100 kN
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D E
F
GH
88
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D E
F
GH
(0.5)(16)(12/14) = 6.857
RH
12/14
8/14
4/146/14
Maximum Reaction
2 kN/m
5 kN/m
50 kN
(RH)max = (2)(6.857) + (5)(6.857) + (50)(12/14)
= 90.86 kN
89
2 m 2 m 4 m 4 m 4 m
2 m 2 m
A
B C D E
F
GH
+ (0.5)(5.6)(4/14) = + 0.8
-[0.5(4)(2/14) + 0.5(2/14) + (6/14)(4) + 0.5(2.4)(6/14)] = -1.943
2.4 m
VCD
-1/14 -2/14
-6/14
4/14
Maximum Shear
2 kN/m
5 kN/m
50 kN
(VCD)max = (2)(-1.943 + 0.8) (5)(-1.943) + (50)(-6/14)
= -33.43 kN
C D
90
SP 6-1
Draw the influence line for
-the reaction at support A and D
-the shear and moment at E
- the moment at B and C .
2 m 2 m 2 m 2 m 2 m
A B E C D
91
Influence Line for Trusses
RA
x
1
RE
x
1
(3/4)
(2/4)
(1/4)
(2/4)
(3/4)
(1/4)
A
B C
E
GH
D
F
4 @ x m
h
92
A
B C
E
GH
D
F
4 @ x m
h
1 kN
Consider the section to the right
FCB
RE
FGB
FGH
FBC x
(2x/h)(1/4)
+ ΣMG = 0:
0)()2( =− hFxR BCE
EBC R
h
x
F
2
=
RE
x
1
(2/4)
(3/4)
(1/4)
93
A
B C
E
GH
D
F
4 @ x m
h
1 kN
Consider section to the left
FHG
FBC
RA
FBG
+ ΣMG = 0:
0)2()( =− xRhF ABC
ABC R
h
x
F
2
=
FBC x
(2x/h)(1/4)
RA
x
1
(3/4)
(2/4)
(1/4)
(2x/h)(1/4)
(2x/h)(2/4)
94
Determine the maximum force developed
in member BC , BG, and CG of the truss
due to the wheel loads of the car. Assume the
loads are applied directly to the truss.
the wheel loads of the car
4 kN 1.5 kN2 m
Example 6-8-1
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
95
RA
x
1
0.75
0.5
0.25
RE
x
0.5
0.75
0.25
1
SOLUTION
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
96
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
Influence Line for FBC
1 kN
Consider the section to the right
FBC = (6/4) RE
= 1.5 RE
FCB
RE
FGB
FGH
RE
x
0.5
0.75
0.25
1
FBC x
1.5(0.25) = 0.375
+ ΣMG = 0:
97
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
0.375
1.5(0.5) = 0.75
1 kN
Consider the section to the left
FHG
FBC
RA
FBG
RA
x
1
0.75
0.5
0.25
FBC = 1.5 RA
FBC
x
0.375
+ ΣMG = 0:
98
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
RE
x
0.5
0.75
0.25
1
Influence Line for FBG
1 kN
Consider the section to the right
ΣFy = 0 ;
FBG cos θ = RE
FGH
FGB
FCB
RE
θ
FBG = 1.25 RE
FBG (4/5) = RE1.25(0.25) = 0.3125
FBG x
99
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
1 kN
Consider the left hand
ΣFy = 0 ;
FBG cos θ + RA = 0
RA
x
1
0.75
0.5
0.25
FHG
FBC
RA
FBG
θ
0.3125
FBG x
FBG = -1.25 RA
FBG (4/5) = -RA
-0.3125
-1.25(0.5) = -0.625
100
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
FCG x
Influence Line for FCG
1 kN
0
1 kN
0
101
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
FCG x
1 kN
1
1
102
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
(FBC)max by Loads
(FBC)max = (4)(0.75) + (1.5)(0.5)
= 3.75 kN (T)
0.375
0.75
FBC
x
0.375
4 kN 1.5 kN2 m
0.5
103
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
(FBG)max by Loads
(FBG)max = (4)(-0.625) + (1.5)(-0.417) = -3.126 kN (C)
FBG x
-0.3125
0.3125
-0.625
4 kN 1.5 kN2 m
-0.417
104
A
B C
E
GH
4 m
D
F
3 m 3 m 3 m 3 m
(FCG)max by Loads
FCG x
1
0.333
(FCG)max = (4)(1) + (1.5)(0.333) = 4.50 kN (T)
4 kN 1.5 kN2 m
105
Draw the influence line for FBC , FBH,and FCH.
Example 6-8-2
A
B C
E
HI
4 m
D
F
3 m 3 m 3 m 3 m
GJ
106
RA
x
1
0.75
0.5
0.25
RE
x
0.5
0.75
0.25
1
SOLUTION
A
B C
E
HI
4 m
D
F
3 m 3 m 3 m 3 m
GJ
107
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJInfluence Line for FBC
1 kN
Consider the section to the right
FBC = (6/4) RE
= 1.5 RE
FCB
RE
FHB
FHI
RE
x
0.5
0.75
0.25
1
FBC x
1.5(0.25) = 0.375
+ ΣMH = 0:
108
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJ
0.375
1.5(0.5) = 0.75
1 kN
Consider the section to the left
FHI
FBC
RA
FBH
RA
x
1
0.75
0.5
0.25
FBC = 1.5 RA
FBC
x
0.375
+ ΣMH = 0:
109
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJ
RE
x
0.5
0.75
0.25
1
Influence Line for FBH
1 kN
Consider the section to the right
ΣFy = 0 ;
FBH cos θ = RE
FHI
FBH
FCB
RE
θ
FBH = 1.25 RE
FBH (4/5) = RE1.25(0.25) = 0.3125
FBH x
110
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJ
1 kN
Consider the section to the left
ΣFy = 0 ;
FBH cos θ + RA = 0
RA
x
1
0.75
0.5
0.25
FHI
FBC
RA
FBH
θ
0.3125
FBH x
FBH = -1.25 RA
FBH (4/5) = -RA
-0.3125
-1.25(0.5) = -0.625
111
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJ
FCH x
Influence Line for FCH
1 kN
FGH
FCH
FCB
RE
x
0.5
0.75
0.25
1
RE
ΣFy = 0 ;
FCH = -RE
-0.25
112
A
B C
E
HI
4 m
D
G
3 m 3 m 3 m 3 m
FJ
FCH x
1 kN
FGH
FCH
FCB
RA
ΣFy = 0 ;
FCH = RA
-0.25
RA
x
1
0.75
0.5
0.25
0.5
0.25
113
Draw the influence line for FBC , FBG,and FHG.
Example 6-8-3
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
114
RA
x
1
0.75
0.5
0.25
RE
x
0.5
0.75
0.25
1
SOLUTION
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
115
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
Influence Line for FBC
1 kN
Consider the section to the right
FBC = (6/4.5) RE
= 1.33 RE
RE
x
0.5
0.75
0.25
1
FBC x
1.33(0.25) = 0.333
+ ΣMG = 0:
RE
FBC
FBG
FHG
116
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
1 kN
Consider the section to the left
FBC = (6/4.5) RA
= 1.33 RA
FBC x
1.33(0.25) = 0.333
+ ΣMG = 0:
RA
RA
x
1
0.75
0.5
0.25
FBC
FBG
FHG
1.33(0.5) = 0.667
1.33(0.25) = 0.333
117
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
Influence Line for FHG
1 kN
Consider the section to the right
RE
x
0.5
0.75
0.25
1
FHG x
+ ΣMB = 0:
RE
FBC
FBG
FHG
26.57o
(FHG cos 26.57)(3) = -9RE
FHG = -3.35RE
-3.35(0.25) = -0.84
118
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
1 kN
Consider the section to the left
RA
RA
x
1
0.75
0.5
0.25
FBC
FBG
FHG
FHG x
-0.84
+ ΣMB = 0:
(FHG cos 26.57)(3) = -3RA
FHG = -1.12RA
-1.12(0.5) = -0.56
-1.12(0.25) = -0.28
119
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
Influence Line for FBG
1 kN
Consider the section to the right
RE
x
0.5
0.75
0.25
1
FBG x
RE
FBC
FBG
FHG
26.57o
FHG x
-0.84
-0.56
-0.28
ΣFy = 0:+
-FBG cos 33.69
- FHGsin26.57 + RE = 0
FHG = +1.2RE - 0.54 FHG
33.69o
1.2(0.25)-0.54(-0.84) = 0.75
120
FHG x
-0.84
-0.56
-0.28
ΣFy = 0:+
RA + FBG cos33.69
+ FHG sin 26.57 = 0
FBG = -1.2RA - 0.54FHG
A
B C
E
G
H
3 m
D
F
3 m 3 m 3 m 3 m
1.5 m
1 kN
RA
FBC
FBG
FHG
Consider the section to the left
RA
x
1
0.75
0.5
0.25
FBG x
0.75
-1.2(0. 5)-0.54(-0.56) = -0.30
-1.2(0. 25)-0.54(-0.28) = -0.15

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influence line

  • 1. 60 A B C D EF GH Influence Line for Girder • Forces Apply to the Girder (b/L)P1 (a/L)P1 P2 P1 a b P2 L A B P1 D P2 A B C D F GH
  • 4. 63 A F GH • Shear L a b b b 1 0.5 0.5 1 1 VC VC VC x 2b/L -(a+b)/L 1 C
  • 5. 64 A F GH L VCD VCD 1 0.5 0.5 1 0.5 0.5 VCD x -a/L b/L a b
  • 6. 65 A C F GH • Bending Moment L a b ab/L 1 0.5 0.5 MC x 1 1 MC MC C
  • 7. 66 A B C D E F GH L MF x 1 0.5 0.5 1 0.5 0.5 MF MF a b ab/L
  • 8. 67 Example 6-5 Draw the influence for - the Reaction RG and RF - Shear VCD - the moment MC and MH 1.5 m 1.5 m A C D H F 3 m 3 m 3 m 3 m G
  • 9. 68 1 RG x RG 1.333 0.667 0.333 1.5 m 1.5 m A H F 3 m 3 m 3 m 3 m G
  • 10. 69 RF x RF 1 0.667 0.333 -0.333 1.5 m 1.5 m A H F 3 m 3 m 3 m 3 m G
  • 11. 70 1.5 m 1.5 m A H F 3 m 3 m 3 m 3 m G VCD x VCD VCD 1 0.5 0.5 4.5/9 -4.5/9 0.333 -0.333 0.333 C D
  • 12. 71 1.5 m 1.5 m A H F 3 m 3 m 3 m 3 m G MC MC 1 1 MC x (3)(6)/9 = 2 -2 1 C
  • 13. 72 MH MH 1 0.5 0.5 MH x (4.5)(4.5)/9 = 2.25 1.51.5 -1.5 1.5 m 1.5 m A H F 3 m 3 m 3 m 3 m G
  • 14. 73 Example 6-6 Draw the influence line diagrams of girder for - the reaction at C and G, - shear at E and H, - bending moment at H. 2 m A GB 6 @ 4 m = 24 m C D E FH
  • 16. 75 A GB 6 @ 4 m = 24 m C D E FH 2 m RG RG 1 1 1 0.25 0.50 0.75 -0.25
  • 17. 76 A GB 6 @ 4 m = 24 m C D E FH 2 m VE 1 1 1 1 VE VE 8/16 = 0.5 -8/16 = 0.5-0.25 0.250.25 8 m 8 m
  • 18. 77 A GB 6 @ 4 m = 24 m C D E FH 2 m 6/16 = 0.375 -10/16 = 0.625 VH 1 1 VH VH 1 0.5 0.5 -0.25 0.250.25 -0.50 10 m 6 m
  • 19. 78 A GB 6 @ 4 m = 24 m C D E FH 2 m MH 1 1 1 0.5 0.5 MH MH (10)(6)/16 = 3.75 1.50 2.50 -1.50 3 10 m 6 m
  • 20. 79 Draw the influence for - the Reaction RG and RH - Shear VC and VCD - the moment MC, MD, and MF and determine the maximum for - the Reaction (RG)max and (RH)max - Shear (VCD)max due to - a uniform dead load 2 kN/m - a uniform live load 5 kN/m - a concentrated live load 50 kN Example 6-7 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH
  • 21. 80 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH RG 1 0.5 0.5 10/14 6/14 2/14 1/14 RG 11 RH
  • 22. 81 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D E F GH 1 0.5 0.5 RGRH RH 1 12/14 8/14 4/146/14
  • 23. 82 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH VC VC 1 0.5 0.5 VC x 8/14 -6/14 1 1 1 -2/14 4/14 -1/14
  • 24. 83 -8/14 6/14 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH VF VF 1 0.5 0.5 1 0.5 0.5 VCD x -1/14 -2/14 -6/14 4/14
  • 25. 84 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH (6)(8)/14 = 3.43 1 0.5 0.5 MC x (4/8)(3.43) (2/6)(3.43) 1 1 MC MC
  • 26. 85 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D E F GH 1 0.5 0.5 1 1 MD x (10)(4)/14 = 2.86(6/10)(2.86) (2/10)(2.86) MD MD
  • 27. 86 (8)(6)/14=3.428 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D F GH MF x 1 0.5 0.5 1 0.5 0.5 2.285 2.571 0.857 0.429 MF MF
  • 28. 87 [0.5×4 (2/14)] + [(0.5)(2/14 + 1)(12) = 7.143 RG 1 10/14 6/14 2/14 1/14 Maximum Reaction 2 kN/m 5 kN/m 50 kN (RG)max = (2)(7.143) + (5)(7.143) + (50)(1) = 100 kN 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D E F GH
  • 29. 88 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D E F GH (0.5)(16)(12/14) = 6.857 RH 12/14 8/14 4/146/14 Maximum Reaction 2 kN/m 5 kN/m 50 kN (RH)max = (2)(6.857) + (5)(6.857) + (50)(12/14) = 90.86 kN
  • 30. 89 2 m 2 m 4 m 4 m 4 m 2 m 2 m A B C D E F GH + (0.5)(5.6)(4/14) = + 0.8 -[0.5(4)(2/14) + 0.5(2/14) + (6/14)(4) + 0.5(2.4)(6/14)] = -1.943 2.4 m VCD -1/14 -2/14 -6/14 4/14 Maximum Shear 2 kN/m 5 kN/m 50 kN (VCD)max = (2)(-1.943 + 0.8) (5)(-1.943) + (50)(-6/14) = -33.43 kN C D
  • 31. 90 SP 6-1 Draw the influence line for -the reaction at support A and D -the shear and moment at E - the moment at B and C . 2 m 2 m 2 m 2 m 2 m A B E C D
  • 32. 91 Influence Line for Trusses RA x 1 RE x 1 (3/4) (2/4) (1/4) (2/4) (3/4) (1/4) A B C E GH D F 4 @ x m h
  • 33. 92 A B C E GH D F 4 @ x m h 1 kN Consider the section to the right FCB RE FGB FGH FBC x (2x/h)(1/4) + ΣMG = 0: 0)()2( =− hFxR BCE EBC R h x F 2 = RE x 1 (2/4) (3/4) (1/4)
  • 34. 93 A B C E GH D F 4 @ x m h 1 kN Consider section to the left FHG FBC RA FBG + ΣMG = 0: 0)2()( =− xRhF ABC ABC R h x F 2 = FBC x (2x/h)(1/4) RA x 1 (3/4) (2/4) (1/4) (2x/h)(1/4) (2x/h)(2/4)
  • 35. 94 Determine the maximum force developed in member BC , BG, and CG of the truss due to the wheel loads of the car. Assume the loads are applied directly to the truss. the wheel loads of the car 4 kN 1.5 kN2 m Example 6-8-1 A B C E GH 4 m D F 3 m 3 m 3 m 3 m
  • 37. 96 A B C E GH 4 m D F 3 m 3 m 3 m 3 m Influence Line for FBC 1 kN Consider the section to the right FBC = (6/4) RE = 1.5 RE FCB RE FGB FGH RE x 0.5 0.75 0.25 1 FBC x 1.5(0.25) = 0.375 + ΣMG = 0:
  • 38. 97 A B C E GH 4 m D F 3 m 3 m 3 m 3 m 0.375 1.5(0.5) = 0.75 1 kN Consider the section to the left FHG FBC RA FBG RA x 1 0.75 0.5 0.25 FBC = 1.5 RA FBC x 0.375 + ΣMG = 0:
  • 39. 98 A B C E GH 4 m D F 3 m 3 m 3 m 3 m RE x 0.5 0.75 0.25 1 Influence Line for FBG 1 kN Consider the section to the right ΣFy = 0 ; FBG cos θ = RE FGH FGB FCB RE θ FBG = 1.25 RE FBG (4/5) = RE1.25(0.25) = 0.3125 FBG x
  • 40. 99 A B C E GH 4 m D F 3 m 3 m 3 m 3 m 1 kN Consider the left hand ΣFy = 0 ; FBG cos θ + RA = 0 RA x 1 0.75 0.5 0.25 FHG FBC RA FBG θ 0.3125 FBG x FBG = -1.25 RA FBG (4/5) = -RA -0.3125 -1.25(0.5) = -0.625
  • 41. 100 A B C E GH 4 m D F 3 m 3 m 3 m 3 m FCG x Influence Line for FCG 1 kN 0 1 kN 0
  • 42. 101 A B C E GH 4 m D F 3 m 3 m 3 m 3 m FCG x 1 kN 1 1
  • 43. 102 A B C E GH 4 m D F 3 m 3 m 3 m 3 m (FBC)max by Loads (FBC)max = (4)(0.75) + (1.5)(0.5) = 3.75 kN (T) 0.375 0.75 FBC x 0.375 4 kN 1.5 kN2 m 0.5
  • 44. 103 A B C E GH 4 m D F 3 m 3 m 3 m 3 m (FBG)max by Loads (FBG)max = (4)(-0.625) + (1.5)(-0.417) = -3.126 kN (C) FBG x -0.3125 0.3125 -0.625 4 kN 1.5 kN2 m -0.417
  • 45. 104 A B C E GH 4 m D F 3 m 3 m 3 m 3 m (FCG)max by Loads FCG x 1 0.333 (FCG)max = (4)(1) + (1.5)(0.333) = 4.50 kN (T) 4 kN 1.5 kN2 m
  • 46. 105 Draw the influence line for FBC , FBH,and FCH. Example 6-8-2 A B C E HI 4 m D F 3 m 3 m 3 m 3 m GJ
  • 48. 107 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJInfluence Line for FBC 1 kN Consider the section to the right FBC = (6/4) RE = 1.5 RE FCB RE FHB FHI RE x 0.5 0.75 0.25 1 FBC x 1.5(0.25) = 0.375 + ΣMH = 0:
  • 49. 108 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJ 0.375 1.5(0.5) = 0.75 1 kN Consider the section to the left FHI FBC RA FBH RA x 1 0.75 0.5 0.25 FBC = 1.5 RA FBC x 0.375 + ΣMH = 0:
  • 50. 109 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJ RE x 0.5 0.75 0.25 1 Influence Line for FBH 1 kN Consider the section to the right ΣFy = 0 ; FBH cos θ = RE FHI FBH FCB RE θ FBH = 1.25 RE FBH (4/5) = RE1.25(0.25) = 0.3125 FBH x
  • 51. 110 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJ 1 kN Consider the section to the left ΣFy = 0 ; FBH cos θ + RA = 0 RA x 1 0.75 0.5 0.25 FHI FBC RA FBH θ 0.3125 FBH x FBH = -1.25 RA FBH (4/5) = -RA -0.3125 -1.25(0.5) = -0.625
  • 52. 111 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJ FCH x Influence Line for FCH 1 kN FGH FCH FCB RE x 0.5 0.75 0.25 1 RE ΣFy = 0 ; FCH = -RE -0.25
  • 53. 112 A B C E HI 4 m D G 3 m 3 m 3 m 3 m FJ FCH x 1 kN FGH FCH FCB RA ΣFy = 0 ; FCH = RA -0.25 RA x 1 0.75 0.5 0.25 0.5 0.25
  • 54. 113 Draw the influence line for FBC , FBG,and FHG. Example 6-8-3 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m
  • 56. 115 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m Influence Line for FBC 1 kN Consider the section to the right FBC = (6/4.5) RE = 1.33 RE RE x 0.5 0.75 0.25 1 FBC x 1.33(0.25) = 0.333 + ΣMG = 0: RE FBC FBG FHG
  • 57. 116 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m 1 kN Consider the section to the left FBC = (6/4.5) RA = 1.33 RA FBC x 1.33(0.25) = 0.333 + ΣMG = 0: RA RA x 1 0.75 0.5 0.25 FBC FBG FHG 1.33(0.5) = 0.667 1.33(0.25) = 0.333
  • 58. 117 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m Influence Line for FHG 1 kN Consider the section to the right RE x 0.5 0.75 0.25 1 FHG x + ΣMB = 0: RE FBC FBG FHG 26.57o (FHG cos 26.57)(3) = -9RE FHG = -3.35RE -3.35(0.25) = -0.84
  • 59. 118 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m 1 kN Consider the section to the left RA RA x 1 0.75 0.5 0.25 FBC FBG FHG FHG x -0.84 + ΣMB = 0: (FHG cos 26.57)(3) = -3RA FHG = -1.12RA -1.12(0.5) = -0.56 -1.12(0.25) = -0.28
  • 60. 119 A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m Influence Line for FBG 1 kN Consider the section to the right RE x 0.5 0.75 0.25 1 FBG x RE FBC FBG FHG 26.57o FHG x -0.84 -0.56 -0.28 ΣFy = 0:+ -FBG cos 33.69 - FHGsin26.57 + RE = 0 FHG = +1.2RE - 0.54 FHG 33.69o 1.2(0.25)-0.54(-0.84) = 0.75
  • 61. 120 FHG x -0.84 -0.56 -0.28 ΣFy = 0:+ RA + FBG cos33.69 + FHG sin 26.57 = 0 FBG = -1.2RA - 0.54FHG A B C E G H 3 m D F 3 m 3 m 3 m 3 m 1.5 m 1 kN RA FBC FBG FHG Consider the section to the left RA x 1 0.75 0.5 0.25 FBG x 0.75 -1.2(0. 5)-0.54(-0.56) = -0.30 -1.2(0. 25)-0.54(-0.28) = -0.15