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Influencelines Lineas de Influencia

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INFLUENCE LINES IN CONTINUOUS BEAMS

A
Span No. 1 2 3 4
Span
Number of Spans ( <=10 ): 4 Length: 60 90 50 40
Stiffness
No. of Sections in Span (<=30): 10 EI 0 1000
60 1000
150 1000
200 1000
240
0 0 0 0 0

● Internal Forces

● Support Reactions Pier No. 4


40

Continuous Beam Influence Lines


1
0.9
0.8
0.7
0.6
0.5
0.4
0.3
0.2
0.1
0
0 50 100 150 1
200

Reaction
RESULTS Maximum Value: 1 0
X-Global Span X-Local Reaction Minimum Value: -0.3118 0
0 1 0 0 Positive Area: 56.4353 0
0.00001 0.00001 2.45E-08 Negative Area: -17.167 0
6 6 0.014533 Total Area: 39.2687 0
12 12 0.028184
18 18 0.040075
24 24 0.049323
30 30 0.055048
36 36 0.056369
42 42 0.052405
48 48 0.042277
54 54 0.025102
60 60 0
60 2 0 0
69 9 -0.05252
78 18 -0.11626
87 27 -0.18265
96 36 -0.24309
105 45 -0.289
114 54 -0.31179
123 63 -0.30287
132 72 -0.25366
141 81 -0.15556
150 90 0
150 3 0 0
155 5 0.113114
160 10 0.24026
165 15 0.375085
170 20 0.511231
175 25 0.642346
180 30 0.762072
185 35 0.864056
190 40 0.941942
195 45 0.989375
200 50 1
200 4 0 1
204 4 0.97873
208 8 0.932598
212 12 0.864366
216 16 0.776797
220 20 0.672653
224 24 0.554697
228 28 0.425692
232 32 0.288399
236 36 0.14558
240 40 0
240
0 240
0 240
0 240
0 240
0 240
0

200

0
0
0
0
0
Bending Moment Analysis Option
Shear Force
Stiffness Matrix [d] Deflections
Reactions
1 2 3
1 0.05 0.015 0
2 0.015 0.046667 0.008333
3 0 0.008333 0.03

Load Vector [Dp]


Point load in span 4 Moment in simple beam under Point load:
Distance from the beginning of span: 40 Msimple= 0
-X(L-X)/(6LEI): 0

[Dp] 0 0 0
1 2 3 4 5 6 7 8 9
0 0 0 #N/A #N/A #N/A #N/A #N/A
0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0
0 0 0 0 0 0 0 0 0
0 0 0 0 1 0 0 0 0
0 0 0 0 1 0 0 0 0

Section in span 4
Distance from the beginning of span: 40

Mp 1 2 3
0 0 0 0

M= 0

Vp 1 2 3
-1 0 0 0

V= -1

Simple span moments in statically determined structure


1 2 3 4
0 0 0 0

R=

Defined Ranges
D_IL =OFFSET(X_Global,,5)
deltaP =OFFSET(p1x10,0,0,1,Nspans-1)
DiagramLink =Input!$I$13
EI =Input!$G$5:$P$5
InfluenceLine =CHOOSE(DiagramLink,M_IL,V_IL,D_IL)
L =Input!$G$4:$P$4
LoadSpan =Solver!$E$17
LoadX =Solver!$E$18
M_IL =OFFSET(X_Global,,3)
m10x10 =Solver!$B$6:$J$14
matrix =OFFSET(m10x10,0,0,Nspans-1,Nspans-1)
Moment =Solver!$B$30
Msimple =Solver!$H$18
Msup =Solver!$B$22:$J$22
Nsections =Input!$D$5
Nspans =Input!$D$4
p1x10 =Solver!$B$21:$J$21
SectionSpan =Solver!$E$24
SectionX =Solver!$E$25
Shear =Solver!$B$35
V_IL =OFFSET(X_Global,,4)
X =Solver!$E$18
X_Global =OFFSET(X_Global_Big,,,COUNT(X_Global_Big))
X_Global_Big =Input!$A$18:$A$848
XGLOBAL =Input!$A$18:$A$61
XLoc1 =Input!$C$17
2 Piers
1
2
3
4
5
6
7
8
9
10
11

am under Point load:

10 11 Piers
#N/A Msup
0 0 Msup/Li-1
0 0 Msup/Li
0 0 Reaction Msup/L
0 0 Reaction in statically determined structure
0 0 Reaction Total

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