12 influence line diagrams - ii
TRANSCRIPT
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CED. UET. Taxila 1
Influence Line Diagrams-II
Theory of Structures - I
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Contents
Qualitative Influence Lines
Influence lines for Girders
Influence Lines for Trusses
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Qualitative Influence Lines
In 1886, Heinrich Muller-Breslau developed a technique for rapidly constructing influence lines.
It states
“the influence line for a function (reaction, shear or moment) is to be the same scale as the deflected shape of the beam when the beam is acted upon by that function”
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In order to draw deflected shape properly, the capacity of the beam to resist the applied function must be removed so the beam can deflect when the function is applied.
A
A
Ay
Ay
x
Influence line for Ay
REACTION
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CSHEAR
Vc
Vc
Deflected Shape
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CMOMENT
Deflected Shape
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Proof: Reaction
A Ay
x
1y’
1
y
Work = Force . Displacement
= Moment . Rotational displacement
C C
'
;1
0'.1
yy
y
yyy
A
A
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C
SHEAR
Vc
Vc
'
;1
0'.1
yc
y
yyc
V
V
y’
1
1
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C
MOMENT
Deflected Shape
Mc Mc
y’
1
1'
;1
0'.1
yc
yc
M
M
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Example 6-9
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Practice Problems
Example 6-9 to 6-12
Chapter 6
Structural Analysis by R C Hibbeler
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Influence Lines for Girders
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Unit load on the slab is transferred to the girder only at points where it is in contact with the floor beams.
A, B, C and D are panel points and the region between these points is known as panel.
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BP
FFV
sdFdFM
1
1 )(
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Moment will depend on where the point p is located but shear will remain same in the whole panel.
Influence line for shear in floor girders are specified for panels in the girder and not specific points along the girder.
Shear is referred to panel shear.
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Since the girder is affected only by the loadings transmitted by the floor beams, the unit load is generally placed at each floor-beam location to establish the necessary data used to draw the influence line.
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Example 6-13
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x VCD
0 0.333
10 0
20 -0.333
30 0.333
40 0
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Practice Problems
Example 6-13 to 6-14
Chapter 6
Structural Analysis by R C Hibbeler
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top cord
deck
sway bracing
top lateralbracing
stringers
portal end post
portalbracing
panel
floor beam
bottom cord
Truss
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Example 6-15
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x FGB
0 0
10 0.354
20 -0.707
30 -0.354
40 0
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Practice Problems
Example 6-15 to 6-17
Chapter 6
Structural Analysis by R C Hibbeler
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