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1
ENCE717 – Bridge EngineeringBridge Analysis
Chung C. Fu, Ph.D., P.E.
(http: www.best.umd.edu)
Introduction – Bridge Analysis
7. Numerical Methods (3.0)
Numerical Methods – 3D FEM
Advantages and Disadvantages of Grid Analysis
Advantages and Disadvantages of 3D FEM Analysis
3D FEM Example
Numerical Methods – Elastic Stabili ty (3.2.8 & 14.0)
Numerical Methods – Creep and Shrinkage Analysis (3.3
& 5.2)
Numerical Methods – Influence Surface (3.4)
Numerical Methods – 3D FEM
Numerical Methods –
Applications in Bridge Analysis
Issues include:
1) what types of element a bridge model should be
used;
2) when a 2D model is sufficient and when a 3D
model is necessary; and
3) how to correctly interpret FEM results from bridge
engineering perspectives, especially when a
bridge is modeled as plate or shell elements.
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Numerical Methods –
Elements used in Bridge Analysis
In general, truss, frame(/beam) and shell(/plate) elements can
cover most bridge analyses; Truss element is also called link element. Bridge bearings,
hangers, prestress tendons, cables, and etc. can be modeled
as truss elements.
In line models, girders, stringers, diaphragms, pylons,
columns, piers, and etc. are usually modeled as frame
elements.
Shell element combines in-plane stress/strain behaviortogether with bending of a plate, either as a thin plate or a
thick plate.
Numerical Methods – Advantages and
Disadvantages of Grid Analysis
Middle- and short-span girder bridges, an intermediate model,
or the so-called grid model, is widely used;
Grid model: each node of an element has only vertical
displacements, bending rotation and torsional displacements.
Element internal forces contain bending and torsional
moments plus shear, accordingly;
• Some behaviors of a wide thin walled box girder, such as
warping when torsion is restrained, distortion when insufficient
diaphragm is used and shear lagging due to longitudinal shear
deformations of flanges, cannot be represented in a gridmodel;
Numerical Methods – Advantages and
Disadvantages of 3D FEM Analysis (1)
For truss or frame elements, internal forces output from FEM
analyses can be used directly for engineering design and
code checks;
For shell elements, the original FEM results are not
meaningful and cannot be used in design or code because the
stresses in each element’s local coordinate system.
•Shell elements of a web in a box girder and vertical shear stresses
Numerical Methods – Advantages and
Disadvantages of 3D FEM Analysis (2)
a) Curves – axial stresses distribution
from a shell element model
b) Straight lines – axial stresses
distribution re-computed from beam
bending theory by using equivalentinternal forces obtained from stress
integration
•Stresses along horizontal direction after unfolded
•Major principal stresses
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3D FEM Example - MD28 in Tuscarora 3D FEM Example - MD28 in Tuscarora
Pattern: Allcracks are
initiated from
skewed
abutment and
normal to the
abutment line.
Then, turnparallel to the
girder lines
3D FEM Analysis - 55’ Span, 15 Skew
• Little difference
4 Skewed Ties at 5’ and 20’
from Supports
2 Staggered Ties (Full-
Width)
3D FEM Analysis - 55’ Span, 30 Skew
• Skewed ties show significant improvement
4 Skewed Ties at 5’ and 20’
from Supports
2 Staggered Ties (Full-
Width)
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Numerical Methods – Elastic Stability Numerical Methods – Elastic Stability
Figure 14.12 – The first mode of a simple arch
bridge bulking, out-of-plane ( 408.516
Elastic Stabili ty Example
Figure 14.13 – The second mode of a
simple arch bridge bulking, out-of-plane
( 1046.208
Figure 14.14 – The third mode of a
simple arch bridge buckling, in-plane
( 1259.367
Numerical Methods –
Creep and Shrinkage Analysis
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Numerical Methods –
Creep and Shrinkage Analysis
Figure 3.13 – Moment distribution of a 3‐span continuous bridge built span by span,
without consideration of concrete creep considered (kN∙M )
Figure 3.14 – Moment distribution of a 3‐span continuous bridge 8 years after built span
by span, with consideration of concrete creep considered (kN∙M )
Creep and Shrinkage Typical Time Curve (1)
4.04.0
3.53.5
3.03.0
2.52.5
2.02.0
1.51.5
3.723.72
3.033.03
2.572.57
2.222.22
2.002.00
1.701.70
1.441.44
1.01.0
0.50.5
00 33 77 1414 21212828 42425656 33 44 55 66 99 11 1.51.5 22 33 55
DaysDays MonthsMonths YearsYears
1 1 . . 2 2
0 0
1 1 . . 0 0
7 7
1 1 . . 0 0
0 0
0 0 . . 9 9
6 6
0 0 . . 9 9
1 1
0 0 . . 9 9
4 4
0 0 . . 9 9
0 0
0 0 . . 8 8
8 8
tt
DURATION OF LOADINGDURATION OF LOADING
T T O O
T T A A L L
E E L L A A S S T T I I C C
A A N N D D
C C R R E E E E P P
S S T T R R A A I I N N
4.0
3.5
3.0
2.5
2.0
1.5
3.72
3.03
2.57
2.22
2.00
1.70
1.44
1.0
0.5
0 3 7 14 21 28 42 56 3 4 5 6 9 1 1.5 2 3 5
Days Months Years
1 . 2
0
1 . 0
7
1 . 0
0
0 . 9
6
0 . 9
1
0 . 9
4
0 . 9
0
0 . 8
8
t
DURATION OF LOADING
T O
T A L
E L A S T I C
A N D
C R E E P
S T R A I N
Creep and Shrinkage Typical Time Curve (2) Moment due to Creep
Free Cantilever Statical SystemFree Cantilever Statical System
Changed Statical System (Midspan Continuous)Changed Statical System (Midspan Continuous)
MMFinal (t)Final (t)
½L½L ½L½L
MMII M =M =II
FixedFixed FixedFixed
qLqL22
88
MMIIIIM =M =IIII
qLqL22
1212qLqL22
2424
MMIIII
MMII
MMcr (t)cr (t)
Free Cantilever Statical System
Changed Statical System (Midspan Continuous)
MFinal (t)
½L ½L
MI M =I
Fixed Fixed
q
qL2
8
MIIM =II
qL2
12qL2
24
MII
MI
Mcr (t)
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Structural Concrete subjected to Creep
elel (t )(t )00
cr cr (t )(t )
PP PP
PPef ef PPef ef
Cantilever BeamCantilever Beam
Simple BeamSimple Beam
elel ( )( )tt 00cr cr (t )(t )
el (t )0
cr (t )
P P
Pef Pef
Cantilever Beam
Simple Beam
el ( )t 0cr (t )
Structural Concrete subjected to Creep
PP
Post-Tensioned BeamPost-Tensioned BeamPP
PP PP
PPef ef
PPef ef
elel (t )(t )00
elel (t )(t )00
elel (t )(t )
PT TendonPT Tendon
P
Post-Tensioned BeamP
P P
Pef
Pef
el (t )0
el (t )0
el (t )
PT Tendon
Collapse of Palau Bridge due to CreepNumerical Methods –
Influence Surface
Figure 3.19 – Influence surface of a tied arch bridge
For spatial bridge analyses, traditional lateral load distribution theories,
influence lines and simplified calculation methods are substituted by
spatial structural analyses and influence surface loading.