Detailed calculations of main girder by means
of grillage FEM model Bridges CE – educational materials for design exercise
Dr Mieszko KUŻAWA Wrocław, May 4th, 2016
Faculty of Civil Engineering
Content of project report
1. Design assumptions
a) Objective of the project
b) Basic assumption concerning the design structure
• Theoretical length of span
• Type of construction of superstructure,
• Width of the roadway,
• Width of the sidewalks,
• Material of structure,
c) Scope of the project
• Range of conceptual design,
• Range of detailed design
d) Codes, regulations and literature
2. Technical description of entire structure
3. Initial calculations of main girder
4. Detailed calculations of main girder of superstructure
• Cross section
• Lateral view / Longitudinal view and static system
A B C D
Basic dimensions of analysed bridge superstructure
General geomerty modeling assumptions
• Model class (e1,s3) is applied – grillage system conssited of 1-dimensional bar elements in 3-dimensional space,
• Longitudinal elements are intended to represent T-shape main girder (stiffness of girder web as well as concrete deck is included),
• Transversal elements are supposed to model cross beams and concrete deck in transversal direction to longitudinal span axis.
• 2-dimensional shell elements are used to projecting the loads from deck surface to the bars.
• Geometrical characteristics of particular elements of FEM model are calculated according to centroid of its the cross-section and than offset vertical offset is applied for selected bar elements to properly represent stiffness of span.
• Geometrical characteristics of particular elements do not include the impact of reinforcing steel.
4.1. FEM model of bridge superstructure
Discretization of multi-girder monolithic RC
superstructure for grillage FEM model
• The definition of cross-sections
Main menu bar -> Geometry -> Properties - > Sections->
New section definition
Torsional stiffness of elements of superstructure
Graphics of geometry model
Properties of elements cross sections
Choose element-> clik left mouse button -> Object properties
Limitations of applied modeling and analysis approach
• FEM model is evaluated using Linear Elastic type of Analysis.
• Cracking effects of concrete on bending stiffness changes of subsequent sections of main girder as well as on redistribution of internal forces is neglected.
• Effective width effect aiming to represent flow of longitudinal axial forces in concrete deck is not considered.
Flow of compressive forces stream
4.2. Lateral load distribution
KA,A
KA,B
KA,C KA,D
P = 1
max min
Influence Line for Lateral Load Distribution ILLLD
In initial calcuations characteristic values of ILLLD „i” ordinates were calculated using Courbon formula:
Ay
yy
nK
i
ji
ji
2,
1
where:
• yi – denotes location of girder,
• yj – denotes location of P force, • A=0 – parameter relataed to torsional stiffness
ILLLD „i” [-] – function specifying action of unit
force, located in subsequent points of cross
section of span, on investigated girder „i”.
Cross-sectional deformation after loading
Symmetrical part of the cross-sectional deformation after loading
Asymmetric part of the cross-sectional deformation after loading
Źródło [5]
• Principle of the Courbon method
a) The cross section of the span has a vertical axis of symmetry.
b) Beam bending stiffness and their spacing are equal.
c) Problem is static, linear-elastic, the principle of rigid cross-section is valid.
d) In the analyzed cross-section of the span infinitely rigid cross member is located.
e) Mechanical model allowing to analyze the behavior of the cross-section of the span subjected to P force is assumed in the form of an infinitely stiff beam with elastic Winkler-type supports.
• Symmetrical part of the cross-sectional deformation
The cross-section has moved evenly (translation) as a rigid body with a vector 𝑢(𝑠) which caused equal reactions in all elastic supports.
Conditions of equilibrium:
Symmetrical part of the cross-sectional deformation after loading
0
0
0
0
)(
M
H
n
PV s Symmetrical part of the cross-sectional deformation after
loading in real multi-girder bridge superstructures
ILLLD „A” [-]
• Asymmetric part of the cross-sectional deformation
As a result of infinitely rigid cross beam the cross-section of the span rotated as a rigid body by an angle φ.
The rotation center is located on the vertical axis of symmetry of the system.
• Conditions of equilibrium:
Assuming hinged connection of girders with the cross beam!
• Deformation compatibility condition:
Asymmetric part of the cross-sectional deformation after loading
xPbbM
H
V
aa
1
)(
12
)(
20 20
0
0
1
)(
1
2
)(
2
1
)(
1
2
)(
2
bbb
u
b
u
tgaa
aa
Finally, the formula for reaction in edge springs if as follows:
2
2
2
1
2)(
22 bb
bxPa
• In presented example rigid connection of girders with the cross beam can be assumed as well.
• Rotation of the cross beam will cause, in addition to the deflection, also the torsion of all main girders of φ angle.
• Conditions of equilibrium:
SSi
s
i MMyRM
H
V
60
0
0
1
0
Asymmetric part of the cross-sectional deformation after loading
y
z
u
• Uniform (pure) Torsion – ends are free to wrap
• Non-Uniform Torsion – warping deformation is constrained
ω11
ω21
ω31 ω41
1 2 3 4
1 2
3 4
Analysed girder
ωij – denotes deflection of node „i” caused by load located at node „j”
Main menu bar -> Loads Types -> Add Load Case
Main menu bar -> Loads -> Loads Definition - > Node Tab
Cross beam
• Transversal deformation of analysed cross section
• Deformation of multi-girder bridge superstructure
1 2 3 4
1 2 3 4
ω11
ω21
ω31 ω41
ω12 ω22
ω32 ω42
P1 • ω12 = P2 • ω21
P1 = 500 kN
P2 = 500 kN
On the basis of Maxwell-Betii reciprocal work theorem:
ω12 = ω21
1 2 3 4
ω11/ω0 = kAA
ω21/ω0 = kAB
ω31/ω0 = kAC
ω41/ω0 = kAD
P1 = 1
A B C D
kij – denotes ordinate of ILLLD [-] function for girder „i” when load is located above girder „j”
• Obtaining of Influence Line of Lateral Load Distribution (ILLLD) function for girder A
ω0 = ω11 + ω21 + ω31 + ω41
ILLLD „A” [-]
max min
A B C D
• Applied load pattern it across the width of the span
Exemplary combination of live loads in cross section
max
min
35,1F
35,1F
Analysis of influence lines
of bending moments
4.3. Influence lines of global internal forces along
investigated girder
• Load case for maximum bending moment in section x/Lt = 0.9 of girder A
Exemplary load pattern for extreme values of bending moments in selected section of girder A
γf max
γf max
γf max
γf min γf min
γf min
ILL
LD
„A
” [
-]
• Load case for minimum bending moment in section x/Lt = 0.9 of girder A
Extreme values of bending moments in selected sections of girder A
γf min
γf min
γf min
γf max γf max
γf max
ILL
LD
„A
” [
-]
Analysis of
influence lines
of shear forces
Girder A
ILL
LD
„A
” [
-]
UDL loads patterns for unfavorable
possible load combinations acting on
girder A
IL M [m] / IL V [-]
MIN width
MAX width
A1 A2 A3 A4 A5 A7
A6 A8
Selected simple load cases of UDL dead loads applied in MAX width
Selected combinations of simple load cases of UDL dead loads applied in
MAX width
4.4. Loads
a) Dead loads
• Uniformly Distributed Loads (UDL), [kN/m2]
• Path Loads [kN/m] – cross beams:
characteristic value: Gk
design values: Gmax, Gmin
Bridge deck equipment
Left sidewalk
• characteristic value
gk
• design value
gmax, gmin
Bridge superstructure web of main girders + deck slab
Roadway
• characteristic value
gk
• design value
gmax, gmin
Right sidewalk
• characteristic value
gk
• design value
gmax, gmin
Ca
rria
ge
wa
y w
idth
– w
Notional
Lane
Nr.
Notional
Lane
Nr.
Notional
Lane
Nr.
Remaining
area
Remaining
area
Load Model LM1:
• set of concentrated loads [kN] TS
• UDL [kN/m2] q
which cover most of the effects of the traffic of lorries and cars. This model should be used for general and local verifications.
ikiq Qikiq Q
ikqi q
kq q11
kq q22
rkqr q
b) Live loads
• Crowd of pedestrians – UDL [kN/m2] p
• Application of moving Tandem System (TS) in FEM model
Exemplary distribution of bending moments [kNm] in main girders corresponding to selected location of TS
4.4. Internal forces
a) Selected diagrams of M and V for selected load combinations for
different actions (dead loads, UDL live loads, TS moving load)
Show exemplary distributions of analysed internal forces (M & V) for 3x3 selected
combinations of investigated loads - 3 for dead loads + 3 for UDL live loads + 3 for TS
moving load.
b) Partial envelopes of M and V corresponding to combinations for:
• Dead loads g,
• UDL live loads q & p
• TS live loads.
Show 3 partial envelopes of analysed internal forces (M & V) - for dead loads +
for UDL live loads + for TS moving load.
Exemplary envelope of bending moments [kNm] in main girders corresponding to prescribed route of TS
Route of TS
b) Full envelopes of M and V
Envelope of bending moments M [kNm] in analysed main girder
Envelope of shear forces V [kNm] in analysed main girder
Thank you for your
attention!