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Numerical Investigation of Shear Buckling and Post-buckling of Thin Steel
Plates with FRP Strengthening
Mohamad Alipour1, Alireza Rahai
2, Devin K. Harris
1
1Department of Civil and Environmental Engineering, University of Virginia,
Charlottesville, VA, USA
2Department of Civil and Environmental Engineering, Amirkabir University of
Technology (Tehran Polytechnic), Tehran, Iran
ABSTRACT
The behavior of thin steel plates under shear loading is governed by early diagonal
buckling and subsequent formation of an inclined tension field. This behavior
describes the load carrying mechanism in deep steel plate girder webs and steel plate
shear walls. Traditionally, steel stiffeners are used on the thin plate in some
applications to mitigate out-of-plane buckling and encourage shear yielding, which is
preferable and a more stable and energy-dissipating load carrying mechanism.
However, the cost and practical difficulties associated with welding these stiffeners,
especially on very thin plates and for in-service rehabilitation purposes, are
considered as major drawbacks.
In this paper, the behavior of thin steel plates strengthened with FRP strips was
numerically investigated. FRP wraps were hypothesized to act as an elastic support
for the thin steel plate in the early loading stages and as an auxiliary load transfer path
in the inelastic tension field action. Numerical investigations were carried out using
the finite element method and were divided into two phases; buckling and post-
buckling. Elastic eigenvalue analysis for buckling and full inelastic analysis with
geometrical and material nonlinearity for the post-buckling phase were carried out.
FRP fracture and damage were incorporated in the models. Optimum angle of FRP
fibers was studied both for buckling mitigation and post-buckling behavior
enhancement. A number of FRP strengthening configurations together with a range of
common FRP materials were also employed in the analyses. It was concluded that
bonding FRP patches on the steel plate can effectively encourage behavior
enhancements, especially given appropriate configuration and material properties.
KEYWORDS:
FRP Composites, Shear Buckling, Post Buckling, Steel Plate Shear Wall, Finite
Element Method (FEM)
INTRODUCTION
Steel and Composite Plate Shear Walls
Steel plate shear wall (abbreviated hereafter as SPSW) is a lateral load resistant
system composed of a very thin steel plate connected along its four sides to two
columns and two successive beams. SPSW systems are internal structural
components used to resist lateral loads exerted by wind or earthquake. In this
configuration, the plate is loaded in shear and will buckle similar to a slender plate-
girder web. A post-buckling phenomenon will form an inclined tension field which
accounts for the system shear strength as schematically depicted in Figure 1. The
inclined tension strips formed along the dominant principal tension brings to mind the
possibility of using an orthotropic material to strengthen this mechanism.
Figure 1. Inclined tension field in SPSW
Although the system has been proven to have acceptable behavior, a number of issues
emerge. Plate instabilities restrain energy dissipation of the system, which is
demonstrated as pinching of the hysteresis curves. A thick or stiffened plate will yield
in shear which is a more ductile behavior and increases energy dissipation. On the
other hand, buckling-induced out-of-plane deformations of the thin plate may cause
non-structural damage. The inclined tension field also exerts strong inward forces on
beams and columns compared with a thick plate, which yields in shear before
buckling happens.
In a series of cyclic tests on SPSWs, Hatami et al. (2012) and Hatami and Rahai
(2008) tested three one-story SPSW specimens with a 3-mm thick steel plate. In one
of the models, the steel infill plate was made composite by attaching a 0.176-mm
thick CFRP layer using epoxy resin. Comparing the acquired data, the researchers
observed less damage in the retrofitted specimen along with rupture of some bolts
connecting the plate to the boundary members. They also found the FRP layer
responsible for a 37% increase in energy dissipation and 50% in lateral stiffness. It
was stated however that FRP bonding issues had decreased the ductility of the wall by
8%.
Alipour (2010) carried out a numerical investigation on buckling and post-buckling
behavior of FRP-composited steel shear walls. The buckling behavior of a steel infill
plate under pure shear was studied using elastic eigen-value analysis and its post-
buckling behavior was simulated using plasticity for steel and progressive damage for
FRP materials. Both the buckling and post-buckling analyses demonstrated the ability
of the FRP layer to act as an elastic support for the thin steel plate (Alipour, 2010).
Rahai and Alipour (2011) also investigated the fiber direction and geometry for FRP-
composited steel shear walls using the finite element method. It was found that the
optimum direction for fibers is the direction of tension field in the plate as can be
calculated using an energy-based formula (Rahai and Alipour, 2011). Tabrizi and
Rahai studied FRP strips as edge reinforcement for perforated SPSWs and reported
promising results (Tabrizi and Rahai 2011). The current paper builds on the
experiences from these numerical analyses and seeks to investigate the buckling and
post-buckling behavior of the SPSW system with different configurations of FRP
strengthening.
METHOD OF ANALYSIS
In this investigation, a step-by-step numerical analysis was used to describe the global
behavior of a FRP-strengthened SPSW. First, a SPSW was designed according to
AISC provisions. Numerical simulation of the model is then carried out using the
finite element method. Two sets of parametric analyses were then carried out on the
model. First, the shear buckling behavior of the system is studied using linear elastic
eigen-value analyses. Then, a series of nonlinear analyses incorporating steel
plasticity and fracture in FRP materials were conducted.
Model Properties
The steel plate shear wall model of this study was designed using the guidelines
outlined in the AISC seismic provisions for structural steel (AISC 2005). According
to these provisions, the design of a SPSW is considered acceptable when the infill
plate undergoes considerable yielding prior to yielding in the boundary members.
Moreover, with an increase in story drift, yielding must occur in the ends of the
beams to ensure a safe load path for the gravity loads (plastic hinge formation). For
sizing the SPSW sections, a force equal to yield stress of the infill plate was applied
on the beams and columns at the angle of tension field and the boundary frame
members were designed accordingly. Reduced beam section (RBS) connections were
used to reduce the beam plastic moment on the column ends and ensure plastic hinge
formation at the beam ends. The designed SPSW details together with its yield pattern
at 2.5% drift are illustrated in Figure 2. The yield pattern confirms the design being
compliant with AISC provisions.
(a) (b)
Figure 2. SPSW model: (a) designed model details, (b) Yield pattern at 2.5% drift
Finite Element Modeling
Modeling and analysis of the SPSW were carried out using the ABAQUS finite
element package (Abaqus 2008). Models were simulated using 2-dimensional planar
parts and the four-node reduced integration S4R shell elements were used in the
discretization. First, eigen-value buckling analysis was performed on the models to
acquire the buckling shapes of the model and the scaled first buckling mode shape
was introduced to the models to account for the initial imperfections of the plate.
Geometric and material nonlinearity effects were also accounted for.
ASTM A36 and ASTM A572 Gr.50 steel was used for the infill plate and the
boundary frame members respectively. Elastic perfectly plastic stress-strain curves
with Fy=248 MPa for the infill plate and Fy=345 MPa for the frame, and E=209 GPa
and ν=0.3 for the elastic range were used.
Behavior of FRP materials was modeled through elastic behavior, damage initiation
and damage evolution models incorporated in ABAQUS (Abaqus 2008). Orthotropic
elastic behavior was defined through the introduction of elastic coefficients (E11, E22,
G12, ν12) in a local coordinate system with the main 1-direction along the fibers.
Initiation of damage at a specific point is examined through the calculation of Hashin
failure criteria (Hashin and Rotem 1973, Hashin 1980) and once a criterion is met in a
longitudinal, transverse or shear mode, corresponding stiffness was reduced
according to a linear softening rule. The softening rule governing damage evolution
in each failure mode was based on the energy dissipated during fracture (Abaqus
2008).
Four representative FRP materials were selected from the literature: An ordinary
strength and stiffness carbon fiber reinforced plastic (CFRP), a high modulus
composite (HM-CFRP), a high-strength CFRP (HS-CFRP), and finally a glass fiber
reinforced plastic material (GFRP) (Zhao and Zhang 2007, Accord and Earls 2006,
Jones 1999, Buyukozturk et al. 2003). Table 1 shows the mechanical properties of the
FRP materials used in the analysis. In this table, XT and X
C denote the tensile and
compressive strengths in fiber direction, YT and Y
C are for the matrix and S is the
shear strength.
Table 1. Mechanical properties of the materials used
Material
E11 E22 G12 V12 XT X
C Y
T Y
C S
(GPa) (GPa) (GPa) - (MPa) (MPa) (MPa) (MPa) (MPa)
CFRP 146.8 11.4 6.1 0.3 1,730 1,379 66.5 268.2 58.7
HM-CFRP 450 11.4 6.1 0.3 1,540 1,232 66.5 268.2 58.7
HS-CFRP 210 11.4 6.1 0.3 3,200 2,560 66.5 268.2 58.7
GFRP 20.3 11.4 6.1 0.3 855 684 66.5 268.2 58.7
Validation of the Modeling Approach
To verify the modeling of a SPSW and the nonlinearity and post-buckling phenomena
in its behavior, a benchmark case study of a four-story shear wall tested at the
University of Alberta was selected and simulated (Driver et al 1997). Using the same
procedures as those adopted in current paper, shear force of the first story was plotted
against first story lateral displacement and a comparison of the simulated pushover
curve with the laboratory hysteresis curves is shown in Figure 3. The good agreement
achieved demonstrates the ability of the adopted procedures to simulate key features
of SPSW behavior.
(a) (b)
Figure 3. Benchmark case study simulation: (a) FE model, (b) agreement of results
(Driver et al 1997)
To investigate the ability of the finite element procedures used in this study to predict
the interaction of metal plasticity and FRP fracture and damage behaviors, a fiber
metal laminate (FML) specimen found in the literature was modeled and analyzed
(Lapczyk and Hurtado 2007). The FLM consisted of three thin aluminum layers
bonded with two GFRP layers under tension with a central hole as depicted in Figure
4. Lapczyk and Hurtado modeled the FLM using solid elements for the aluminum and
GFRP layers and cohesive elements for the adhesive films, while we used the same
modeling assumptions outlined in the previous section. Results available in the work
by Lapczyk and Hurtado and the simulations of this study demonstrate good
agreement.
(a) (b)
Figure 4. FRP/metal interaction study (a) test setup (b) agreement of results (Lapczyk
and Hurtado 2007)
ANALYSIS RESULTS
This section presents the results of the numerical investigations in two separate
sections. First, the performance in buckling phase studied using eigen-value buckling
analysis is presented. Later, the post-buckling behavior is discussed through inelastic
analyses incorporating steel plasticity and fracture and damage in FRP composites. In
each one of these sections, two strengthening configurations of full-wrap FRP and
diagonal strips are separately studied.
Performance in Buckling Phase
Parametric Study on Full Wrap configuration.
In the first configuration, the 3mm-thick steel plate is fully covered with two 1.5 mm
CFRP layers at (θ/-θ) from horizontal. The angle θ is then gradually incremented and
the shear buckling force per unit edge length is calculated for each angle and plotted
in Figure 5. The optimal fiber angle is 45° as shown by Figure 5 which is in
agreement with the fact that pure shear corresponds to diagonal compression and
tension at (45/-45).
Figure 5. Shear buckling force for different fiber angles
For a steel infill with (+45/-45) layers of full wrap FRP, the effect of increasing FRP
thickness is illustrated in Figure 6. The order of strengthening effects between the
four materials is justifiable considering the order of their moduli of elasticity. In the
same geometry and orientation, the highest buckling prevention is gained by the
material with the highest modulus of elasticity (HM-CFRP).
Figure 6. Buckling force for different FRP materials and thicknesses (full-wrap)
Diagonal Strips Configuration
In the second configuration, two diagonal FRP strips were attached to the steel plate
with widths of 150, 300 and 450 mm (Figure 7). The shear buckling critical stress
was calculated for each plate strengthened with the three FRP widths and different
thicknesses and shown in Figure 8.
050
100150200250300350400450
0 2 4 6
Cri
tica
l S
hea
r buck
ling F
orc
e
Per
Unit
Len
gth
of
Edge
(N/m
m)
FRP full wrap thickness (mm)
GFRP
CFRP
HM-CFRP
HS-CFRP
(a) (b) (c)
Figure 7. Configuration of diagonal FRP strips (a) w=150mm (b) w=300mm (c)
w=450mm
(a) (b)
(c) (d)
Figure 8. Buckling stress comparison for diagonal strip configuration with different
widths and thickness (a) GFRP, (b) HS-CFRP, (c) CFRP, (d) HM-CFRP
Using Figure 8, considering a cross-sectional area for the FRP strip, it is obvious from
the evaluation of buckling stress that a narrower and thicker strip provides better
buckling prevention than a thinner strip with a greater width. Figure 9 provides a
representative comparison between the buckling mode of a plate strengthened with a
150x4.5 mm strip and that of a plate with 450x1.5mm strip. For this comparison, the
bending stiffness of the thicker strip (as estimated by bh3/12) is 9 times that of the
thinner strip and therefore the diagonal of the plate tends to resist out-of-plane
bending better and force the plate to buckle in its second mode shape, thereby
increasing its shear buckling stress.
(a)
(b)
Figure 9. First shear buckling mode shapes for the plate with (a) 450x1.5 mm FRP
strips, and (b) 150x4.5mm strips
Performance in the Post-Buckling Phase
Retrofit Using FRP materials
Similar to the buckling phase studies, the steel infill plate of the SPSW was
strengthened with FRP materials in two patterns. First, the plate was fully covered
with FRP layers with the fibers oriented at (θ/-θ) as shown in Figure 10 (a). The
second configuration was diagonal FRP strips with varying widths and the fibers were
oriented along the length of the strip as previously depicted in Figure 7.
For each model, the load displacement pushover curve was extracted for each fiber
angle (θ). The curve was then idealized as a bilinear curve with equivalent initial
slope, yield point and ultimate strength by equating the enclosed area under the real
and the idealized curves as depicted in Figure 10 (b). Using the idealized curve,
quantitative measurement of the behavior of the composite SPSW was done through
strength parameters (Fu and Fy), lateral stiffness (K) and area enclosed by the load-
displacement curve (A).
Figure 10. FRP retrofit assumptions (a) Full wrap FRP bonding pattern (b) Bilinear
idealization of load-displacement curves
Optimum Fiber Angle in Full Wrap.
Figure 11 provides an illustration of the influence of fiber angle on strength and
stiffness behavior of the full wrap SPSW. The analyses show that for a SPSW with
two 1.5mm
-thick layers of CFRP, ultimate force and enclosed area are maximized at
37.5°, while the stiffness of the system is maximized at 45° and yield force at 42.5°.
Figure 11. Influence of fiber angle on strength and stiffness parameters of the full
wrap model (a) Ultimate strength, (b) area under the curve (c) lateral stiffness
Comparison of different FRP materials in Full Wrap
Table 2 provides a summary of the contributions to the behavior of the system by
different FRP materials. The models pertaining to this table are retrofitted using two
1.5 mm thick FRP layers oriented at an angle of 45°. This table shows considerable
strength and stiffness gains together with minor reductions in ductility. The highest
strength is obtained in the model with HS-CFRP and the highest lateral stiffness
occurs in the model with HM-CFRP. The model retrofitted using ordinary CFRP
shows considerable increases of 42.7% and 32.8% in strength and stiffness
respectively. The GFRP materials used seem to be relatively weak for strengthening a
SPSW.
Table 2. Comparison of different FRP materials for 1.5mm
full-wrap fibers at 45°
Material Fu (kN) A (kN.mm) K(kN/mm) Ductility
No FRP 3,396 214,507 280 7.6
CFRP 4,846 284,933 330 7.2
Increase (%) 42.7 32.8 18.0 -4.5
HS-CFRP 5,197 301,980 348 7.3
Increase (%) 53.0 40.8 24.7 -3.0
GFRP 3,949 236,973 290 7.5
Increase (%) 16.3 10.5 3.6 -0.8
HM-CFRP 3,890 262,226 384 8.0
Increase (%) 14.6 22.2 37.4 6.2
Figure 12 shows the general load-displacement curves of SPSWs retrofitted using
different FRP materials. The curves show a similar ascending trend except for the
model with HM-CFRP which demonstrates premature softening.
Figure 12. Load-displacement curves for SPSWs strengthened with different FRPs
To investigate the reason for this different behavior of the HM-CFRP system in
Figure 12, the Von Mises stress in the infill plate and the tensile damage variable in
the diagonal FRP layer at 2.5% story drift were evaluated (Figure 13). This figure
shows that the FRP layer is ruptured along the perimeter and the steel plate undergoes
strain hardening. This is to be expected considering the fact that the HM-CFRP
material has the smallest fracture strain capacity (0.34%) compared with the other
three materials which have 1.18%, 1.52% and 4.54% fracture strains for CFRP, HS-
CFRP and GFRP materials, respectively. It can be inferred that if the fracture strain of
the FRP material is small, severe damage and rupture of the fibers might occur, which
can produce a detrimental effect on the strength behavior of the SPSW.
0
2000
4000
6000
0 10 20 30 40 50 60 70
Sto
ry S
hea
r (k
N)
Story Lateral Displacement (mm)
HS-CFRP HM-CFRP CFRP
GFRP No FRP
(a) (b)
Figure 13. Behavior of the full wrap system at 2.5% drift (a) Von Mises equivalent
stress distribution in the steel infill plate, (b) tensile damage in the FRP wrap
Effect of the width of a diagonal FRP strip configuration.
An important question regarding the use of FRP materials to retrofit a SPSW is about
the spread of the FRP layer over the steel infill plate. Table 3 compares the
parameters of a SPSW retrofitted using 300mm
-wide diagonal strips with those of a
fully wrapped SPSW. It is notable that although the amount of FRP material used in
the full-wrap model is 6 times that of the diagonal strip model, the resulting increase
in strength is much smaller (e.g. 2.5 times increase in strength). This implies that
concentrating the FRP material in the diagonal region rather than spreading it on the
whole surface of the plate produces a better result. The reason is that the diagonal
region on the infill plate experiences the largest strains as the inward forces of the
plate gives the frame members an hourglass shape while the ends of columns are
forced away by the support provided by the ends of the upper and lower beams.
Table 3. Comparison of the model with 300mm
strip, with a full wrap model
(thickness=1.5mm
)
SPSW System Fu (kN) A (kN.mm) K (kN/mm)
No FRP 3,391 214,108 280
SPSW with full-wrap HM-CFRP 3,890 262,226 384
Increase (%) 14.7 22.5 37.2
SPSW with 300mm strip of HM-CFRP 3590.3 227397.8 305.2
Increase (%) 5.9 6.2 9.0
Full-wrap/strip ratio of increase in Fu, K or A 2.5 3.6 4.1
Table 4 provides a comparison between the parameters of two SPSWs with 150 mm
and 300 mm diagonal strips. The thickness of both CFRP strips is 6 mm and thus the
amount of material used in the 300-mm wide strip is twice that of the 150 mm-wide
strip. It can be seen that although the amount of FRP material used is doubled in the
300-mm model, the ratio of strength or stiffness increase never exceeds 1.8, which
implies that using a narrower strip of FRP results in a better retrofit which is again a
result of the strain concentration on the diagonal of the plate.
Table 4. Influence of FRP strip width on strength and stiffness parameters (strip
thickness=6 mm)
SPSW System Fu (kN) A (kN.mm) K (kN/mm)
No FRP 3,391 214,108 280
SPSW with 300mm CFRP strip 5,062 286,094 326
Increase (%) 49.3 33.6 16.4
SPSW with 150mm CFRP strip 4,336 256,670 307
Increase (%) 27.9 19.9 9.8
w300/w150 ratio of increase in K, A, Fu 1.8 1.7 1.7
CONCLUSIONS
Models of steel plate shear walls were designed and simulated using the finite
element method. FRP materials were attached to the steel infill plate in full wrap and
diagonal strip patterns and numerical analysis and comparisons of results of these
models were carried out in the two phases of buckling and post-buckling. The results
of the investigations reported in this paper showed that:
The optimum fiber angle for buckling prevention is 45º. Larger values of
elastic modulus resulted in greater improvement in shear buckling capacity.
In the diagonal strip configuration, for the same FRP cross section, the
thickest and narrowest strip results in the greatest buckling resistance.
The optimum orientation of fibers is in the direction of the inclined tension
field in the steel plate.
Both of the proposed retrofit patterns show significant improvements in terms
of shear strength and lateral stiffness.
Concentrating FRP on the diagonal region rather than its full spread on plate
yields improved results due to the strain concentration on the diagonal.
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The images used in this paper are created by the authors unless otherwise indicated.