Shear Conector
Shear Conector
Project performed in cooperation with the Texas Department of Transportation and the Federal Highway
Administration.
Center for Transportation Research
The University of Texas at Austin
3208 Red River
Austin, TX 78705
www.utexas.edu/research/ctr
iv
Disclaimers
Author's Disclaimer: The contents of this report reflect the views of the authors, who
are responsible for the facts and the accuracy of the data presented herein. The contents do not
necessarily reflect the official view or policies of the Federal Highway Administration or the
Texas Department of Transportation (TxDOT). This report does not constitute a standard,
specification, or regulation.
Patent Disclaimer: There was no invention or discovery conceived or first actually
reduced to practice in the course of or under this contract, including any art, method, process,
machine manufacture, design or composition of matter, or any new useful improvement thereof,
or any variety of plant, which is or may be patentable under the patent laws of the United States
of America or any foreign country.
Notice: The United States Government and the State of Texas do not endorse products or
manufacturers. If trade or manufacturers' names appear herein, it is solely because they are
considered essential to the object of this report.
Engineering Disclaimer
NOT INTENDED FOR CONSTRUCTION, BIDDING, OR PERMIT PURPOSES.
v
Acknowledgments
The authors gratefully acknowledge the financial support provided for this project by the
Texas Department of Transportation. The authors extend a special thanks to Jon Kilgore and
Clara Carbajal of the Texas Department of Transportation for their support, assistance, and
advice throughout the entire course of this project.
Products
Product P1, Recommended methods and design procedures for adding composite action
to existing non-composite bridge floor systems, is included in Chapter 6 of this report.
vi
Table of Contents
Chapter 1. Introduction................................................................................................................ 1
1.1 General ...................................................................................................................................1
1.2 Objective of TxDOT Project 0-4124 .....................................................................................2
1.3 Scope of Report .....................................................................................................................3
Chapter 2. Background: Behavior and Design of Composite Beams ...................................... 5
2.1 Introduction ............................................................................................................................5
2.2 Composite Action ..................................................................................................................5
2.3 Behavior of Stud Shear Connectors .......................................................................................7
2.4 AASHTO Provisions for Shear Connectors in Composite Bridges ....................................18
2.5 Design of Partially Composite Beams .................................................................................21
2.6 Approaches for Design of Composite Bridge Girders with Post-Installed Shear
Connectors .....................................................................................................................25
Chapter 3. Single-Shear Connector Tests: Phase I—Static Tests .......................................... 27
3.1 Introduction ..........................................................................................................................27
3.2 Investigated Types of Post-installed Shear Connectors .......................................................27
3.3 Development of Direct-Shear Single-Connector Test Specimens .......................................34
3.4 Setup for Single Connector Shear Test ................................................................................39
3.5 Test Results and Discussion ................................................................................................43
Chapter 4. Single-Shear Connector Tests: Phase II—Fatigue and Further Static
Tests.................................................................................................................................. 51
4.1 Introduction ..........................................................................................................................51
4.2 Test Setup and Procedure ....................................................................................................51
4.3 Test matrix ...........................................................................................................................54
4.4 Material Properties ...............................................................................................................54
4.5 Test Results ..........................................................................................................................56
4.6 Discussion of Test Results ...................................................................................................64
Chapter 5. Full-Scale Beam Tests.............................................................................................. 79
5.1 Introduction ..........................................................................................................................79
5.2 Test Program ........................................................................................................................79
5.3 Test Results ..........................................................................................................................91
5.4 Discussion of Full-Scale Beam Tests ..................................................................................95
Chapter 6. Summary, Conclusions, and Preliminary Design Recommendations............... 103
6.1 Summary ............................................................................................................................103
6.2 Conclusions ........................................................................................................................103
6.3 Preliminary Design Recommendations .............................................................................106
6.4 Recommendations for Further Research............................................................................107
References .................................................................................................................................. 109
vii
viii
List of Figures
ix
Figure 3.17: Concrete compressive strength of test specimens versus time ................................. 38
Figure 3.18: Test setup and test specimen for single-shear connector tests ................................. 41
Figure 3.19: Washer load cell ....................................................................................................... 42
Figure 3.20: DCDTs and load washer........................................................................................... 42
Figure 3.21: Typical characteristics of a load-slip curve .............................................................. 44
Figure 3.22: Typical failure of welded stud above the weld pool ................................................ 44
Figure 3.23: Typical failures at threads below the shear plane (WEDGB, HITTZ) ..................... 45
Figure 3.24: HAS-E adhesive anchor failure at the shear plane ................................................... 45
Figure 3.25: Epoxy plate failure of the concrete below the adhered surface (3MEPX) ............... 46
Figure 3.26: Load-slip curves for post-installed shear connectors ............................................... 48
Figure 4.1: Side view of direct shear test setup ............................................................................ 52
Figure 4.2: Average concrete compressive strength up to 28 days............................................... 55
Figure 4.3: Specimen designation system..................................................................................... 57
Figure 4.4: Load-slip curves for post-installed shear connectors ................................................. 57
Figure 4.5: S-N data for test specimens ........................................................................................ 58
Figure 4.6: Static and cyclic load-slip curves for Specimen CIPST25 ......................................... 59
Figure 4.7: Failed Specimen DBLNB-56HF ................................................................................ 60
Figure 4.8: Failed Specimen HASAA-38HF: a) concrete block, b) steel plate ............................ 61
Figure 4.9: HAS-E anchor failed at two locations (Specimen HASAA40) .................................. 61
Figure 4.10: Load-slip behavior after low-cycle fatigue loading (HASAA) ................................ 63
Figure 4.11: Change in load resisted by connector over time (Specimen DBLNB-01LF).......... 64
Figure 4.12: Comparison of load and ultimate slip capacity as a percentage of
corresponding values for CIPST connectors..................................................................... 65
Figure 4.13: Comparison of load ratios ........................................................................................ 68
Figure 4.14: Comparison of load ratios ........................................................................................ 69
Figure 4.15: Comparison of load ratios (Equation 4.1) ................................................................ 70
Figure 4.16: Comparison of S-N data from past research with current data ................................ 71
Figure 4.17: Ratios of residual to initial static load capacities ..................................................... 74
Figure 5.1: Details of specimen cross-section .............................................................................. 80
Figure 5.2: Reinforcement layout ................................................................................................. 80
Figure 5.3: Concrete formwork..................................................................................................... 81
Figure 5.4: Predicted load capacity of test specimens versus shear connection ration
(based on minimum specified material properties) ........................................................... 82
x
Figure 5.5: Coring and drilling into the specimen ........................................................................ 83
Figure 5.6: Drilling through beam flange ..................................................................................... 84
Figure 5.7: Drilled holes for DBLNB installation ........................................................................ 84
Figure 5.8: Use of “Squirter” Direct Tension Indicating (SDTI) washer ..................................... 84
Figure 5.9: Installation of HASAA shear connectors ................................................................... 86
Figure 5.10: ASTM A193 B7 rods after shear and tension tests .................................................. 88
Figure 5.11: Test setup.................................................................................................................. 89
Figure 5.12: Linear potentiometers for measuring slip at the end of the specimen ...................... 90
Figure 5.13: Strain gage locations ................................................................................................ 90
Figure 5.14: Load-deflection curves for the test specimens ......................................................... 91
Figure 5.15: Specimen NON-00BS—Cracks in the slab and beam local buckling (11-in.
deflection) ......................................................................................................................... 92
Figure 5.16: Specimen NON-00BS – Overall view of specimen at end of test (11.5-in.
deflection) ......................................................................................................................... 92
Figure 5.17: Specimen DBLNB-30BS—Cracks on the bottom of the concrete slab (3.25-
in deflection) ..................................................................................................................... 94
Figure 5.18: Specimen DBLNB-30BS—Flange and web local buckling (8-in. deflection) ........ 94
Figure 5.19: Specimen HASAA-30BS—Cracks on the bottom of the concrete slab (4.25-
in deflection) ..................................................................................................................... 95
Figure 5.20: Test results compared with theoretical values of stiffness and strength .................. 97
Figure 5.21: Failed sections of shear connectors .......................................................................... 98
Figure 5.22: Typical beam local flange and web buckling at large displacements ...................... 98
Figure 5.23: Slip at the ends of Specimen NON-00BS ................................................................ 99
Figure 5.24: Slip at the ends of Specimen DBLNB-30BS ......................................................... 100
Figure 5.25: Slip at the ends of Specimen HASAA-30BS ......................................................... 100
Figure 5.26: Neutral axis locations of test specimens................................................................. 101
xi
xii
List of Tables
Table 2.1: Coefficients for static stiffness of a shear connector per Equation 2.7 ....................... 11
Table 2.2: Maximum slip used for each specimen and corresponding number of cycles to
failure (Gattesco et al. 1997) ............................................................................................. 18
Table 3.1: Properties of connector materials ................................................................................ 39
Table 3.2: Summary of various connector test results .................................................................. 49
Table 4.1: Test matrix for high-cycle fatigue tests ....................................................................... 54
Table 4.2: Experimental and theoretical ultimate shear strength of connectors ........................... 56
Table 4.3: Summary of results for low-cycle fatigue tests ........................................................... 62
Table 4.4: Comparison of experimental and predicted values for ultimate load (Equations
2.2 and 2.3) ....................................................................................................................... 67
Table 4.5: Comparison of experimental and predicted values for ultimate load (Equations
2.4 and 2.5) ....................................................................................................................... 68
Table 4.6: Comparison of experimental and predicted values for ultimate load (Equation
4.1) .................................................................................................................................... 69
Table 4.7: Comparison of static strength to residual strength for connectors previously
subjected to fatigue loading .............................................................................................. 72
Table 4.8: Comparison of values obtained in residual static tests and initial static tests ............. 73
Table 4.9: Normalized material costs of connection methods ...................................................... 76
Table 5.1: Concrete slump and compressive strength .................................................................. 87
Table 5.2: Steel coupon test results............................................................................................... 87
Table 5.3: Reinforcing bar test results .......................................................................................... 87
xiii
xiv
Chapter 1. Introduction
1.1 General
Of the nearly 49,200 bridges in Texas, almost 3,000 are considered structurally deficient
by the National Bridge Inventory (National Bridge Inventory 2006). With a replacement cost
estimated at over $15 billion, alternative economically feasible methods of rehabilitating these
structurally inadequate bridges are highly desirable. For steel girder bridges, one way of doing
this is by making their concrete decks act compositely with their underlying steel girders.
Composite construction has been used in bridges and buildings since the 1930s. It implies
connecting one or more components of a structure so that they resist loads as a single unit, with a
load-carrying capacity greater than what could be achieved if the components acted separately.
In bridge construction, a steel girder and a concrete slab can be made to act together in flexure by
welding shear connectors to the top flange of the steel girder and then casting the slab on top.
In Texas, approximately two out of every five bridges are made of steel girders topped
with concrete slabs (National Bridge Inventory 2006). A significant number of older bridges with
steel girders were not designed for composite action, and hence have no shear connectors.
Connecting the steel girders and the concrete slab using shear connectors can increase the
flexural capacity of the girders by 50% or more. Figure 1.1 shows a typical bridge that is a
candidate for strengthening by creating composite action. This bridge was not designed for
composite behavior and was not provided with shear connectors.
For such non-composite bridges, composite action can be achieved by using post-
installed shear connectors. While such connectors are not common, they can be a potentially
cost-effective alternative to replacement of the bridge. This study focuses on finding cost-
effective, straightforward, and practical ways to create composite action in bridges originally
designed as non-composite.
1
Steel- concr ete
inter face
2
1.3 Scope of Report
This report consists of six chapters. Chapter 2 provides background information
necessary to assess the performance of shear connectors and composite beams. A summary of
AASHTO specifications on the design of shear connectors in composite bridges is also included
in Chapter 2. Chapter 3 summarizes single-shear connector tests under static loading. The static
load-slip behavior of post-installed shear connectors and the criteria used to recommend
particular shear connectors for further research are described. In Chapter 4, single-shear
connector behavior under high-cycle fatigue and low-cycle fatigue is described; more static test
results are provided; and preliminary design equations for post-installed shear connectors are
provided. Chapter 5 summarizes full-scale beam tests of partially composite beams retrofitted
with post-installed shear connectors. Behavior of the retrofitted beams is compared with non-
composite beams. Chapter 6 includes a summary, conclusion, and recommendations for further
research.
This report provides a summary of the activities and findings for TxDOT Research
Project 0-4124. More detailed documentation of this research is provided in three MS theses
(Hungerford 2004, Kayir 2006, Schaap 2004) and a PhD dissertation (Kwon 2008) completed in
the Department of Civil, Architectural, and Environmental Engineering at The University of
Texas at Austin. The reader is referred to these theses and dissertation for in-depth
documentation of this research.
3
4
Chapter 2. Background: Behavior and Design of Composite Beams
2.1 Introduction
The American Association of State Highway and Transportation Officials (AASHTO)
provides guidelines for the design of bridges in the U.S. Until recently, only allowable stress
design (ASD) and load factor design (LFD) were used in AASHTO provisions and made
available through the publication: AASHTO Standard Specifications for Highway Bridges. Since
1994, AASHTO LRFD Bridge Design Specifications has also been published utilizing load and
resistance factor design (LRFD). The AASHTO Standard Specifications for Highway Bridges
(2002) will be referred to as AASHTO ASD or AASHTO LFD in this report, depending on the
type of design method discussed. AASHTO LRFD Bridge Design Specifications (2005) will be
referred to as AASHTO LRFD.
The purpose of this study is to develop efficient and practical ways to increase load
carrying capacity of existing non-composite bridge girders by post-installing shear connectors.
This chapter starts with a general discussion of terms related to composite beams followed by
various research results on welded stud shear connectors (shear studs) under static and fatigue
loading. Welded stud shear connectors are the most common shear connector for new composite
beam construction. Understanding the behavior of the shear studs and composite action are
necessary to select structurally adequate post-installed shear connectors. Next, AASHTO design
procedure for composite bridge girders is summarized, including the requirements of the
AASHTO LRFD and of the AASHTO Standard Specifications. This chapter concludes with a
discussion of partially composite design. Stiffness and strength of the partially composite beams
are compared with non-composite steel girder system.
5
a) Non-composite action
b) Composite action
Figure 2.1: Composite action
A girder is defined to be “fully composite” when sufficient shear connectors are provided
to develop the full flexural strength of the given cross-section. That is, the flexural strength of the
member is governed by the strength of the steel girder and the concrete slab; girder strength is
not governed by the strength of the shear connectors. The number of shear studs required to
develop fully composite strength, Nf, is the number of shear connectors that allows the composite
girder to achieve its full ultimate strength and is obtained by calculating the force required to be
transferred at the steel-concrete interface at the ultimate load state (Faella, Martinelli, and Nigro
2003). A simple procedure is provided in the AASHTO ASD, LFD and LRFD Specifications to
determine Nf. The same procedure is also provided in the Specification for Structural Steel
Buildings published by the American Institute of Steel Construction (AISC 2005). This
procedure computes the force at the steel concrete interface when the fully composite cross-
section reaches its plastic capacity. The plastic capacity of the fully composite cross-section
occurs when the slab reaches its full compression capacity or when the steel girder is fully
yielded.
A girder is defined to be “partially composite” when the flexural strength of its girder is
governed by the strength of the shear connectors. The ultimate strength of a partially composite
girder is less than that of a fully composite girder because the concrete cannot achieve its full
plastic limit state, as the force in the slab is limited by the strength of the connectors. The
decrease in flexural strength can be related to the degree of shear connection N / Nf (or η). The
shear connectors must have the slip capacity required to achieve the desired load capacity
(Johnson and Molenstra 1991). Further discussions on the maximum slip required by a bridge
girder, as well as the slip capacity of a stud shear connector, are given later in this chapter.
For both fully composite and partially composite girders, some slip occurs at the steel-
concrete interface, because shear connectors are not stiff enough to prevent it (Faella, Martinelli,
and Nigro 2003). This slip primarily affects the stiffness of the composite member. In typical
design practice, the elastic stiffness of a fully composite girder for checking service load
deflections ignores slip at the steel-concrete interface, and the moment of inertia of the
composite girder is computed based on a transformed cross-section. On the other hand, the
calculation of elastic stiffness of a partially composite girder normally accounts for slip at the
6
steel-concrete interface, recognizing that slip will have a significant impact on stiffness even at
service load levels.
7
In a push-out specimen, two concrete slabs are typically attached to the flanges of a steel
beam with shear connectors. Figure 2.2 shows the standard push-out test setup included in the
Eurocode (ENV 1994-1-1, 1992). Typically four shear connectors are installed on each side of a
steel beam. Load is applied to the steel beam monotonically or cyclically until the shear
connectors fail.
Figure 2.2: Push-out test setup according to the Eurocode (SI units)
8
(1971) conclude that the concrete is the controlling medium, based on the observed behavior at
ultimate load. They produced Equation 2.1:
Qu = 1.106 × As × f ' c ×E c ≤ As × f u
0.3 0.44
(Eq. 2.1)
The AISC LRFD Specification for Structural Steel Buildings (2005) and AASHTO
specifications adopted a simplified equation, using the same variables:
Qu = 0.5 × As × f ' c ×E c ≤ As × f u (Eq. 2.2)
Ollgaard, Slutter and Fisher (1971) conclude from a plot of Qu / As versus f c × Ec used
to derive the equation that an upper bound to the connector strength is approached when
f c × Ec is about 130, as the test data tend to plot along a horizontal line. Since this corresponds
to a value of Qu / As of about 65 ksi, they conclude that the cap is related to the ultimate tensile
strength of the connector.
Equation 2.1 and Equation 2.2 are functions of only the concrete properties and the
diameter of the stud (except for the cap in strength defined by As Fu). Oehlers and Johnson
(1987) propose a simple expression for mean connector strength that also accounts for the
constitutive properties of the steel:
0.4 0.35
⎛E ⎞ ⎛ f '⎞
Qu = 5.0 × As × f u ⎜⎜ c ⎟⎟ × ⎜⎜ cu ⎟⎟ (Eq. 2.3)
⎝ Es ⎠ ⎝ fu ⎠
Design equations for the nominal shear strength of cast-in-place studs and post-installed
anchors are also provided in Appendix D of ACI 318-05. The commentary to ACI 318-05 states
that the shear strength of cast-in-place and post-installed anchors far from the edge of concrete
are usually governed by either the pryout strength of concrete or the shear strength of the anchor.
Since no pryout failure was observed during static tests in this study (described in Chapters 5 and
6), failure should therefore be governed by the strength of the anchor steel. ACI 318-05 provides
two separate equations for the shear strength of cast-in-place studs and post-installed anchors.
The equation for cast-in-place studs is the same equation for the ultimate tensile strength of steel
as shown in Equation 2.4. The ultimate tensile strength is used instead of ultimate shear strength
9
because the area of the weld pool is greater than the nominal cross-sectional area of the
connector.
Qn = As f u (Eq. 2.4)
An equation predicting the ultimate shear strength of post-installed connectors exists only
in ACI 318-05, and is based on the ultimate shear strength of steel. This equation is shown here
as Equation 2.5.
Qn = 0.6 As f u (Eq. 2.5)
This equation has a vertical slope at zero load. This was observed by Ollgaard, Slutter,
and Fisher (1971) in the load-slip curves due to the bond between the concrete slab and the steel
girder. For a slip equal to 0.2 in., the equation predicts loads of 99% of the ultimate load.
However, bond at the steel-concrete interface may be lost in a bridge after being subjected to
service loads for some period of time. Therefore, it is believed that Equation 2.6 overestimates
the initial stiffness of the connector in an existing bridge. The stiffness at 0.5Qu is proposed as
initial stiffness of a shear stud by Oehlers and Bradford (1995).
Oehlers and Coughlan (1986) derived the stiffness of the stud shear connector under
static and dynamic loads from 116 push-out test results. From the results of 42 push-out
specimens with 19 mm and 22 mm diameter shear studs, a static load-slip curve was derived
from linear regression analyses. Eq. 2.7 shows the load-slip relationship as the ratio of the slip to
the shear connector diameter.
Δ = ( A + B ⋅ f cu ') ⋅ d (Eq. 2.7)
The coefficients A and B are listed in Table 2.1. f cu ' is measured in N / mm 2 . Figure
2.3 shows load-slip relationships for a stud shear connector under static loading according to
Equation 2.6 and Equation 2.7. Maximum strength of the stud shear connector is assumed to be
21.4 kips.
10
Table 2.1: Coefficients for static stiffness of a shear connector per Equation 2.7
25
20
Load (kips)
15
10
Ollgaard et al. (1971)
5
Oehlers and Coughlan (1986)
0
0 0.1 0.2 0.3 0.4
Slip (in.)
Figure 2.3: Load-slip relations for shear studs
11
Where: su = ultimate slip capacity of connector.
SI units should be used for this equation.
Subsequent work has shown that slip at 0.95 × Qu on the descending branch is about
7.25-mm (0.29-in.) (Johnson and Molenstra 1991).
12
maximum shear. Badie (2002) focused on the testing of larger diameter studs (7/8-in. and 1-1/4-
in. diameter) and their response to fatigue loads.
Slutter and Fisher (1965) and Lehman et al. (1965) found that stress range is the most
important variable affecting the fatigue life of a shear connector. Stress range is defined as the
difference between the maximum and minimum stress acting on a connector, where the average
stress is calculated based on the effective tensile stress area of a stud. Johnson (2000), citing the
work of Oehlers (1990), states that the maximum load applied to a shear connector has a small
influence below load levels that are about 60% of the connector’s static shear strength. Loading
frequency was reported to be insignificant to the fatigue life of shear connectors (Nakajima
2003).
Concrete strength was found to not have a significant effect on fatigue life (Slutter and
Fisher 1966). The study by Lehman et al. (1965) shows no significant difference between the
fatigue behavior of shear connectors (3/4-in. diameter) in lightweight and normal weight
concrete.
Lehman et al. (1965) indicate that no direct relationship can be drawn between the slip
and fatigue life of a shear connector, however, distinct slip characteristics can be observed under
fatigue loading. They report an initial gradual increase in slip followed by leveling of the slip
curve with little increase up to failure. A sudden increase in the rate of slip was observed as
specimens reached failure, which they believe can be used as a failure criterion in both beam and
push-out tests. Roberts and Dogan (1997) indicate that the sudden increase in slip occurs
simultaneously with the propagation of fatigue cracks through a connector, which leads to a
reduction in stiffness. For a constant stress range, Mainstone and Menzies (1967) observed
reduction in the range of slip with increasing load ratio (increasing mean load).
Early beam tests suggested that no direct relationship exists between the static and fatigue
strength of shear connectors (King et al. 1965, Toprac 1965). This was later observed also by
Slutter and Fisher (1966) and became the basis for AASHTO Specifications, where the static
strength of a connector is treated separately from its fatigue strength. This concept was later
challenged by Mainstone and Menzies (1971), Oehlers and Foley (1985), and Oehlers (1990)
who found that the ultimate strength of a connector decreases once fatigue loads are applied.
13
Thurlimann'59 (3/4 in.) Mainstone and Menzies'67 (3/4 in.)
30 Ryu et al.'03 (3/4 in.) Badie et al.'02 (7/8 in.)
Slutter and Fisher'66 (7/8 in.) Slutter and Fisher'66 (3/4 in.)
Lehman et al.'67 (3/4 in.)
25
Stress Range (ksi) 20
15
10
5
0
1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08
Number of Cycles to Failure
Figure 2.4: S-N data for shear studs from push-out tests
As a result of push-out tests conducted by Slutter and Fisher (1966) the relationship
between the number of fatigue cycles to failure and the stress range is presented as Equation
2.12. This equation conservatively ignores data obtained from reversed load tests.
Based on the fact that push-out tests underestimate results from beam tests, Slutter and
Fisher (1966) used push-out test results to derive a conservative design equation for shear
connectors. The derived equation is the basis for current AASHTO Specifications for small
diameter shear connectors (less than or equal to 7/8-in.).
The design recommendations made by Slutter and Fisher (1966) enabled the uniform
spacing of shear connectors along the length of a bridge. This was followed by a significant
reduction in the number of shear connectors used in design and reduction in construction costs.
While most research focused on the fatigue endurance of shear connectors, some
researchers such as Oehlers and Foley (1985) and Oehlers (1990) focused on the strength of
shear connectors after application of fatigue loads. Contradicting the earlier belief of researchers
such as Slutter and Fisher (1966), they believe that the fatigue and static behavior of shear
connectors are related. The analytical work of Oehlers and Foley (1985) and the experimental
work of Oehlers (1990) show that the static strength of a shear connector decreases as soon as
fatigue loads are applied. They propose changing the design of shear connectors in bridges to
account for the reduction in static strength due to fatigue.
14
2.3.3.2 Low Cycle Fatigue
Factors that influence the fatigue life of shear connectors have been widely studied in the
past several decades. Research suggests that the fatigue life of shear connectors depends mostly
on the stress range applied to them. However, most research has focused on loading cases in
which shear connectors deform within their elastic range. In recent years, studies have also
considered cases where connectors are loaded into their inelastic range. These studies show
loading shear connectors into their inelastic range results in a low number of cycles to reach
failure; a phenomenon called low-cycle fatigue. Although a composite bridge would typically
undergo high-cycle fatigue under service loads, shear connectors could experience low-cycle
fatigue due to recurring overloads; especially in the case of partially composite design. Oehlers
and Foley (1985) suggest that “the peak load or an occasional overload does not affect the rate of
fatigue crack propagation, but it does affect the endurance [of a stud shear connector] by limiting
the amount of fatigue cracking that can occur before the stud fractures.”
Oehlers and Seracino (1998) indicate that with the application of fatigue loads, the
stiffness of a shear connector decreases, eventually reducing the state of the bridge to partial
composite interaction. Therefore, they believe that the research by Gattesco et al. (1997) does not
only apply to bridges with partially composite design, but also to bridges with fully composite
design.
Gattesco et al. (1997) suggested that inelastic behavior of shear connectors change the
structural response of a bridge in two ways:
1) Reduction in load amplitude: As the number of loading cycles increase the load
amplitude experienced by shear connectors reduces with time (Fig. 2.5(b)).
2) Load reversal: This usually occurs when connectors, typically at beam supports, yield
while the rest of the beam behaves elastically. Load reversal is experienced if the
recovered slip required by the beam is greater than the slip a yielded connector can
recover by unloading (Figures 2.5(c) and 2.6).
Due to the difficulty in capturing the effects of load redistribution between shear
connectors, researchers believe high-cycle and low-cycle fatigue should differ in the way they
are studied. While high-cycle fatigue is usually studied using load control, low-cycle fatigue is
typically studied using a displacement control approach. With displacement controlled tests the
“slip-history” of a shear connector gains importance (Gattesco et al. 1997).
15
Figure 2.5: Load (Q)-Slip (s) and Load (Q)-Time (t) curves of a shear connector in a structure:
(a) Elastic behavior; (b) Inelastic behavior; (c) Inelastic behavior with reversed loading
(Gattesco et al. 1997)
16
2.3.3.2.1 Research by Gattesco and Giuriani
The main goal of the tests performed by Gattesco and Giuriani (1996) was to investigate
the behavior of shear connectors under reversed shear loading. Tests were performed by applying
blocks of loading cycles with varying ranges of shear. Load cycles were applied at a rate of 500
N/s and the accumulated damage was monitored after each loading cycle. Each block of cycles
ended when the slip increment, Δs , reached either a null or a constant value. For unidirectional
tests, Δs was found to increase during initial cycles and later tend to a constant value. On the
other hand, for reversed load tests, a more rapid deterioration was reported of the stud shank and
the concrete in front of the stud. In this case, Δs was observed to grow with each loading cycle.
Over 300 cycles, the authors reported a 15 to 25% reduction in the slope of the unloading
branch of the load-slip curve. This suggests that the recovered slip increases with each cycle.
This is expected due to the accumulation of damage and loss of stiffness of the connector and
concrete after each loading cycle (Gattesco and Giuriani 1996).
17
Table 2.2: Maximum slip used for each specimen and corresponding number of cycles to
failure (Gattesco et al. 1997)
Specimen
Maximum slip (mm) Number of cycles
Number
1 0.80 38,338
2 1.00 18,400
3 1.00 13,200
4 1.25 5,274
5 1.50 3,040
6 2.00 3,230
7 2.00 1,440
8 3.00 432
The authors found that as the maximum slip value exceeded 1mm, the fatigue life of the
connectors were lower than 10,000 cycles. The corresponding shear load at every displacement
cycle was also found to reduce at the beginning of each test due to concrete damage around the
shear connector. Fatigue failure was observed through the stud shank (Gattesco et al. 1997).
18
As AASHTO Standard Specifications consider the effects of fatigue at service loads, the
response of a composite bridge is calculated using elastic theory. This leads to the horizontal
shear present per unit length of the beam, S r , also known as shear flow, to be determined using
Equation 2.14 (AASHTO ASD 10.38.5.1.1).
Vr Q
Sr = (Eq. 2.14)
I
Where: Vr = range of shear at cross section due to live and impact loads (kips)
Q = first moment of area of the transformed concrete section under
compression, about the neutral axis of the composite section (in3)
I = moment of inertia of the transformed composite section (in4)
Once the shear strength of a welded stud and shear flow are determined, the spacing of
shear connectors at a bridge cross section can be calculated with Equation 2.15 (AASHTO ASD
10.38.5.1.1).
s=
∑Z r
≤ 24 in. (Eq. 2.15)
Sr
Where: s = required spacing (center-to-center) of shear connectors (in.)
∑ Zr = the sum of the allowable range of horizontal shear on all connectors at
cross-section (kips)
After the spacing of shear connectors are determined to satisfy fatigue requirements, this
value must also be checked for ultimate strength requirements. These requirements utilize plastic
theory. The force in the slab is taken as the smaller of either the ultimate strength of the steel in
tension (Equation 2.16) or the ultimate strength of the concrete in compression (Equation 2.17)
(AASHTO ASD 10.38.5.1.2).
P1 = As Fy (Eq. 2.16)
To determine the number of shear connectors required, the ultimate strength of single
connector, Qu is needed and is given in Equation 2.18 (AASHTO ASD 10.38.5.1.2). This
19
equation was developed by Ollgaard et al. (1971) and suggests that the static strength of a shear
connector depends on its diameter, the strength of concrete, the elastic modulus of concrete, and
the tensile strength of the shear connector (assuming fu of shear connector steel is 60,000 psi).
General requirements are also given in AASHTO Standard Specifications for shear
connectors and are the same for both ASD and LFD design. Shear connectors are required to be
mechanical anchors and “…shall be capable of resisting both horizontal and vertical movement
between the concrete and the steel” (AASHTO ASD 10.38.2.2). A minimum embedment depth of
2 in. is specified for shear connectors, with a minimum clear cover requirement of 2 in.
(AASHTO ASD 10.38.2.3). Edge distance and longitudinal spacing requirements are also given in
Section 10.38.2.4. The edge to edge clear distance between the girder flange and the shear
connectors must be greater than 1 in. Also, adjacent shear connectors must be at least 4 in. apart
on center (AASHTO ASD 10.38.2.4).
The location of shear connectors is discussed in AASHTO ASD Section 10.38.4.2. Shear
connectors are to be placed in either positive moment regions or throughout the entire length of a
bridge. In the case of a continuous span bridge, shear connectors may be placed in the negative
moment regions if the reinforcing steel in the concrete is considered as part of the composite
section (AASHTO ASD 10.38.4.2).
20
for ultimate strength requirements. General provisions for shear connector design in AASHTO
LRFD are the same as in AASHTO ASD.
AASHTO LRFD uses somewhat different equations for determining the strength of a
shear stud under fatigue and static loads compared to AASHTO ASD. Equation 2.21 shows the
shear resistance of a single connector, Z r , for fatigue loading, given in AASHTO LRFD Section
6.10.10.2. This equation is same as Equation 2.13, except with a lower limit, below which the
connector is not expected to fail. Z r has units of ksi.
. d2
55
Zr = α d ≥2
(Eq. 2.21)
2
α = 34.5− 4.28log N (Eq. 2.22)
Where: d = diameter of stud (in.)
N = number of fatigue load cycles specified in AASHTO LRFD Section
6.6.1.2.5 for a bridge with a design life of 75 years.
21
A more practical solution for predicting deflection of a composite beam considering slip
at the steel-concrete interface was proposed by Johnson and May (1975). For a composite beam
with a shear connection ratio of η , a convenient design equation was proposed by a linear
interpolation approach. The equation is:
v part = v full + α ⋅ (v steel − v full ) ⋅ (1 − η ) (Eq. 2.24)
This equation was compared with the results from theoretical composite beam analysis by
McGarraugh and Baldwin (1971). This comparison showed that this equation provides a
conservative prediction of deflections for partially composite beams.
The commentary of the AISC LRFD Specification for Structural Steel Buildings provides
an equation for the effective moment of inertia to estimate deflections of partially composite
beams in the elastic range of behavior. This equation results in the deflection of fully composite
beams and bare beams, when η = 1 and η = 0 , respectively. The equation is:
I eff = I s + (∑ Q n / C f )(I tr − I s ) (Eq. 2.25)
Figure 2.7 shows the elastic stiffness of composite beams with different shear connection
ratios derived from Equation 2.25.
As shown in Figure 2.7, partially composite beams show much higher stiffness than non-
composite beams. This indicates that a significant decrease in deflection under service load is
expected when even a small number of post-installed shear connectors are installed in an existing
non-composite beam.
22
50
40
Load (kips)
30
Bare steel beam
η=0.2
20 η=0.4
η=0.6
10 η=0.8
η=1.0
0
0 0.2 0.4 0.6 0.8 1
Displacement (in.)
Figure 2.7: Initial stiffness of composite beams (AISC, 2005)
C 3 = ∑ Qn (Eq. 2.26c)
23
C 0.85fc'
(Py-C)/2
fy
(Py+C)/2
fy
Comp. Tension
Figure 2.8: Plastic cross-section analysis for composite beams
An example of the ultimate load carrying capacity of a composite beam with different
shear connection ratios is shown in Figure 2.9. Details of the composite beam are same as the
full-scale beam test specimens described in Chapter 5. Observe that a partially composite beam
with low shear connection ratios still shows much higher strength than the non-composite beam.
For example, even with a shear connection ratio as low as 30%, a strength increase of about 50%
is achieved.
300
250
Load (kips)
200
150
100
0 0.2 0.4 0.6 0.8 1
Shear connection ratio (ηmax)
Figure 2.9: Ultimate load carrying capacity of a composite beam
24
2.6 Approaches for Design of Composite Bridge Girders with Post-Installed
Shear Connectors
This chapter discussed design procedures for composite beams in the AASHTO
Specifications. The AASHTO composite beam design provisions are intended for new
construction using welded stud shear connectors, and are based on past research on these
systems. Further, current AASHTO Specifications only recognize fully composite design, and do
not include provisions for partially composite design. The absence of partially composite design
provisions in AASHTO likely reflects the fact that fatigue design requirements for shear studs
normally results in the need for a large number of shear connectors that will typically lead to a
fully composite beam for static strength calculations. Thus, the use of partially composite design
is not normally used for bridge girders. By contrast, partially composite design is used on a
routine basis for composite beams in buildings, and the AISC Specification for Structural Steel
Buildings has included detailed design provisions for partially composite beams for many years.
The popularity of partially composite beams in buildings reflects the great efficiency of partially
composite design for both strength and stiffness, as illustrated in Figures 2.7 and 2.9. The
different approaches to composite beam design in buildings versus bridges (bridges normally use
fully composite beams; buildings normally use partially composite beams) likely reflects the
dominating influence of fatigue in design of the composite beams for bridges, and the absence of
fatigue considerations in design of composite beams for buildings.
When considering the development of composite action in existing non-composite bridge
beams, a number of changes from conventional bridge design practice are needed. The welded
shear stud, commonly used in new construction, is not likely to be a practical alternative as a
post-installed shear connector. Consequently, new types of shear connectors must be developed,
and these connectors must be tested to determine their strength, stiffness, and deformation
capacity under static loads. They must also be tested to determine their performance under both
high-cycle and low-cycle fatigue loading. Thus, the current practice of using welded stud shear
connectors must be changed to enable the use of unconventional shear connectors. While there is
a long history of research and testing of welded stud shear connectors, there is little data on post-
installed shear connectors. Consequently, much of this research project was aimed at developing
concepts for post-installed shear connectors, and conducting tests to determine properties needed
for design.
In addition to developing new types of shear connectors, economical strengthening of
existing non-composite beams will almost certainly require adopting partially composite design.
The cost of post-installed shear connectors for an existing bridge is likely to be far greater than
the cost of welded studs for new construction. Fully-composite design will therefore likely be
very costly for strengthening existing bridges. Thus, the economic viability of strengthening
existing non-composite bridges by post-installing shear connectors is likely to depend largely on
the ability to implement partially composite design.
The development and testing of post-installed shear connectors are described in the
following chapters. Shear connectors were tested under static loading high-cycle fatigue loading
and low-cycle fatigue loadings. The feasibility of partially composite design using post-installed
shear connectors is then demonstrated in tests on large-scale composite beam specimens.
25
26
Chapter 3. Single-Shear Connector Tests: Phase I—Static Tests
3.1 Introduction
When choosing a post-installed shear connector for strengthening an existing bridge, both
the structural performance of the connector as well as the difficulty of installation are important
factors. In this chapter, various types of post-installed shear connectors considered in this study
are first described. Next, a setup for testing single-shear connectors was developed and various
types of shear connectors were tested to identify load-slip behavior under static monotonic
loading. Based on the results of these tests and on considerations of constructability, the most
promising post-installed shear connectors for bridge strengthening applications were identified.
These post-installed shear connectors were then subjected to further testing, which is described
in Chapter 4.
27
Figure 3.1: Post-installed shear connectors investigated under static loading
28
3.2.2 Post-Installed Welded Stud (POSST)
This method also uses the welded shear stud. However, the stud is installed after the
concrete slab is in place. This requires coring a hole through the concrete slab to allow enough
space for a shear stud and stud welding gun to fit. Once the hole is cored, the top flange of the
girder is cleaned and the stud is welded. The hole is then filled with non-shrink grout (see Figure
3.3).
29
3.2.4 Double-Nut Bolt (DBLNB)
The connector used in this method is a high strength ASTM A325 or A490 bolt. The
installation of this connector requires drilling holes through both the concrete slab and the steel
girder. The connector is then inserted in the hole and is held in place by two nuts. A bottom nut
is placed and tightened while the two top nuts prevent rotation of the bolt. Once the connector is
in place the hole is filled with non-shrink grout (see Figure 3.5).
30
3.2.6 Expansion Anchor (KWIKB)
For this connector, holes are drilled through both the girder flange and the concrete slab
from the bottom of the slab. The anchor is then tapped into the hole and tightened (see Figure
3.7). The expansion anchor is another connector that initially utilizes friction to transfer shear
forces between the slab and the girder. Once friction at the steel-concrete interface is overcome
with increasing load, the connector moves in the hole and transfers shear forces through bearing.
31
3.2.8 Welded Threaded Rod (POSTR)
As shown in Figure 3.9, this method is another variation on the POSST method. A hole is
cored through the concrete slab and a fully threaded rod is welded onto the steel girder. Prior to
grouting, a sheath is placed around the rod to prevent grout from filling the threads. The hole is
grouted leaving room for a washer and a nut. The sheath is later removed and the nut is
tightened. As a result, the rod transfers shear forces first by friction, and then by bearing once
friction is overcome.
32
3.2.10 HIT-TZ Adhesive Anchor (HITTZ)
Similar to the HAS-E anchor this anchor uses friction followed by bearing to transfer
shear forces from the bridge girder to the slab. The difference between these two connectors is
the way forces are transferred from the connector to the adhesive. The Hilti HAS-E anchor relies
on the bond between its threads and the adhesive. The HIT-TZ anchor, on the other hand,
transfers forces to the adhesive through wedging action due to its special threads (see Figure
3.11).
33
girder flange. The perimeter of the plate is then sealed with epoxy. Epoxy is injected to fill the
gap between the slab and the plate until epoxy ejects through predrilled exit holes.
34
84 in.
1 in. 7 in.
1 in.
12 in.
Figure 3.14: Cross-section of prototype composite bridge used to develop direct-shear test
specimens
35
Figure 3.15: (a) Empty waffle slab form; (b) form with plastic reinforcing chairs; (c) form with
plywood; (d) form with plywood and caulk; (e) form with reinforcing cage; (f) cast
concrete with steel test plate
36
(a) Top View
The concrete was ordered as Mix Design #261 ( f c ' =3,000 psi) from Capitol Aggregates
in Austin, Texas. The cast blocks were covered with plastic and sprinkled with water twice daily
for 5 days after casting. Test cylinders were covered with plastic and kept next to the test blocks.
To determine compressive strength, cylinder tests were performed at 7, 14, 21, and 28 days, and
37
on four later occasions during static testing. Results are shown in Figure 3.17. Note that the
compressive strength of the concrete was in the range of 3000 to 3500 psi.
4000
Compressive Strength (psi)
3000
Testing Ended at
2000 Testing Started 202 days on
at 41 days on 2/26/2004
9/18/2004
1000
Average Strength
Individual Strength
0
0 50 100 150 200 250
Days Cured
Figure 3.17: Concrete compressive strength of test specimens versus time
3.3.3 Grout
Several shear connection methods require grouting to fill the drilled holes during the
installation. For the selection of the grout material, the following qualities were necessary:
suitable for traffic applications, fast setting, high early compressive strength, low shrinkage, and
simple application.
Five Star™ Highway Patch met all of those requirements and was selected for use in this
study. This is a fast-setting grout typically used in traffic areas, including bridges. It is a one-
component material with a specified compressive strength of 2000 psi at 2 hours, 5100 psi at 24
hours, 7000 psi at 7 days. Due to its high early strength, roads can be opened to traffic 2 hours
after application (Five Star Products 2006).
38
3MEPX connection method, 3M DP-460 NS Epoxy was used. Its specified shear capacity is
4650 psi at 73° F and 1360 psi at 180° F.
39
connectors. With this method the load is applied closer to the steel-concrete interface. Details of
this direct-shear test setup and advantages over the push-out test are discussed in Schaap (2004).
3.4.2 Instrumentation
The instrumentation and data acquisition system consists of the hydraulic actuator load
cell for measuring applied load, a washer load cell for measuring anchor tension, and two
displacement transducers, for measuring slip. The load cell attached to the hydraulic actuator had
a 100-kip capacity. The measurement output was given to the nearest pound and was accurate to
within 0.5%, based on a statistical evaluation of the output. The load cell is located in the test
setup between the hydraulic actuator and the clevis.
Several setups included a 7/8-in. diameter washer load cell, intended to measure anchor
clamping force (see Figure 3.19). The washer load cell measurement was given to the thousandth
of a pound, but it was only accurate to within 20% of the output in the experiments, based on the
same statistical evaluation.
The displacement transducer, shown in Figure 3.20, were direct current differential
transformers (DCDT) that receive a DC input, convert that input to AC within the device, and
then convert the output signal back to DC. The DCDT has a precision of 0.0001 in., and it was
accurate to 0.2% of the displacement reading, based on the same statistical analysis.
40
Hydr aulic r am
Load Cell
Hydraulic Ram Steel Plate
Concrete
Specimen
Steel Plate
Concrete Block
Shear Connector
Figure 3.18: Test setup and test specimen for single-shear connector tests
41
Figure 3.19: Washer load cell
42
2) The hydraulic actuator, whose capacity was 100 kips, was operated using a 10,000-psi
capacity pneumatic oil pump and a manual regulator to apply load to the steel test plates
at rates ranging from 0.1 to 0.3 kips per second.
3) Load was applied until the connector failed or the concrete test block had developed a
significant crack through its entire section.
43
plastic defor mation
ultimate str ength
Load
yield
failur e
elastic connection
load stiffness
without
slip
slip without load Slip
Figure 3.21: Typical characteristics of a load-slip curve
Figure 3.22: Typical failure of welded stud above the weld pool
44
Figure 3.23: Typical failures at threads below the shear plane (WEDGB, HITTZ)
45
Figure 3.25: Epoxy plate failure of the concrete below the adhered surface (3MEPX)
46
3.5.3 Discussion
47
35
HTFGB
30 DBLNB
25
Load (kips)
POSST
20
CIPST
15
STWPL
10 POSTR
5
0
0 0.1 0.2 0.3 0.4 0.5 0.6
Slip (in.)
35
30
WEDGB
25
Load (kips)
HITTZ HASAA
20 KWIKB
CIPST
15
10
MAXIB
5
0
0 0.1 0.2 0.3 0.4 0.5 0.6
Slip (in.)
Figure 3.26: Load-slip curves for post-installed shear connectors
The shear resistance at a slip of 0.2 in. was chosen as a key parameter for comparative
evaluation of the strength of various shear connectors, and a criteria for selecting a limited
number of post-installed shear connectors for further testing under fatigue loading. According to
Equation 2.6, which approximates the load-slip curve for a stud shear connector, a 3/4-inch
diameter CIPST connector in 3,000 psi concrete attains approximately 95% of its ultimate
strength at a slip of 0.1 in., and 99% of its ultimate strength at a slip of 0.2 in. Strength
evaluations showed that seven shear connection methods performed at least as well as the cast-
in-place welded stud shear connector at the slip limit of 0.2 in.: POSST, STWPL, DBLNB,
HTFGB, HASAA, WEDGS, and 3MEPX.
48
The slip capacity of the shear connectors tested in this study is also significant. It is
generally useful as an index of a connection method’s ability to continue to resist load while
deforming inelastically. Several post-installed shear connectors tested here are made of higher-
strength, less-ductile steel than that of CIPST connector, and therefore have smaller slip
capacities.
49
50
Chapter 4. Single-Shear Connector Tests: Phase II—Fatigue and
Further Static Tests
4.1 Introduction
The Phase I tests described in Chapter 3 focused on evaluating a variety of different post-
installed shear connector concepts and identifying those with the most promising static strength
characteristics. As discussed in Chapter 3, this resulted in the selection of seven shear connectors
for further assessment under fatigue loads.
The primary purpose of the Phase II tests described in this chapter was to investigate the
fatigue performance of single-shear connectors at two distinct load levels: below the yield stress
(high-cycle fatigue) and above the yield stress (low-cycle fatigue). High cycle fatigue tests were
conducted first, and the connectors that showed good high-cycle fatigue performance were then
tested in low-cycle fatigue. Additional static tests were also performed to gather more
information on the load-slip behavior of each connector. All single-shear connector tests were
performed using the direct shear test setup.
51
Clamping Angle Alignment
Steel Plate Hydraulic
Coupler
Ram
Clevis
Load Cell
Test Block Line of Action
52
4.2.3.2 High-Cycle Fatigue Tests
Tests in high-cycle fatigue were performed to assess the fatigue performance of shear
connectors under repeated service loads. For these tests, stress range was used as the primary test
variable and the corresponding fatigue life of each connector was measured as the number of
cycles to failure, permitting construction of S-N curves as discussed in Chapter 2.
Stress ranges typical of those used by earlier researchers for the fatigue assessment of
welded studs were also used for CIPST specimens in these tests. This enabled a direct
comparison of results. For all other connection methods, a single test was performed for each
type of connector at a stress range already used for the CIPST specimens. Depending on the
response of each connector, the subsequent stress ranges were adjusted as needed. The selected
stress ranges were chosen to lie below the yield stress of the connector material.
The cyclic tests were controlled by applying a specified load range. Load ranges were
determined by multiplying the effective shear stress area of each connector by the desired stress
range. To prevent inadvertent reversal of load a minimum load of 0.9 kips was specified for each
load range. For most tests, a constant mean value was used, eliminating mean load as a variable.
For tests with high stress ranges, however, the mean load was adjusted to keep the maximum
load below the yield strength of the connector.
The tests were started with an initial static loading before the application of cyclic loads,
permitting comparison of the load-displacement data between high-cycle fatigue and static tests.
The static load was applied by first manually increasing the load up to the upper limit of the load
range (maximum load). Next, the load was reduced down to the lower limit (minimum load).
Finally, the load was increased up to the mean load which corresponds to the “set point” in the
407 Controller.
Once the “set point” was reached, half of the loading amplitude (span) and the loading
frequency were specified in the controller. Cyclic loading was then applied until connector
failure. A fatigue test was typically stopped if a connector showed no signs of failure after 5
million loading cycles. Several specimens that did not fail were loaded statically up to failure.
53
4.3 Test matrix
4.4.1 Concrete
The concrete used for the test specimens was ordered from Capitol Aggregates in Austin,
Texas (Mixture Design #261) and had a target 28 day compressive strength of 3,000 psi.
Concrete strength was evaluated by cylinder tests at 7, 14, 21, and 28 days using the 6- x 12-in.
cylinders. Average concrete strength was determined as 2960 psi at 28 days. The increase in
average concrete strength within the first 28 days is shown in Figure 4.2. Additional cylinder
54
tests were performed regularly throughout the testing program. Further data on concrete strength
is given in Kayir (2006).
3000
2500
Strength (psi)
2000
1500
1000
500
0
0 5 10 15 20 25 30
Time (Days)
Figure 4.2: Average concrete compressive strength up to 28 days
4.4.3 Grout
Five Star8 Highway Patch was also used for POSST and DBLNB methods. The strength
of the grout used in each specimen is provided in Kayir (2006).
55
area was taken as 80% of the gross area of the connector as in AISC LRFD Specification for
Structural Steel Buildings (2005). Also listed in Table 4.2 is the estimated ultimate tensile
strength of the connector materials. The ultimate tensile strength was estimated by assuming that
the shear strength of the material is equal to 60% of the tensile strength. It was also assumed that
the net area in tension for threaded rods was 75% of the gross area. Finally, Table 4.2 also lists
the minimum specified tensile strength for the connector materials. Observe that the actual
strength of the connectors was significantly greater than the minimum specified values.
Measured Minimum
Estimated
Ultimate Specified Ultimate
Connector Type Ultimate Tensile
Shear Tensile Strength
Strength (ksi)
Strength (ksi) (ksi)
CIPST & POSST 48.7 81.2 60
DBLNB 86.6 144.3 120
HTFGB 82.7 137.8 120
HASAA 70.1 116.8 72.5
WEDGB 100.6 167.7 145
56
Static test: Sequence of test
High-cycle fatigue test: Stress range
Low-cycle fatigue test: Sequence of test
HASAA-30HF
Applied connection method
ST: Static test
HF: High-cycle fatigue test
LF: Low-cycle fatigue test
40 POSST-04ST(F)
HTFGB-04ST
POSST-04ST CIPST-04ST
30
Load (kips)
DBLNB-04ST
WEDGB-04ST
20 CIPST-Average
HASAA-04ST
10
0
0 0.2 0.4 0.6 0.8
Slip (in.)
Figure 4.4: Load-slip curves for post-installed shear connectors
57
4.5.3 High-Cycle Fatigue Test Results
This section presents results from 20 high-cycle fatigue tests conducted at predetermined
stress ranges for each shear connection method. Due to the brittle behavior exhibited by
Specimen 3MEPX specimens, 3MEPX specimens were not tested in high-cycle fatigue and were
excluded from further consideration.
Each high-cycle fatigue test started with an initial application of monotonic load followed
by the application of load cycles until failure, as previously described in Section 4.2.3.2. Each
specimen was tested either until failure occurred or until at least 5 million loading cycles was
reached.
Test results are summarized in Figure 4.5. Specimens for which testing was stopped
before connector failure are shown with arrows adjacent to the data points. Stress ranges were
calculated based on the effective shear area of each connector at the steel-concrete interface.
Figure 4.5 also shows the S-N curve adopted by AASHTO LRFD for welded stud shear
connectors. The AASHTO S-N curve was based on the mean behavior of welded stud shear
connectors under high-cycle fatigue loading from push-out tests. Slutter and Fisher (1966) report
that push-out test results conservatively estimate the behavior of shear connectors, so push-out
tests are assumed to represent a lower bound of shear connector failure in real beams.
60 CIPST POSST
DBLNB HTFGB
50
Stress Range (ksi)
HASAA WEDGB
40
30
20
10 AASHTO (2005)
0
1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08
Number of Cycles to Failure
Figure 4.5: S-N data for test specimens
As shown in Figure 4.5, post-installed shear connectors generally shows better fatigue
strength than the conventional CIPST connectors. HTFGB and DBLNB connectors show
significantly higher fatigue strength than CIPST connectors. These two connectors appear to
exhibit an endurance limit at about a 35 ksi stress range, whereas AASHTO LRFD defines the
endurance limit of welded stud shear connectors as 3.5 ksi. POSST connectors which require
welding for installation show less fatigue endurance than the other types of post-installed shear
connectors which do not require welding. DBLNB connectors using a high strength rod (ASTM
58
A193 B7 rod) with rolled threads showed higher fatigue strength than HASAA connectors using
a rod (HAS-E anchor) with cut threads. Specimens DBLNB-38HF and DBLNB-31HF were
tested under static loading after the high-cycle fatigue tests. Specimen DBLNB-38HF reached an
ultimate load of 29.0 kips, while Specimen DBLNB-31HF reached 29.4 kips.
Load-slip readings for connectors were recorded during the initial application of
monotonic load and intermittently throughout high cyclic testing, to assess degradation in
stiffness under high-cycle fatigue loading. The resulting load-slip curves showed increasing slip
and decreasing stiffness with cycling for all connectors, with the changes varying with stress
range and connection type. In Figure 4.6 are shown the static and cyclic load-slip curves for
Specimen CIPST-25HF, representative of the general trend observed in the load-slip behavior of
all investigated connectors.
14
12
10
Load (kips)
8
6
Number of Cycles
4 Static
2 1200
5000
0
0 0.01 0.02 0.03 0.04 0.05 0.06
Slip (in.)
Figure 4.6: Static and cyclic load-slip curves for Specimen CIPST25
Failure modes of the single-shear connector test specimens under high-cycle fatigue
loading were similar to those under static loading except Specimens DBLNB-56HF, HASAA-
38HF, and HASAA-33HF. The failure plane of Specimen DBLNB-56HF corresponded to the
level at which the second nut on the threaded rod ended (see Figure 4.7). Significant crushing of
both the grout and concrete was observed in front of the connector. This may be attributed to the
local crushing of concrete. This may have shifted the reaction on the connector below the steel-
concrete interface resulting in the observed failure mode.
59
Figure 4.7: Failed Specimen DBLNB-56HF
60
a)
b)
Figure 4.8: Failed Specimen HASAA-38HF: a) concrete block, b) steel plate
61
4.5.4 Low-Cycle Fatigue Test Results
Shear connection methods that performed well under high-cycle fatigue were tested
under low-cycle fatigue. Specimens were tested cyclically under displacement control until either
failure or 4,000 cycles was reached. As described previously in Section 4.3.3, a maximum
displacement of 0.2 in. and a minimum displacement of 0.1 in. were applied to each specimen.
Table 4.3 summarizes the results obtained from the low-cycle fatigue tests. All post-
installed shear connector specimens performed better than Specimen CIPST-01LF, which failed
immediately upon the application of fatigue cycles. Failure occurred only in Specimen HTFGB-
01LF, which had previously been subjected to 5.6 million cycles of fatigue loading under a 35
ksi stress range (HTFBG-35HF). Specimens that remained intact up to 4,000 cycles (5,000
cycles for HTFGB-02LF) were finally tested statically to failure. Results of these static tests are
also given in Table 4.3. Figure 4.10 shows typical load–slip behavior under static load after
4,000 cycles of fatigue load. Residual slip due to the inelastic behavior during the low cycle
loading was about 0.15 in. for the specimens under low-cycle loading.
62
30
25
Load (kips)
20
15
HASAA-04ST
10
HASAA-01LF
5 HASAA-02LF
0
0 0.1 0.2 0.3 0.4
Slip (in.)
Figure 4.10: Load-slip behavior after low-cycle fatigue loading (HASAA)
The load sustained by the connector at each displacement cycle was recorded during each
test, permitting the development of a load-time graph for each specimen. The load-time graph for
Specimen DBLNB-01LF is shown in Figure 4.11 and is representative of the trend observed for
each specimen. The graph indicates a considerable reduction in the load applied to the connector
with each cycle to constant displacement amplitude. This load reduction is due to decreasing
lateral stiffness of the connector as the concrete around the connector crushes. The decrease in
applied load continues until a somewhat constant load is reached. Load reversal starts with the
monotonic application of the displacement range and continues throughout the 4000
displacement cycles. This suggests that the connector behaves inelastically and endures loading
in the opposite direction to achieve the required minimum displacement. Load reversal was not
observed for the WEDGB specimens.
63
Figure 4.11: Change in load resisted by connector over time
(Specimen DBLNB-01LF)
64
ASTM A193 B7 threaded rod for its anchor material, whereas the other DBLNB specimens used
SAE J429 – Grade 8 tap bolt. Thus, only Specimen DBLNB-04ST was compared with CIPST
specimens for the connection method. For the POSST method, POSST-04ST(F) was used instead
of POSST-04ST because of the premature failure of shear connector due to a weld defect.
As shown in Figure 4.12, post-installed shear connectors show higher ultimate strength
than CIPST connectors except HASAA connectors. The HASAA method shows higher load at
0.2 in. of slip. However, most of post-installed shear connectors show less slip capacity than
CIPST connector. This can be attributed to the use of high strength grout and high strength
connector materials.
250
Ultimate Load (%)
200 Max. Slip (%)
Percent of CIPST
100
50
0
CIPST POSST DBLNB HTFGB HASAA WEDGB 3MEPX
Connection method
Figure 4.12: Comparison of load and ultimate slip capacity as a percentage of corresponding
values for CIPST connectors
65
of the experimental load divided by the predicted load also are given for each specimen. Load
ratios less than 1.0 indicate that the predicted strength was higher than the experimentally
measured ultimate strength (in other words, the predicted strength was unconservative). Load
ratios for both tables are compared in Figure 4.13 and 4.14. Variables and corresponding values
used in each equation are described in greater detail in Kayir (2006).
Loads ratios for Equation 2.2 are compared in Figure 4.13. The equation governed by the
compressive strength of concrete conservatively underestimates the ultimate shear strength of
almost all post-installed shear connectors except that of POSST specimens and Specimen
DBLNB-04ST. Except for Specimen CIPST-01ST and Specimen CIPST-04ST, the ultimate load
of all welded shear studs is overestimated.
Figure 4.14 shows a comparison of experimental and predicted ultimate strength values
for Equation 2.3 proposed by Oehlers and Johnson (1987). This equation includes material
properties of both concrete and connector steel for the prediction of ultimate strength of shear
connectors. As indicated in Figure 4.14, ultimate load values predicted by Equation 2.3 are
generally unconservative.
Figure 4.14 also presents comparisons of experimental and predicted values for the
ultimate load of each specimen for Equation 2.4 and 2.5. Predicted values are calculated using
equations that are governed by the ultimate strength of the connector steel. These equations are
the ultimate tensile strength of steel ( As f u ), which is used in Equation 2.4, and the ultimate shear
strength of steel ( 0.6 As f u ), which is used in Equation 2.5. The ultimate tensile strength equation
gives an unconservative estimate of the ultimate load for all specimens. The ultimate shear
strength equation more conservatively estimates the ultimate load. However, it still results in
unconservative results for many cases.
Based on those comparisons it appears that none of the existing equations conservatively
predicts the experimentally observed ultimate load for all shear connectors tested in this current
research. Variability in experimental data is also clearly apparent. As an alternative to the
existing shear connector strength design equations discussed earlier, the following equation is
proposed for estimating the shear strength of post-installed connectors for design purposes:
This equation corresponds to one-half the ultimate tensile strength of the connector steel.
Predicted ultimate load values and corresponding load ratios for this formula are presented in
Table 4.6. Load ratios are compared in Figure 4.15, and it can be observed that the proposed
equation provides a conservative estimate of ultimate shear strength for post-installed shear
connectors, except the WEDGB connectors. For the DBLNB, HTFGB, and HASAA specimens,
the predicted strength is 10 to 25 percent lower than the experimentally measured ultimate
strength. This suggests that the proposed Equation 4.1 is not excessively conservative.
66
Table 4.4: Comparison of experimental and predicted values for ultimate load (Equations
2.2 and 2.3)
Test Result Eq. (2.2) Load Ratio Eq. (2.3) Load Ratio
Specimen ID.
(kips)a (kips)b (a/b) (kips)c (a/c)
CIPST-01ST 24.3 22.5 1.08 - -
CIPST-02ST 21.7 22.5 0.96 - -
CIPST-03ST 17.8 22.5 0.79 - -
CIPST-04ST 29.4 22.4 1.31 24.0 1.23
POSST-01ST 22.8 27.6 0.82 - -
POSST-02ST 22.4 29.2 0.77 - -
POSST-03ST 23.3 29.2 0.80 - -
POSST-04ST(F) 28.8 35.9 0.80 38.2 0.75
DBLNB-01ST 31.1 18.8 1.66 - -
DBLNB-02ST 30.6 18.8 1.63 - -
DBLNB-03ST 28.4 18.8 1.51 - -
DBLNB-04ST 28.9 35.7 0.81 46.3 0.62
HTFGB-01ST 30.7 23.2 1.32 - -
HTFGB-02ST 34.3 23.2 1.48 - -
HTFGB-03ST 33.5 23.2 1.45 - -
HTFGB-04ST 38.8 24.1 1.61 35.7 1.09
HASAA-01ST 22.7 18.5 1.23 - -
HASAA-02ST 21.8 18.5 1.18 - -
HASAA-03ST 23.1 18.5 1.25 - -
HASAA-04ST 22.9 19.6 1.17 26.0 0.88
WEDGB-01ST 23.0 20.9 1.10
WEDGB-02ST 23.8 20.9 1.14
WEDGB-03ST 27.6 20.9 1.32
WEDGB-04ST 27.5 21.5 1.28 35.9 0.77
67
Table 4.5: Comparison of experimental and predicted values for ultimate load (Equations
2.4 and 2.5)
Test Result Eq. (2.4) Load Ratio Eq. (2.5) Load Ratio
Specimen ID.
(kips)a (kips)b (a/b) (kips)c (a/c)
2.00
AASHTO (2005)
1.50
Load ratio
1.00
0.50
0.00
F)
SA 4 S T
T
T
T
G ST
G ST
G ST
ST
T
SS ST
SS ST
ST
04 T
SA 1ST
SA 2ST
SA 3ST
G ST
TF 01S
1S
3S
2S
TF 04S
TF 02S
TF 03S
CI -02S
CI -01S
CI -03S
S
BL ST(
3
2
04
PO -04
4
PO -01
PO -02
SS -03
H B-0
D B-0
D B-0
D B-0
H A-0
W A-0
H A-0
H A-0
W B-0
W B-0
W B-0
B-
B-
B-
B-
B-
T
P O ST
PS
PS
PS
PS
G
N
G
T-
S
ED
ED
BL
BL
BL
ED
ED
CI
A
H
H
D
Specimen
68
1.50
Oehers and Johnson (1987)
ACI for shear stud (2005)
Load Ratio ACI for post-installed anchor (2005)
1.00
0.50
0.00
CIPST- POSST- DBLNB- HTFGB- HASAA- WEDGB-
04ST 04ST(F) 04ST 04ST 04ST 04ST
Specimen
Figure 4.14: Comparison of load ratios
Table 4.6: Comparison of experimental and predicted values for ultimate load (Equation
4.1)
69
2.00
1.64 1.61
Load Ratio 1.50 1.27
1.13 1.11
1.00 0.85
0.50
0.00
CIPST- POSST- DBLNB- HTFGB- HASAA- WEDGB-
04ST 04ST(F) 04ST 04ST 04ST 04ST
Specimen
Figure 4.15: Comparison of load ratios (Equation 4.1)
70
Past Research CIPST
60 POSST DBLNB
HTFGB HASAA
Stress Range (ksi) 50 WEDGB
40
30
20
10
AASHTO (2005)
0
1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08
Number of Cycles to Failure
Figure 4.16: Comparison of S-N data from past research with current data
Data from the current fatigue tests for the cast-in place welded stud are generally similar
to the data from past research. It is clear from Figure 4.16 that S-N data from past tests show
considerable scatter. In general, data from the current tests fall within the overall scatter band of
the data from past tests. Thus, even though the current tests were not conducted on push-out type
specimens, the direct-shear single connector test setup used for the current tests gives fatigue
results comparable to push-out type specimens.
Scatter in fatigue life is evident at every level of stress range in the past data. This scatter
may be the result of many factors, including variability in material properties, variability in stud
weld quality, and intrinsic variability in fatigue life. The presence of scatter suggests that many
tests are needed to adequately characterize the fatigue behavior of shear connectors.
All specimens with post-installed shear connectors had improved fatigue life compared to
the CIPST specimens. The superior fatigue performance of DBLNB and HTFGB specimens is
readily apparent in this figure. Failure was achieved for DBLNB specimens only at a stress range
56 ksi. Specimen DBLNB-38HF and DBLNB-31HF did not fail and are shown as runnout
specimens with arrows next to the corresponding data points. Specimen HTFGB-35HF did not
fail after 5 million cycles of fatigue loading. .
71
test). The load ratios are all essentially unity, suggesting that the application of 5 million or more
high-cycle fatigue cycles did not reduce the ultimate strength of the connectors.
Table 4.7: Comparison of static strength to residual strength for connectors previously
subjected to fatigue loading
Residual Ultimate Ultimate Load from Load
Specimen
Load (kips) Initial Static Test (kips) Ratio
POSST-15HF(F) 29.0 28.8 1.00
DBLNB-38 29.0 28.9 1.00
DBLNB-31 29.4 28.9 1.01
Due to the intrinsic scatter of fatigue test results, more tests would be desirable to better
define fatigue endurance of other types of post-installed shear connectors under higher stress
ranges.
72
the low-cycle fatigue tests were conducted by applying selected displacement cycles to the
connectors, rather than applying load cycles, as was done in the high-cycle fatigue tests.
Fatigue failure was not obtained for specimens tested under low-cycle fatigue, except for
Specimen HTFGB-01LF, which had been previously subjected to 5 million loading cycles in the
high-cycle fatigue tests (HTFGB-35HF). Also, Specimen CIPST-01LF could not be properly
tested under low-cycle fatigue due to a defective weld.
After 4,000 displacement cycles were applied, the residual static strength of each
specimen was evaluated and the load-slip curves were captured. Values for ultimate strength and
slip, and load at 0.2 in. of slip, are reported in Table 4.8. These values are compared to those
obtained from initial static tests and the load and slip ratios are given (the residual static test
value divided by the initial static test value). Load and slip ratios are compared in a bar chart
form in Figure 4.17.
Table 4.8: Comparison of values obtained in residual static tests and initial static tests
Residual Ultimate Residual Ultimate
Load at 0.2 in.
Load Slip
Specimen
Exp. Load Load Exp. Slip Slip Exp. Load Load
(kips) Ratio (in.) Ratio (kips) Ratio
DBLNB-01LF 32.5 1.13 0.30 0.91 9.2 0.34
DBLNB-02LF 34.6 1.20 0.32 0.95 11.1 0.41
HTFGB-02LF 18.0 0.52 0.77 1.23 4.9 0.18
HTFGB-03LF 37.5 1.08 1.00 1.60 4.7 0.17
HASAA-01LF 23.6 1.05 0.32 0.89 6.9 0.31
HASAA-02LF 21.8 0.97 0.30 0.83 4.8 0.22
WEDGB-01LF 28.4 1.11 0.73 1.14 1.7 0.10
WEDGB-02LF 27.8 1.09 1.00 1.57 2.2 0.13
73
2.00
Ultimate Load (%)
Residual Static/Initial Static Ultimate Slip (%)
1.50 Load at 0.2 in. (%)
1.00
0.50
Specimen
Figure 4.17: Ratios of residual to initial static load capacities
It can be seen in Figure 4.17 that the static capacities of the post-installed shear
connectors were not significantly affected by low-cycle fatigue loading except Specimen
HTFGB-02LF. In Specimen HTFGB-02LF, the connector failed inside the steel plate. It is
considered that the first root of the threads is vulnerable to fatigue loading. This failure mode
under fatigue loading was observed in Specimen HTFGB-45HF and all WEDGB specimens.
The ultimate slip experienced by each specimen is almost matched the values observed in
initial static tests except Specimen HTFGB-03LF and Specimen WDEGB-02LF. These
specimens showed a significant increase in ultimate slip. At a slip of 0.2 in., a significant
decrease in load is apparent for all specimens. The slip of 0.2 in. coincides with the maximum
displacement applied to each specimen during fatigue cycles.
It appears that a high number of displacement cycles had no significant effect on the
ultimate strength of the shear connectors. Increasing damage of the concrete in front of the
connector with each displacement cycle may have reduced the confinement around the
connector, and, as the connector deformed inelastically, resulted in less load applied to the
connector with each displacement cycle. As a result, the possibility of degradation in the
connector material and a low-cycle fatigue failure could have been reduced.
74
connection methods are discussed for constructability and cost evaluation. Comparative
connector costs and relative ease of installation are given in Table 4.9 for the connection
methods discussed in this chapter.
The POSST method is the only retrofit method using a welded shear stud, and also the
only method that can be installed completely from the top of a bridge. Static and fatigue tests,
however, showed that the behavior of this connection depends heavily on the quality of the stud
weld. This prompts the need for inspections of the weld quality in a field application. For welded
studs in new construction, stud welds are typically inspected by a non-destructive “bend test” in
which a number of shear studs are bent a specified amount. This technique is not easy to use for
the POSST method, since no room is available to bend the stud inside a 3.5-in. diameter hole.
Consequently, some other stud weld inspection technique would be needed, and it is unclear if
another practical method is available.
Like the Post-Installed Welded Stud (and Stud Welded to Plate) method, the Double-Nut
Bolt requires coring holes through the concrete slab. Unlike the Post-Installed Welded Stud,
however, installation of this connector requires access from underneath the bridge as well as
from the top. The smaller diameter hole (2-in.) used with the Double-Nut Bolt may require less
time and effort to drill than the 3.5-in. core used with the Post-Installed Welded Stud.
The High-Tension, Friction Grip Bolt was found to be the hardest of all tested connectors
to install in a laboratory setting. Drilling two different size holes was cumbersome in the
laboratory, and could be even more difficult on a real bridge. This method also requires access
both from the top and the bottom of the slab.
The Adhesive Anchor was found to be one of the easiest connectors to install in a
laboratory setting. This connector can be installed in a bridge with minimal damage to the
concrete slab from under the bridge. The only drawback of the installation process is the time
needed for the adhesive to cure. For a 68 o F temperature a 50 min. curing time is required for
the adhesive used in the tests. During this time the adhesive should not be disturbed, which may
require traffic to be stopped on a bridge.
The Concrete Screw was the easiest connector to install. This one-piece screw requires
drilling only from the bottom of the bridge. The concrete screw can be easily installed while the
bridge is in service; it requires no grout or adhesive and can resist load immediately after
installation.
The Epoxy Plate method has several installation disadvantages. First, a long curing time
of 7 days is required for the epoxy used in the tests. During this time, it may be necessary to
restrict traffic on the bridge. Second, the epoxy is brittle, which means no slip can be observed
between the steel girder and concrete deck prior to failure. This would require high safety factors
to be used in design. Finally, the effects of weathering and extreme temperature on epoxy
durability are also unknown for this type of application.
Costs listed in Table 4.9 include materials (connectors, grout and adhesive as applicable),
but do not include labor costs, as little information was available on actual labor requirements for
each method. The comparative cost analysis was performed assuming 300 connectors (the
number required for a 50-ft long span with six girders, with rows of two connectors, spaced
longitudinally at 2 ft.). Costs are normalized to the cost of the cast-in-place, welded headed
studs. Costs for 3MEPX method were estimated assuming that the adhered area was
approximately equal to that of two cast-in-place welded studs spaced at 2 ft, with an additional
safety factor of about 1.5 due to the brittle failure of the connection. No other connection
75
methods were so adjusted for relative strength or failure mode. Cost evaluation results are listed
in Table 4.9.
76
used for DBLNB connectors and its fatigue endurance is better understood and design
recommendation in Equation 4.6 can be used for the rod.
77
78
Chapter 5. Full-Scale Beam Tests
5.1 Introduction
In the previous chapters, several types of post-installed shear connectors were tested
under static, high-cycle fatigue, and low-cycle fatigue loading using the direct shear test setup.
Based on the test results, two types of shear connectors were recommended for further evaluation
in full-scale beam tests: the double nut bolt (DBLNB) and the adhesive anchor (HASAA). Two
full-scale partially composite beams retrofitted with DBLNB and HASAA connectors were
tested under static loading. One non-composite beam was also tested as a benchmark to compare
the structural performance of retrofitted partially composite beams with existing non-composite
beams.
The selected post-installed shear connectors were installed using procedures which could
be used in an actual field application. Thus, constructability issues for the connection methods
could also be evaluated during the construction of the specimens in the laboratory.
79
by the test specimen to be cured in the same environment with the test specimens. After casting,
the exposed surface of the concrete was covered with plastic sheets for 5 days under moist
conditions. The concrete formwork was removed from the specimen 7 days after the casting, and
reused for the other specimens.
84
12 #5 & #4 @6in.
7
#4@12in.
W30x99
Unit: in.
80
Figure 5.3: Concrete formwork
81
connector shear strength was computed as 0.5As fu, where fu is 125 ksi, and As is 0.48 in2. This
results is 30.1 kips per shear connector.
Also, the specimens were tested only under static load; fatigue strength of the shear
connectors was checked with Equation 2.4 and Equation 4.2. Fatigue load was calculated with
the design truck described in AASHTO LRFD with a spacing of 30 ft between 32-kip axles.
Under this truck load, the maximum shear force sustained by the shear connectors is 164.4 kips.
Therefore, each shear connectors in one shear span sustains 10.27 kips. Since the diameter of the
shear connectors is 7/8 in., stress range in each shear connector is 21.36 ksi ( = 10.27 kips / 0.48
in2), which satisfies Equation 4.2.
300
250
Load (kips)
150
137 kips
30%
100
0 0.2 0.4 0.6 0.8 1
Shear connection ratio (ηmax)
Figure 5.4: Predicted load capacity of test specimens versus shear connection ration (based on
minimum specified material properties)
82
1) A 2.5-in. diameter hole was drilled into the concrete slab from the top using a Hilti
DD200 coring machine. A DD-BL U4 diamond core bit was used for the coring
operation (see Figure 5.5). This core bit is designed for coring a wide range of
concrete and medium steel reinforcing. A constant water supply is needed to keep the
drill bit cool. It took 5 to 10 minutes to complete each hole through the concrete slab.
2) A 15/16-in. diameter hole was drilled through the steel beam top flange from the top
side of the slab using a portable magnetic drill. A 10 in. long drill bit was used to the
drill holes from the top of the slab. A hollow round bar was placed inside of the cored
hole in the concrete to serve as a guide for the steel drill bit. This guide also helped to
keep the inside surface of the concrete clean from machine oil (see Figure 5.6). To fix
the coring machine and the magnetic drill to the concrete slab surface, a 1 in. thick
steel plate was anchored to the concrete slab using four concrete anchors.
3) A 7.25-in long ASTM A193 B7 rod was placed from the top to provide a 5-in.
embedment length. Figure 5.7 shows the concrete surface after drilling. The connector
was tightened to a pretension of 39 kips using an impact wrench. “Squirter” Direct
Tension Indicating (SDTI) washers were used to confirm the required pretension as
shown in Figure 5.8. This washer has several bumps on the surface. Under this bump,
orange-color silicone is embedded. As a bolt is tightened, the silicone material comes
out and gives a visual indication of bolt tension. This washer first tested using the
Skidmore-Wilhelm Bolt-Tension Calibrator and checked to determine the amount of
silicone coming out to achieve the specified pretension.
4) Grout was poured to fill the gap. Five Star® Highway Patch was used for the grout
materials. Five Star® Highway Patch is fast setting, high strength grout which is used
for repair of highways and bridges.
83
Figure 5.6: Drilling through beam flange
84
5.2.1.3.2 Installation of Shear Connectors for Specimen HASAA-30BS
The same 7/8-in. diameter ASTM A193 B7 threaded rods used for the DBLNB-30BS
specimen were also used for the HASAA shear connectors in specimen HASAA-30BS.
Following is the procedure used to install the HASAA shear connectors.
1) A 15/16-in. diameter hole was drilled through the steel flange from the bottom of the
slab. A portable slugger drill with magnetic base was used to drill the hole (see Figure
5.9a).
2) A 5-in. deep hole was drilled into the concrete from the bottom using a 7/8-in. drill bit
and a Hilti TE-55 rotary hammer drill as shown in Figure 5.9b. The 15/16-in. diameter
holes are required to install HASAA shear connectors according to the installation
manual provided by Hilti (Hilti 2006). A 15/16-in. diameter carbide-tipped drill bit did
not fit into the 15/16-in. diameter hole through the steel beam flange. Therefore, a 7/8-
in. diameter drill bit was used to drill the hole in the concrete and worked to make the
hole larger.
3) The drilled hole was cleaned using a wire brush and compressed air before injecting
adhesive.
4) Hilti HIT HY 150 adhesive was injected in the hole using the HIT-MD 2000 manual
dispenser. Eight to nine holes can be completed with an 11.1-fluid ounce cartridge
pack. The adhesive was viscous enough not to run down during the upward
application.
5) An anchor rod was inserted with a twisting motion. The rod can be adjusted during the
specified gel time, but should not be disturbed between the gel time and cure time.
The gel time and the cure time are 6 min. and 50 min. at 68° F. Adhesive that
overflowed was wiped off, leaving adhesive filling the gap between the oversized hole
in the steel flange and the anchor. The hole in the concrete slab was not perfectly
vertical, so the rod was self-braced and was not required to be held during the cure
time to prevent from falling.
6) After the gel time, the rod was fastened with specified torque (125 lb-ft) using a torque
wrench.
85
c) Injecting adhesive d) Tightening with torque wrench
Figure 5.9: Installation of HASAA shear connectors
86
Table 5.1: Concrete slump and compressive strength
87
5.2.2.3 Shear Connectors
ASTM A193 B7 threaded rod has a minimum specified yield stress 105 ksi and minimum
ultimate tensile strength 125 ksi. All of shear connectors for the composite beam tests were cut
from rods from the same production lot. The threaded rods were tested in shear and tension using
a customized bolt testing apparatuses. Figure 5.10 shows sections of threaded roads after the
tests.
Only the ultimate strengths for shear and tension were determined from the tests. The
measured ultimate shear and tensile strength for the threaded rod were 91.1 ksi and 147 ksi. Note
that the measured shear strength of the rod is 62% of the measured tensile strength.
88
Test specimen End bracing
Bracing Support
5.2.3.2 Instrumentation
Vertical deflection, slip between the concrete slab and the steel beam flange, and
longitudinal strain in both the steel beam and reinforcing bars in the concrete slab were measured
during the test. Two string potentiometers at the center of the beam and one at each quarter point
of the beam were installed to measure vertical deflection during the tests. Slip at the interface
between the concrete slab and the steel beam were also measured at the center and quarter points
of the beam. Figure 5.12 shows two linear potentiometers at the one end of the beam for
measuring slip. Strain gages were used to measure longitudinal strain of the composite beam at
89
the center and 6 in. from the center. The location of the strain gages at a beam cross-section is
shown in Figure 5.13.
Loading was applied by two 100-ton capacity hydraulic rams which were operated using
a 10,000-psi capacity pneumatically driven oil pump. Test data were read every at 5 kip loading
intervals in the elastic range. When the test specimen yielded, data were read at increments of
0.25-in. center deflection.
Concrete slab
Steel beam
Linear potentiometer
Figure 5.12: Linear potentiometers for measuring slip at the end of the specimen
84
1.5
12
7
: Strain gage
90
5.3 Test Results
During each test, in addition to electronically recording data, the specimens were visually
examined for phenomena such as cracks in the concrete slab, yielding and local buckling in the
steel beam and failure of the post-installed shear connectors. The observations of various
phenomena during the tests are described in this section. Load versus center deflection curves for
each test specimen are shown in Figure 5.14.
200
max: 231 kips
Load (kips)
150
max: 163 kips
100
DBLNB-30B
50 HASAA-30B
NON-00B
0
0 2 4 6 8 10
Deflection (in.)
Figure 5.14: Load-deflection curves for the test specimens
91
the concrete at the top of the slab. At 6.5-in. deflection, both flange and web local buckling were
observed in the steel beam. Flange buckling occurred only on one side and started about half of
the beam depth away from the center of the beam. Crack widths on the bottom of the concrete
slab were about 1/16 in. At about 6.8-in. deflection, Specimen NON-00BS reached its ultimate
strength which was 163.1 kips. Beyond 6.8 in. deflection, the strength of Specimen NON-00BS
started to reduce due to local flange and web buckling in the W30x99 beam. At 7.5-in.
deflection, flange buckling occurred on the other side of the beam flange. Figure 5.15 shows
cracks in the slab, and local buckling of steel beam at 11-in. deflection. The test stopped at 11.5-
in. deflection for safety reasons. No crushing on the top of the concrete was observed after the
test. An overall view of the specimen at 11.5-in. deflection is shown in Figure 5.16
Figure 5.15: Specimen NON-00BS—Cracks in the slab and beam local buckling (11-in.
deflection)
Figure 5.16: Specimen NON-00BS – Overall view of specimen at end of test (11.5-in. deflection)
92
5.3.2 Specimen DBLNB-30BS
Specimen DBLNB-30BS was constructed with DBLNB (double nut bolt) shear
connectors. It was designed as 30% composite based on the specified strength of concrete, steel
beam, and DBLNB shear connector. In total, 32 shear connectors (16 in each shear span) were
installed in the beam, and were distributed uniformly along the length of the beam.
Figure 5.14 shows the load-deflection response for Specimen DBLNB-30BS. Compared
to Specimen NON-00BS, Specimen DBLNB-30BS showed much higher strength and stiffness.
The specimen showed a sudden strength drop after the peak load due to the failure of multiple
shear connectors. After the strength drop, however, Specimen DBLNB-30BS showed very
similar behavior to Specimen NON-00BS.
The initial stiffness of Specimen DBLNB-30BS was much higher than Specimen NON-
00BS. From around 65 kips, Specimen DBLNB-30BS started losing stiffness. This can likely be
attributed to the nonlinear behavior of the shear connectors near the supports. It is also
considered that the friction force between the connector and steel beam was overcome, so that
the threaded rod slipped in the oversized hole in the steel beam flange. At 130 kips, flaking of
whitewash was detected on the bottom beam flange and on the beam web. The first crack on the
concrete slab was detected at a load of 200 kips. The cracks were observed only on the edge of
the slab and did not propagate on the bottom of the slab. Spacing of the cracks on the concrete
slab edge was 5 to 8 in. At a load of 220 kips, some cracks on the concrete slab propagated to the
bottom. At 220 kips, the stiffness of the specimen reduced significantly, so that the load was
applied by displacement control instead of load control.
At 3.25-in. deflection, some cracks in the concrete slab propagated to the center of the
slab. Most cracks propagated to the center and the width of the cracks was less than 1/32 in (see
Figure 5.17). At 4.25-in. deflection, one shear connector located near the south support failed
with a loud noise. No sudden drop of load, however, was detected due to this failure. This can
likely be attributed to the redistribution of shear force among the shear connectors. From the
single connector tests (Chapter 4), the DBLNB connector exhibits less ductility than the
conventional CIPST shear connectors. This can be attributed to the high strength of the
connector material and high strength of the grout used to fill the hole after installation of the
connectors. At 4.5-in. deflection, more than 10 shear connectors fractured essentially
simultaneously. Accordingly, the strength of the specimen dropped suddenly, as seen in the load-
deflection plot in Figure 5.14. In addition, cracks on the side of the concrete slab propagated
toward the top of the slab. However, there was no sign of crushing of concrete on the top of the
slab.
After the multiple fractures of shear connectors, the structural behavior of Specimen
DBLNB-30BS was similar to that of non-composite Specimen NON-00BS as shown in Figure
5.14. At 5-in. deflection, top flange local buckling occurred at the first shear connector location
from the center of the beam. For Specimen NON-00BS, first beam flange local buckling was
detected at 6.5-in. deflection. At 6.0-in. deflection, beam flange buckling was detected on both
sides of the flange and web local buckling was also observed. Another shear connector failure
was observed for each 8- and 8.5-in. deflection. Figure 5.18 shows slab cracks and steel beam
local buckling at 8-in. deflection. The test stopped at 10-in. deflection for safety reasons.
93
Figure 5.17: Specimen DBLNB-30BS—Cracks on the bottom of the concrete slab (3.25-in
deflection)
Figure 5.18: Specimen DBLNB-30BS—Flange and web local buckling (8-in. deflection)
94
A small amount of whitewash flaking was detected on the bottom beam web at a load of
120 kips. At 190 kips, flaking of whitewash was also observed on the bottom flange. The first
crack on the concrete slab was observed at a load of 200 kips. At 210 kips, the crack propagated
to the center of the slab. At 220 kips, several cracks were observed on the bottom of concrete
slab. Spacing of the cracks was 5 to 8 in. At 225 kips, the stiffness of the specimen reduced
significantly, so the load was applied by displacement control instead of load control. Figure
5.19 shows concrete cracks at 4.25-in. deflection. Between 4.75- and 5.00-in. deflection, multiple
connectors fractured consecutively. Thirteen shear connectors out of sixteen failed in the south
shear span. The deflection of the beam after the failure was 4.87 in.
After failure of multiple shear connectors, the behavior of Specimen HASAA-30BS was
very similar to the behavior of non-composite Specimen NON-00BS. Beam flange local
buckling was first observed at 5.25-in. deflection and web local buckling was detected at 6-in.
deflection. Crack widths on the concrete slab were about 0.04 in. at 5.25-in. deflection. The test
was stopped at 10-in. deflection for safety reason.
Figure 5.19: Specimen HASAA-30BS—Cracks on the bottom of the concrete slab (4.25-in
deflection)
95
The theoretical stiffness and strength of the non-composite specimen (NON-00BS) is
based on the steel beam only. No contribution of the concrete slab for stiffness or strength is
included. The theoretical strength of the specimen was computed using the actual measured yield
strength values for the W30x99 test beam (see Table 5.2).
The theoretical stiffness of the partially composite specimens (DBLNB-30BS and
HASAA-30BS) was determined using an effective moment of inertia, computed using Equation
2.25. The theoretical strength of these specimens was based on simple plastic cross-sectional
analysis, as described in Section 2.5.1.2. In computing the theoretical strength, the actual
measured yield strength of the steel beam and compressive strength of the concrete were used.
Shear connector strength was computed as 0.5 As fu, per Equation 4.1. In this calculation, As was
taken as 80% of the gross area of the 7/8” diameter threaded rod. That is, As = 0.80 × π (7/8″ ÷
2)2 = 0.48 in2. For the ultimate tensile strength of the shear connector material fu, the measured
value of 147 ksi was used (see Section 5.2.2.3).
The behavior of non-composite Specimen NON-00BS, which represents an existing
bridge girder without any shear connectors, basically reflected the behavior of a bare steel beam.
Specimen NON-00BS shows only slightly higher stiffness and strength than the bare beam. By
comparing the theoretical strength and stiffness (which are based on the steel beam only) with
the measured load-deflection response, the contribution of the concrete slab towards stiffness and
strength of the girder appears to be negligible. Note also that load-deflection response of
Specimen NON-00BS exhibited excellent ductility, a desirable attribute for a bridge girder.
The composite beams retrofitted with the post-installed shear connectors showed much
higher stiffness and strength than the non-composite Specimen NON-00BS as expected. Recall
that the composite ratio of the specimens was relatively low (30%) and the spacing between the
connectors was 28.5 in. which is much larger than the spacing required for a fully composite
beam. Despite the relatively small number of shear connectors provided in these specimens, a
40% increase in strength was achieved compared to the non-composite specimen, demonstrating
the efficiency of partially composite design.
The measured ultimate strength of the test specimens showed good agreement compared
to the theoretical values. Specimen HASAA-30BS shows slightly higher strength and ductility
than Specimen DBLNB-30BS. The reason for the small difference in strength and ductility
between HASAA-30BS and DBLNB-30BS is difficult to determine from this limited test data,
but may simply reflect intrinsic variability in structural performance.
The strength of the shear connectors controls the strength of the partially composite
beams. The strength of the DBLNB and HASAA shear connectors is controlled by fracture of the
connector. Based on the individual shear connector tests, fracture of the DBLNB and HASAA
occurs at a smaller slip value than conventional welded shear studs. That is, the DBLNB and
HASAA connectors are somewhat less ductile than the conventional welded shear stud. The
overall load-deflection response of the retrofitted partially composite beam specimens also
showed relatively non-ductile behavior, compared to the non-composite specimen.
96
250
max: 239 kips
150
max: 163 kips
100
DBLNB-30BS
50 HASAA-30BS
NON-00BS
0
0 2 4 6 8 10
Deflection (in.)
Figure 5.20: Test results compared with theoretical values of stiffness and strength
97
combination of tension and shear, whereas HASAA shear connectors failed primarily due to
shear. After failure of the shear connector, both of the retrofitted partially composite beams
showed behavior that was very similar to the non-composite beam specimen. Thus, while the
retrofitted beam specimens showed a sudden strength drop when the shear connectors failed, the
specimens had substantial residual strength and ductility, as they revert back to non-composite
beams.
All of the test specimens exhibited local flange and web buckling at large deflections.
However, the loss of strength drop due to the buckling was quite gradual. Typical local buckling
at large deflections is shown in Figure 5.22.
Figure 5.22: Typical beam local flange and web buckling at large displacements
98
5.4.3 Interface Slip and Neutral Axis Locations
All of the test specimens showed an increase in slip at the interface between the concrete
slab and the steel beam with increase in load. Figure 5.23 shows the interface slip at the ends of
Specimen NON-00BS. Slip increased linearly with load at the early stages of loading. After local
buckling of the web and flange occurred, slip on the south end with the hinge support increased
continuously, whereas the slip on the north end decreased.
Specimen DBLNB-30BS showed much less slip at the early stages of loading (see Figure
5.24). At 60 kips loading, the slope of the load-slip curve decreases, but still shows linear
behavior. It is possible that friction between the connector and steel beam due to tensioning of
the shear connectors was overcome and shear connector slip occurred in the oversized holes.
Specimen HASAA-30BS did not show a sudden change of slope in the load-slip curves (see
Figure 5.25). In Specimen HASAA-30BS, the oversized holes were filled with HY 150 adhesive
during installation. After shear connector failure, both retrofitted partially composite beams
showed a continuous increase in slip on the south end of the beams as in Specimen NON-00BS.
Specimens DBLNB-30BS and HASAA-30BS showed beam end slip values, at the point
of connector failure and sudden strength loss, of 0.23 in. and 0.27 in., respectively. These values
are 26% and 31% of the shear connector diameter (7/8 in.), which are less than the values from
the single-shear connector tests. It appears that more single-shear connector tests are necessary to
characterize single-shear connector behavior including its strength and slip capacity.
250
200
Load (kips)
150
100
South End
50
North End
0
0 0.2 0.4 0.6 0.8 1
End slip (in.)
Figure 5.23: Slip at the ends of Specimen NON-00BS
99
250
200
Load (kips)
150 First fracture of
a shear connector
100
North End
50 South End
0
0 0.2 0.4 0.6 0.8 1
End slip (in.)
Figure 5.24: Slip at the ends of Specimen DBLNB-30BS
250
200
Load (kips)
150
100
North End
50
South End
0
0 0.2 0.4 0.6 0.8 1
End slip (in.)
Figure 5.25: Slip at the ends of Specimen HASAA-30BS
Composite action in the retrofitted partially composite beams can be further evaluated by
locating the neutral axis during the tests. For non-composite behavior, the neutral axis is
expected to be at mid-height of the steel beam. For composite behavior, the neutral axis moves
toward the top flange. Figure 5.26 shows the measured neutral axis location at mid-span of the
girder at various load levels throughout the tests. Neutral axis locations were obtained by
interpolating strain data read from the strain gages on the beam section.
100
For Specimen NON-00BS, the neutral axis was located near mid height of the steel
section at most load levels, as expected. At very low load levels at the start of the test, the neutral
axis was located higher up in the cross-section, suggesting some degree of composite action.
This early composite action may have been due to bond and/or friction between the steel and
concrete. However, as indicated in Figure 5.26, this composite action only occurred at very low
load levels. Once the load exceed about 10% of the girder’s full capacity, this composite action
ended, and the girder subsequently behaved in an almost purely non-composite manner. When
evaluating existing non-composite bridges, it is sometimes surmised that some degree of
composite action can be considered when load rating the girders, resulting from bond and
friction between the steel and concrete. However, the test results for Specimen NON-00BS
suggest that such “unintended” composite action should not be relied upon in evaluating the
strength of existing non-composite girders. A similar conclusion was reached after an extensive
series of field load tests on non-composite steel girders in TxDOT Project 0-1741 (Bowen and
Engelhardt 2003).
25
20
Plastic neutral axis
15 for partially composite beam
10 NON-00BS
DBLNB-30BS
5 HASAA-30BS
0
0 100 200 300
Load (kips)
Figure 5.26: Neutral axis locations of test specimens
For the retrofitted partially composite beams, the neutral axis stayed above mid-height of
the steel section at all load levels, as indicated in Figure 5.26. Specimen DBLNB-30BS and
Specimen HASAA-30BS showed almost full composite action in the early stages of loading,
likely due to the friction at the steel-concrete interface. However, the neutral axis moved down as
the load increased, indicting partial composite interaction between the steel beam and concrete
slab.
5.4.4 Constructability
In addition to assessing the structural performance of the retrofitted girders,
constructability related issues for the two shear connection methods were also evaluated during
101
the full-scale beam tests. Procedures used to install the shear connectors in the test specimens are
similar to the procedures that would likely be used on an actual bridge, allowing for an
assessment of construction related difficulties.
102
Chapter 6. Summary, Conclusions, and Preliminary Design
Recommendations
6.1 Summary
This study investigated methods to strengthen existing non-composite steel bridge girders
by the development of composite action between the steel girder and concrete slab. More
specifically, the objective of this study was to identify structurally efficient and practical ways to
post-install shear connectors in existing bridges. Various types of post-installed shear connection
methods were tested under static, high-cycle fatigue, and low-cycle fatigue loads using a direct-
shear test setup. Based on the results of single-shear connector tests, full-scale beam tests were
performed under static load to evaluate system performance of the beams retrofitted for partial
composite action with post-installed shear connectors.
First, using a direct-shear test setup, various post-installed shear connectors were tested
under monotonically increasing loads to examine the load-slip behavior of the connectors, and
characterize their stiffness, strength, and ductility. Conventional cast-in-place welded studs,
which are widely used for new construction, were also tested as a benchmark to assess the
structural behavior of the post-installed shear connectors.
For the post-installed shear connection methods that showed acceptable performance
under static loads, their structural performance was further evaluated through cyclic tests. High-
cycle and low-cycle fatigue tests were conducted to assess the comparative behavior of these
shear connectors subjected to repeated service loads and overloads, respectively. The
performance of shear connectors under fatigue loading was also compared to that of the
conventional cast-in-place welded stud.
The post-installed shear connectors that showed the most promising structural
performance under static and fatigue loading were then selected for further evaluation in full-
scale beam tests. A total of three full-scale beam tests were conducted. Two full-scale non-
composite beams were built and retrofitted with different post-installed shear connectors. One
non-composite beam was also tested as a benchmark to compare the structural performance of
the retrofitted partially composite beams. In constructing the full-scale beam test specimens, the
installation processes of the two shear connection methods were also evaluated.
6.2 Conclusions
The results of this study clearly demonstrate that the strength and stiffness of existing
non-composite steel bridge girders can be increased significantly by post-installing shear
connectors. Development of composite action between the existing steel girder and concrete slab
through the installation of post-installed shear connectors appears to be a structurally efficient
and cost-effective approach to retrofit existing bridges. The addition of post-installed shear
connectors can increase the load capacity of existing steel girders on the order of 40 to 50%.
Some more specific conclusions of this project are as follows:
103
• Of the various types of post-installed shear connectors investigated in this study, the
most promising, from a structural performance and constructability point of view
are:
- double-nut bolt
- adhesive anchor
- high tension friction grip bolt.
• These connectors consist of high strength bolts or threaded rods placed in holes that
are drilled in the concrete slab and top flange of the steel girder. The holes are filled
with high strength grout (double-nut bolt and high tension friction grip bolt) or
structural adhesive (adhesive anchor). Installation of the double-nut bolt and high
tension friction grip bolt require construction operations on both the top and bottom
sides of the concrete slab. The adhesive anchor, on the other hand, can be
completely installed from underneath the slab, thereby minimizing traffic
disruptions on the bridge.
• Static tests on these three post-installed connectors show strength levels that are
similar or greater than conventional welded studs. Fatigue tests on these post-
installed connectors show significantly better fatigue lives than conventional
welded studs. The excellent fatigue performance of these three post-installed shear
connectors is attributed, in large part, to the fact that no welds are involved in their
installation.
• A preliminary recommendation was developed for computing the static strength of
the post-installed shear connectors. The recommended equation is as follows:
For threaded connectors, as used in the double-nut bolt, adhesive anchor and high
tension friction grip bolt, it is recommended that As be taken as 80% of the gross
unthreaded cross-sectional area of the connector.
Equation 6.1 differs considerably from the existing AASHTO shear connector
strength equations for conventional welded shear studs, but is believed to provide a
reasonable and conservative estimate of the strength of the post-installed shear
connectors, based on the tests conducted in this study.
• A limited number of high-cycle fatigue tests on the post-installed shear connectors
showed fatigue lives that are significantly better than conventional welded shear
studs, as noted earlier. However, not enough fatigue tests were conducted to
confidently recommend an S-N relationship for design purposes. Due to the
intrinsic variability of fatigue test results, additional fatigue tests would be desirable
to better identify a design S-N curve for the post-installed shear connectors.
104
Nonetheless, based on the limited available data, a preliminary simplified
recommendation for checking fatigue of post-installed shear connectors made of
ASTM A325 bolts or of ASTM A193 B7 threaded rods is to assume a fatigue
endurance limit of 35 ksi. That is, if the stress range on the effective shear area of
the connector is less than 35 ksi, then a fatigue failure appears unlikely. The
effective shear area of the threaded connectors can be taken as 80% of the gross
cross-sectional area of the connector.
• It is recommended that partial composite design be used as a basis for determining
the number of post-installed shear connectors that will be used to strengthen an
existing bridge girder. Current AASHTO Specifications only recognize full
composite design for steel bridge girders, and do not include provisions for partial
composite design. The absence of partially composite design provisions in
AASHTO likely reflects the fact that fatigue design requirements, than static
strength requirements, normally control the required number of welded shear studs
on a composite girder. Thus, the use of partially composite design is not normally
used for new composite bridge girders. However, because of the outstanding fatigue
characteristics of the post-installed shear connectors, fatigue is not likely to control
the required number of shear connectors, thereby enabling partial composite design.
The cost of post-installed shear connectors for an existing bridge is likely to be far
greater than the cost of welded studs for new construction. Full composite design
will therefore likely be very costly for strengthening existing bridges. Thus, the
economic viability of strengthening existing non-composite bridges by post-
installing shear connectors depends largely on the use of partial composite design.
• To evaluate overall system performance of a steel bridge girder strengthened with
post-installed shear connectors, three large scale beam tests were conducted. These
tests were conducted on a 38-ft long simply supported span, with a point load
applied at mid-span. Each specimen consisted of a W30x99 steel girder with a 7-in.
thick by 7-ft wide reinforced concrete slab on top. For one of the three specimens,
no shear connectors were provided, to provide baseline data on the strength and
stiffness of a non-composite girder. The test of the non-composite specimen showed
that the stiffness and ultimate strength of the girder was controlled by the stiffness
and strength of the W30x99 girder, with a negligible contribution from the slab. At
very low load levels, the non-composite specimen exhibited some degree of
composite action, likely due to bond at the steel-concrete interface. However, this
composite action only occurred at very low load levels. Once the load exceed about
10% of the girder’s full capacity, this composite action ended, and the girder
subsequently behaved in an almost purely non-composite manner. When evaluating
existing non-composite bridges, it is sometimes surmised that some degree of
composite action can be considered when load rating the girders, resulting from
bond and friction between the steel and concrete. However, the test results for the
non-composite specimen suggest that such “unintended” composite action should
not be relied upon in evaluating the strength of existing non-composite girders.
• Two large scale beam specimens were retrofitted with post-installed shear
connectors; one with double-nut bolts and the other with adhesive anchors. Due to
cost constraints, a large scale beam test was not conducted with the high tension
105
friction grip bolt. Each of the retrofitted beam specimens were designed as partially
composite, with a 30% shear connection ratio. That is, the number of shear
connectors installed in these specimens was only 30% of the number required for
full composite design. This resulted in a pair of shear connectors (one on either side
of the beam web) located at intervals of 28.5-in. along the length of the beam. The
ultimate strength of the specimen retrofitted with double-nut bolt shear connectors
was 42% greater than the baseline non-composite specimen. Similarly, the ultimate
strength of the specimen retrofitted with adhesive anchors was 47% greater than the
baseline non-composite specimens. Consequently, a large increase in strength, on
the order of 45%, was achieved with a relatively small number of shear connectors,
demonstrating the efficiency of partial composite design. Further, the elastic
stiffness of the retrofitted beams was about 90 to 100% greater than the baseline
non-composite specimen.
• The strength of the retrofitted beams was controlled by the strength of the shear
connectors. When the shear connectors failed, the strength of the retrofitted beams
dropped sharply, to a level corresponding to the non-composite specimen. That is,
once the shear connectors failed, the behavior of the retrofitted beams reverted back
to the original non-composite condition. The retrofitted beams exhibited less
ductility than the baseline non-composite specimen.
• The strength of the retrofitted beams was well predicted by simple plastic cross-
sectional analysis for partial composite behavior, with shear connector strength
computed per Eq. 6.1. Thus, it appears that the strength of retrofitted beams can be
computed using simple and well established design procedures for partial composite
beams. These procedures are available in many texts on steel design, and are also
reviewed in Chapter 2 of this report (see Section 2.5.1.2). Similarly, the stiffness of
the retrofitted beams was well predicted using the simple expression for the
effective moment of inertia for partial composite girders that is provided in the
commentary to the AISC Specification for Structural Steel Buildings (see Eq. 2.25
in this report).
106
• Use of partial composite design is recommended as an overall basis for
strengthening steel bridge girders with post-installed shear connectors. Use of a
composite ratio less than 30% is not recommended, due to the lack of test results in
this range. The flexural strength of the retrofitted partial composite cross-section
can be computed using simple plastic cross-section analysis.
• The use of Equation 6.1 is recommended for computing the strength of post-
installed shear connectors.
• Pending the availability of additional fatigue test results, it is suggested that the
fatigue strength of post-installed shear connectors be checked using Equation 4.2,
where the stress range on the connector is determined with elastic analysis. Due to
the superior fatigue strength of the post-installed shear connectors, it is anticipated
that fatigue will not normally control the required number of shear connectors.
• It is recommended that general requirements concerning clear cover, edge distance,
and minimum distance between shear connectors in AASHTO Standard
Specifications be followed. AASHTO limits the maximum distance between shear
connectors to 24-in. This limit will often be violated in a partial composite design.
The full-scale beam tests conducted in this study also violated this limit, with no
apparent detrimental effects. Consequently, there appears to be no need to limit the
maximum spacing of shear connectors to 24-in.
107
108
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