# Experimental Study on Strain Penetration Effects in Fixed-End Rotation of RC Beam-Column Connections with High-Strength Reinforcement

Authors: Ling Li; Wenzhong Zheng; Ying Wang; Junke Ma
Journal: Advances in Materials Science and Engineering
 (2018)

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## Abstract

The additional fixed-end rotation resulting from the strain penetration of longitudinal reinforcement in a reinforced concrete beam-column connection is a crucial factor for the plastic hinge rotation capacity. When it comes to high-strength reinforcement, the effects of strain penetration on fixed-end rotation become more obvious because of the increase in yield strength. In this study, 42 beam-column connections with high-strength hot rolled ribbed bars were designed and tested under monotonic loading at the beam end. The test results show that the rebar strains gradually decrease from the critical section towards the beam-column connection, thereby proving the existence of strain penetration in the beam-column connection. The slippage of the embedment reinforcement at the beam-column interface and additional fixed-end rotations were obtained from the test results. In addition, a parametric study involving the yield strength and diameter of reinforcement, concrete tensile strength, and embedment length in the beam-column connection was performed to investigate the effects of various parameters on the additional fixed-end rotation. Finally, a new simple and practical calculation model for predicting the additional fixed-end rotation was proposed. The prediction shows good agreement with the experimental results.


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## Body

## 1. Introduction

For reinforced concrete frame structures, the performance of a plastic hinge designed to form at the beam end of the beam-column connection is critical for moment redistribution, deformation capacities, and seismic behaviour of the structures [1]. As the moment is maximum at the critical section of the beam end, a concrete crack will develop and the tensile force at this section is sustained only by the steel reinforcement. Recent research studies have shown that owing to the bond between concrete and reinforcement, the rebar strain penetration extends bilaterally from the critical section toward both shear span and beam-column connection, which all contribute to the rotation of the plastic hinge [2]. This paper focuses on the latter terms of strain penetration. A slippage of the reinforcement at the beam-column interface is observed because of the accumulation of the rebar strain along the embedment length in the beam-column connection. This slippage is different from the one due to the bond failure and will result in an additional fixed-end rotation, which in turn affects the rotation of the plastic hinge region.Numerous analytical methods on slippage due to strain penetration have been proposed. Some researchers determined the reinforcement strain over the embedment length with a varying local bond-slip relationship [3–9]. This required using iteration loop algorithms to achieve equilibrium of the steel bar. Although this method exhibits good accuracy, the process of this method is complicated. To facilitate the computation, simpler models have been proposed [10–13], such as the stepped local bond-slip relationship derived from the experimental results obtained by Alsiwat and Saatcioglu [10]. Using this type of local bond-slip relationship, an analytical model of slippage was established by Sezen and Setzler [12] for the cases wherein the embedded length is lower than the development length. Moreover, Tastani and Pasntazopoulou [13] proposed an expression to determined the bar slippage with the rebar strain as variable. For determining the additional fixed-end rotation, several other analytical models have been proposed by using the finite element method. For simplicity, nonlinear rotational springs have been used at the beam-column connection to simulate the end rotation [14–17]. The properties of the springs are obtained using an empirical method; however, this reduces the accuracy of the model. Zhao and Sritharan [18] used a zero-length section element to simulate the fixed-rotation at the beam-column interface by performing a fibre-based analysis. In addition, Paulay and Priestley [19] incorporated the effect of strain penetration on the fixed-end rotation into the equivalent plastic length Lsp using the relationship Lsp = 0.022fydb, in which the yield strength fy and diameter of the steel bar db were taken into consideration. Despite the convenience of application, many other factors that affect the properties of slippage were not considered in this method. Tastani and Pasntazopoulou [13] established an analytical expression where the strain penetration length is directly related to the residual bond strength, the diameter, and the hardening modulus of steel bars.Most of the aforementioned studies were based on theoretical analyses. In this paper, an experimental study on the additional fixed-end rotation of reinforced concrete beam-column connections due to strain penetration is presented. 18 interior beam-column connections with straight high-strength reinforcement and 24 exterior beam-column connections with hooked and headed high-strength reinforcement were tested under monotonic loading. The parameters that potentially affect the slippage of the embedment reinforcement in the beam-column connection, including the yield strength and diameter of the high-strength reinforcement, concrete tensile strength, and embedment length in the beam-column connection were investigated to obtain the development trends of the additional fixed-end rotation with respect to each parameter. The main objective of this study was to propose a simple calculation model of the addition fixed-end rotation due to strain penetration at the yielding (rebar strain at the critical section reaches the yield strain) and nominal ultimate states (concrete strain in the extreme compressed fibre reaches the ultimate strain). In this model, the parameters generally used in the structural design are considered instead of the ones used in the theoretical derivation to make the proposed model more practical.


## 2. Experimental Program

### 2.1. Specimen Details

A total of 30 specimens were designed and tested in this study. Each specimen comprises two cantilever beams, a middle column, and a bottom beam. The specimens were divided into two types, as listed in Table1. 18 specimens were used to model the interior beam-column connections, labelled using the letter I as the first letter. 12 specimens were used to model the exterior beam-column connections, each of which were investigated as two exterior beam-column connections and labelled using the letter E as the first letter. The cantilever beams of all the specimens have the same rectangular cross section of 200 mm × 350 mm with an overall length of 1000 mm. For the I-type specimens, the cross-sectional width of each middle column was 300 mm; however, different cross-sectional depths, i.e., 400 mm, 600 mm, and 800 mm, were set to study the strain penetration of the tensile reinforcement with different embedment lengths throughout the beam-column connections. The height of each column was 1100 mm. For the E-type specimens, the height and cross-sectional dimension of the middle columns were 1350 mm and 300 mm × 450 mm, respectively. Four control variables were considered in the design, namely, the yield strength of the tensile reinforcement, the diameter of the tensile reinforcement in the beam-column connection, straight embedment length of the tensile reinforcement in the beam-column connection, and the concrete grade. These variables were all reflected in the “specimens No.” The grades of the tensile reinforcement were HRB500 and HRB600 (specified in the Chinese code for design of concrete structures GB 50010-2010 [20]), represented by the second letter in the “specimens No.,” corresponding to the letters A and B, respectively. The subsequent number indicates the straight embedment length of the tensile reinforcement in the beam-column connection. The levels of the concrete grade were C40, C50, and C60 as per the Chinese code [20], corresponding to the third term in the “specimen No.” The last term represents the diameter of the tensile reinforcement. For example, “IA-400-C40-18” represents an interior beam-column connection with a tensile reinforcement grade of HRB500 and a concrete grade of C40. The straight embedment length and the diameter of the tensile reinforcement in the beam-column connection are 400 mm and 18 mm, respectively.Table 1
Reinforcement of the test specimens.
No.
Beam
Column
Beam no.
Top ①
Tensile reinforcement ratios (%)
Stirrup ③
Stirrup ratios (%)
Anchorage type
l
a/lah (mm)
Longitudinal reinforcement ④
Stirrup ⑤
1
IA-400-C40-18
318
1.17
10@100
0.79
—
400
818
10@100
2
IA-600-C40-20
220
0.97
10@100
0.79
—
600
818
10@100
3
IA-800-C40-22
222
1.17
10@80
0.98
—
800
1018
10@100
4
IA-400-C50-18
318
1.17
10@100
0.79
—
400
818
10@100
5
IA-600-C50-20
320
1.45
10@100
0.79
—
600
818
10@100
6
IA-800-C50-22
222
1.17
10@80
0.98
—
800
1018
10@100
7
IA-400-C60-18
318
1.17
10@100
0.79
—
400
818
10@100
8
IA-600-C60-20
320
1.45
10@100
0.79
—
600
818
10@100
9
IA-800-C60-22
322
1.17
10@80
0.98
—
800
1018
10@100
10
IB-400-C40-18
318
1.17
10@100
0.79
—
400
818
10@100
11
IB-600-C40-20
220
0.97
10@100
0.79
—
600
818
10@100
12
IB-800-C40-22
222
1.17
10@80
0.98
—
800
1018
10@100
13
IB-400-C50-18
318
1.17
10@100
0.79
—
400
818
10@100
14
IB-600-C50-20
220
0.97
10@100
0.79
—
600
818
10@100
15
IB-800-C50-22
222
1.17
10@80
0.98
—
800
1018
10@100
16
IB-400-C60-18
318
1.17
10@100
0.79
—
400
818
10@100
17
IB-600-C60-20
320
1.45
10@100
0.79
—
600
818
10@100
18
IB-800-C60-22
222
1.17
10@80
0.98
—
800
1018
10@100
19
EA-430-C40-18
318
1.17
10@100
0.79
Straight
430
818
10@100
EA-210-C40-22
222
1.17
10@100
0.79
Hooked
210
818
20
EA-330-C40-20
220
0.97
10@150
0.52
Hooked
330
818
10@100
EA-190-C40-20
220
0.97
10@150
0.52
Headed
190
818
21
EA-380-C50-18
318
1.17
10@150
0.52
Straight
380
818
10@100
EA-190-C50-22
222
1.17
10@150
0.52
Hooked
190
818
22
EA-300-C50-20
320
1.45
10@100
0.79
Hooked
300
818
10@80
EA-420-C50-20
320
1.45
10@100
0.79
Straight
420
818
23
EA-350-C60-18
318
1.17
10@150
0.52
Straight
350
818
10@100
EA-300-C60-22
222
1.17
10@150
0.52
Hooked
300
818
24
EA-270-C60-20
320
1.45
10@100
0.79
Headed
270
818
10@80
EA-160-C60-20
320
1.45
10@100
0.79
Hooked
160
818
25
EB-420-C40-18
318
1.17
10@100
0.79
Straight
420
818
10@100
EB-230-C40-22
222
1.17
10@100
0.79
Hooked
230
818
26
EB-380-C40-20
220
0.97
10@150
0.52
Hooked
380
818
10@100
EB-220-C40-20
220
0.97
10@150
0.52
Headed
220
818
27
EB-420-C50-18
318
1.17
10@100
0.79
Straight
420
818
10@100
EB-210-C50-22
222
1.17
10@100
0.79
Hooked
210
818
28
EB-340-C50-20
220
0.97
10@150
0.52
Hooked
340
818
10@100
EB-420-C50-20
220
0.97
10@150
0.52
Straight
420
818
29
EB-400-C60-18
318
1.17
10@100
0.79
Straight
400
818
10@100
EB-340-C60-22
222
1.17
10@150
0.52
Hooked
340
818
30
EB-310-C60-20
320
1.45
10@80
0.98
Headed
310
818
10@80
EB-180-C60-20
320
1.45
10@80
0.98
Hooked
180
818
This table should be read in conjunction with Figure1. The bottom longitudinal reinforcements in all the cantilever beams were denoted by ②, as shown in the cross section A-A in Figure 1. Two HRB400 steel bars with a diameter of 10 mm were used as ② steel bars. The top and bottom longitudinal reinforcements in all the bottom beams of the specimens were denoted by ⑥, as shown in the cross section C-C in Figure 1. Three HRB400 steel bars with a diameter of 18 mm were used as ⑥ steel bars. The transverse reinforcement in all the bottom beams of the specimens were denoted by ⑦, as shown in the cross section C-C in Figure 1. HPB300 steel bars with a diameter of 10 mm were used as ⑦ steel bars with a spacing of 100 mm. , , , and , respectively, indicate reinforcement grades of HPB300, HRB400, HRB500, and HRB600. 210 bars ② were used as the bottom longitudinal reinforcements in all the cantilever beams. In the bottom beams of the specimens, 318 bars ⑥ were used as the top and bottom longitudinal reinforcements and 10 bars with a spacing of 100 mm ⑦ were used as the transverse reinforcement.To ensure that the test beams exhibit good ductile performance and to prevent brittle failure, appropriate tensile reinforcement ratios varying from 0.9%–1.5% were selected for the cantilever beams. Meanwhile, sufficient stirrups were arranged in all the beams to avoid shear failure, and the strong column-weak beam requirement was followed in the design. Table1 and Figure 1 present the details of reinforcement arrangement and specimen dimensions, respectively.Figure 1
Details of the reinforcement arrangement and specimen size. (a) Interior beam-column connection. (b) Exterior beam-column connection.
(a)
(b)


### 2.2. Materials Properties

The material tests included the tensile test for reinforcement and compressive cube test for concrete. The reinforcements are tested under uniaxial tension. The gauge length of the reinforcement is 500 mm, and the reinforcement stress is evaluated based on the nominal diameter of the bars. The stress-strain relationships of the tensile reinforcement are shown in Figure2, and the values of the measured parameters are listed in Table 2. The cubic strength of the concrete fcu was calculated using cubes with a side of 150 mm, tested along with the test specimens. The cubes were prepared and cured in the same manner as the test specimens. Table 3 lists the properties of the concrete.Figure 2
Stress-strain relationships of the tensile reinforcement.Table 2
Material properties of reinforcement.
Grade
Diameter(mm)
Yield strengthfy (MPa)
Ultimate strengthfu (MPa)
Yield strainεy
Percentage elongation at maximum forceεu
HPB300
10
381
513
0.00191
0.150
HRB400
10
498
632
0.00249
0.148
18
460
621
0.00230
0.136
HRB500
18
590
760
0.00295
0.116
20
581
732
0.00291
0.122
22
543
713
0.00272
0.113
HRB600
18
631
825
0.00316
0.108
20
654
837
0.00327
0.104
22
628
801
0.00314
0.107Table 3
Materials properties of concrete.
Grade
C40
C50
C60
Cubic strength,fcu (MPa)
50.6
59.2
74.3
Compressive strength,fc′ (MPa)
40.5
47.4
61.9
Tensile strength,fct (MPa)
3.41
3.73
4.22
For concrete below C50 grade, the compressive strengthfc′ was calculated as 0.8 times the cubic strength fcu; the compressive strength fc′ of C60 concrete was calculated as 0.833 times the cubic strength fcu; the tensile strength fct was calculated by fct = 0.395 fcu0.55 [20].


### 2.3. Test Setup and Procedure

Figure3 shows the test rigs and instrumentations. The bottom beam was connected to the ground with two symmetrical bolts on both sides of the middle column. A point monotonic load was applied symmetrically using two loading jacks at the end of the cantilever beams. A sensor was placed on each loading jack to measure the value of the applied loads and to ensure that the two loads are equal at all times. Two displacement transducers were located underneath the loading point to measure the deflection of the beams. In particular, for the E-type specimens, the heights of the two cantilever beams on both sides of the column were different, as shown in Figure 1(b). In order to prevent the cracks on the sides of the column from affecting strain penetration, an eccentric axial force was applied at the top of the column to balance the flexure moment of the column, as shown in Figure 3(b). Strain gauges with a width of 1 mm and length of 2 mm were attached at the intervals of 40 mm to investigate the strain penetration of the longitudinal tensile reinforcement in the beam-column connections. Figure 4 shows the locations of the strain gauges. To accurately obtain the strain, the strain gauges were placed along the notch of the reinforcement, which was slotted adjacent to the longitudinal ribs, as shown in Figure 5. In this way, the loss of the effective area of the bars and the influence on the bonding performance of the tensile longitudinal reinforcement were minimised to a significant extent.Figure 3
Test rigs and instrumentations. (a) Interior beam-column connection test: (i) schematic; (ii) photograph. (b) Exterior beam-column connection test: (i) schematic; (ii) photograph. (1) Rolling hinge support. (2) Loading jack. (3) Loading sensor. (4) Blade hinge support. (5) Trestle. (6) Displacement transducers. (7) Dial indicator. (8) Extensometer.
(a)
(b)Figure 4
Configuration of strain gauges. (a) Interior beam-column connection. (b) Exterior beam-column connection.
(a)
(b)Figure 5
Strain gauges attached along the notch. (a) Photograph. (b) Schematic.
(a)
(b)


## 2.1. Specimen Details

A total of 30 specimens were designed and tested in this study. Each specimen comprises two cantilever beams, a middle column, and a bottom beam. The specimens were divided into two types, as listed in Table1. 18 specimens were used to model the interior beam-column connections, labelled using the letter I as the first letter. 12 specimens were used to model the exterior beam-column connections, each of which were investigated as two exterior beam-column connections and labelled using the letter E as the first letter. The cantilever beams of all the specimens have the same rectangular cross section of 200 mm × 350 mm with an overall length of 1000 mm. For the I-type specimens, the cross-sectional width of each middle column was 300 mm; however, different cross-sectional depths, i.e., 400 mm, 600 mm, and 800 mm, were set to study the strain penetration of the tensile reinforcement with different embedment lengths throughout the beam-column connections. The height of each column was 1100 mm. For the E-type specimens, the height and cross-sectional dimension of the middle columns were 1350 mm and 300 mm × 450 mm, respectively. Four control variables were considered in the design, namely, the yield strength of the tensile reinforcement, the diameter of the tensile reinforcement in the beam-column connection, straight embedment length of the tensile reinforcement in the beam-column connection, and the concrete grade. These variables were all reflected in the “specimens No.” The grades of the tensile reinforcement were HRB500 and HRB600 (specified in the Chinese code for design of concrete structures GB 50010-2010 [20]), represented by the second letter in the “specimens No.,” corresponding to the letters A and B, respectively. The subsequent number indicates the straight embedment length of the tensile reinforcement in the beam-column connection. The levels of the concrete grade were C40, C50, and C60 as per the Chinese code [20], corresponding to the third term in the “specimen No.” The last term represents the diameter of the tensile reinforcement. For example, “IA-400-C40-18” represents an interior beam-column connection with a tensile reinforcement grade of HRB500 and a concrete grade of C40. The straight embedment length and the diameter of the tensile reinforcement in the beam-column connection are 400 mm and 18 mm, respectively.Table 1
Reinforcement of the test specimens.
No.
Beam
Column
Beam no.
Top ①
Tensile reinforcement ratios (%)
Stirrup ③
Stirrup ratios (%)
Anchorage type
l
a/lah (mm)
Longitudinal reinforcement ④
Stirrup ⑤
1
IA-400-C40-18
318
1.17
10@100
0.79
—
400
818
10@100
2
IA-600-C40-20
220
0.97
10@100
0.79
—
600
818
10@100
3
IA-800-C40-22
222
1.17
10@80
0.98
—
800
1018
10@100
4
IA-400-C50-18
318
1.17
10@100
0.79
—
400
818
10@100
5
IA-600-C50-20
320
1.45
10@100
0.79
—
600
818
10@100
6
IA-800-C50-22
222
1.17
10@80
0.98
—
800
1018
10@100
7
IA-400-C60-18
318
1.17
10@100
0.79
—
400
818
10@100
8
IA-600-C60-20
320
1.45
10@100
0.79
—
600
818
10@100
9
IA-800-C60-22
322
1.17
10@80
0.98
—
800
1018
10@100
10
IB-400-C40-18
318
1.17
10@100
0.79
—
400
818
10@100
11
IB-600-C40-20
220
0.97
10@100
0.79
—
600
818
10@100
12
IB-800-C40-22
222
1.17
10@80
0.98
—
800
1018
10@100
13
IB-400-C50-18
318
1.17
10@100
0.79
—
400
818
10@100
14
IB-600-C50-20
220
0.97
10@100
0.79
—
600
818
10@100
15
IB-800-C50-22
222
1.17
10@80
0.98
—
800
1018
10@100
16
IB-400-C60-18
318
1.17
10@100
0.79
—
400
818
10@100
17
IB-600-C60-20
320
1.45
10@100
0.79
—
600
818
10@100
18
IB-800-C60-22
222
1.17
10@80
0.98
—
800
1018
10@100
19
EA-430-C40-18
318
1.17
10@100
0.79
Straight
430
818
10@100
EA-210-C40-22
222
1.17
10@100
0.79
Hooked
210
818
20
EA-330-C40-20
220
0.97
10@150
0.52
Hooked
330
818
10@100
EA-190-C40-20
220
0.97
10@150
0.52
Headed
190
818
21
EA-380-C50-18
318
1.17
10@150
0.52
Straight
380
818
10@100
EA-190-C50-22
222
1.17
10@150
0.52
Hooked
190
818
22
EA-300-C50-20
320
1.45
10@100
0.79
Hooked
300
818
10@80
EA-420-C50-20
320
1.45
10@100
0.79
Straight
420
818
23
EA-350-C60-18
318
1.17
10@150
0.52
Straight
350
818
10@100
EA-300-C60-22
222
1.17
10@150
0.52
Hooked
300
818
24
EA-270-C60-20
320
1.45
10@100
0.79
Headed
270
818
10@80
EA-160-C60-20
320
1.45
10@100
0.79
Hooked
160
818
25
EB-420-C40-18
318
1.17
10@100
0.79
Straight
420
818
10@100
EB-230-C40-22
222
1.17
10@100
0.79
Hooked
230
818
26
EB-380-C40-20
220
0.97
10@150
0.52
Hooked
380
818
10@100
EB-220-C40-20
220
0.97
10@150
0.52
Headed
220
818
27
EB-420-C50-18
318
1.17
10@100
0.79
Straight
420
818
10@100
EB-210-C50-22
222
1.17
10@100
0.79
Hooked
210
818
28
EB-340-C50-20
220
0.97
10@150
0.52
Hooked
340
818
10@100
EB-420-C50-20
220
0.97
10@150
0.52
Straight
420
818
29
EB-400-C60-18
318
1.17
10@100
0.79
Straight
400
818
10@100
EB-340-C60-22
222
1.17
10@150
0.52
Hooked
340
818
30
EB-310-C60-20
320
1.45
10@80
0.98
Headed
310
818
10@80
EB-180-C60-20
320
1.45
10@80
0.98
Hooked
180
818
This table should be read in conjunction with Figure1. The bottom longitudinal reinforcements in all the cantilever beams were denoted by ②, as shown in the cross section A-A in Figure 1. Two HRB400 steel bars with a diameter of 10 mm were used as ② steel bars. The top and bottom longitudinal reinforcements in all the bottom beams of the specimens were denoted by ⑥, as shown in the cross section C-C in Figure 1. Three HRB400 steel bars with a diameter of 18 mm were used as ⑥ steel bars. The transverse reinforcement in all the bottom beams of the specimens were denoted by ⑦, as shown in the cross section C-C in Figure 1. HPB300 steel bars with a diameter of 10 mm were used as ⑦ steel bars with a spacing of 100 mm. , , , and , respectively, indicate reinforcement grades of HPB300, HRB400, HRB500, and HRB600. 210 bars ② were used as the bottom longitudinal reinforcements in all the cantilever beams. In the bottom beams of the specimens, 318 bars ⑥ were used as the top and bottom longitudinal reinforcements and 10 bars with a spacing of 100 mm ⑦ were used as the transverse reinforcement.To ensure that the test beams exhibit good ductile performance and to prevent brittle failure, appropriate tensile reinforcement ratios varying from 0.9%–1.5% were selected for the cantilever beams. Meanwhile, sufficient stirrups were arranged in all the beams to avoid shear failure, and the strong column-weak beam requirement was followed in the design. Table1 and Figure 1 present the details of reinforcement arrangement and specimen dimensions, respectively.Figure 1
Details of the reinforcement arrangement and specimen size. (a) Interior beam-column connection. (b) Exterior beam-column connection.
(a)
(b)


## 2.2. Materials Properties

The material tests included the tensile test for reinforcement and compressive cube test for concrete. The reinforcements are tested under uniaxial tension. The gauge length of the reinforcement is 500 mm, and the reinforcement stress is evaluated based on the nominal diameter of the bars. The stress-strain relationships of the tensile reinforcement are shown in Figure2, and the values of the measured parameters are listed in Table 2. The cubic strength of the concrete fcu was calculated using cubes with a side of 150 mm, tested along with the test specimens. The cubes were prepared and cured in the same manner as the test specimens. Table 3 lists the properties of the concrete.Figure 2
Stress-strain relationships of the tensile reinforcement.Table 2
Material properties of reinforcement.
Grade
Diameter(mm)
Yield strengthfy (MPa)
Ultimate strengthfu (MPa)
Yield strainεy
Percentage elongation at maximum forceεu
HPB300
10
381
513
0.00191
0.150
HRB400
10
498
632
0.00249
0.148
18
460
621
0.00230
0.136
HRB500
18
590
760
0.00295
0.116
20
581
732
0.00291
0.122
22
543
713
0.00272
0.113
HRB600
18
631
825
0.00316
0.108
20
654
837
0.00327
0.104
22
628
801
0.00314
0.107Table 3
Materials properties of concrete.
Grade
C40
C50
C60
Cubic strength,fcu (MPa)
50.6
59.2
74.3
Compressive strength,fc′ (MPa)
40.5
47.4
61.9
Tensile strength,fct (MPa)
3.41
3.73
4.22
For concrete below C50 grade, the compressive strengthfc′ was calculated as 0.8 times the cubic strength fcu; the compressive strength fc′ of C60 concrete was calculated as 0.833 times the cubic strength fcu; the tensile strength fct was calculated by fct = 0.395 fcu0.55 [20].


## 2.3. Test Setup and Procedure

Figure3 shows the test rigs and instrumentations. The bottom beam was connected to the ground with two symmetrical bolts on both sides of the middle column. A point monotonic load was applied symmetrically using two loading jacks at the end of the cantilever beams. A sensor was placed on each loading jack to measure the value of the applied loads and to ensure that the two loads are equal at all times. Two displacement transducers were located underneath the loading point to measure the deflection of the beams. In particular, for the E-type specimens, the heights of the two cantilever beams on both sides of the column were different, as shown in Figure 1(b). In order to prevent the cracks on the sides of the column from affecting strain penetration, an eccentric axial force was applied at the top of the column to balance the flexure moment of the column, as shown in Figure 3(b). Strain gauges with a width of 1 mm and length of 2 mm were attached at the intervals of 40 mm to investigate the strain penetration of the longitudinal tensile reinforcement in the beam-column connections. Figure 4 shows the locations of the strain gauges. To accurately obtain the strain, the strain gauges were placed along the notch of the reinforcement, which was slotted adjacent to the longitudinal ribs, as shown in Figure 5. In this way, the loss of the effective area of the bars and the influence on the bonding performance of the tensile longitudinal reinforcement were minimised to a significant extent.Figure 3
Test rigs and instrumentations. (a) Interior beam-column connection test: (i) schematic; (ii) photograph. (b) Exterior beam-column connection test: (i) schematic; (ii) photograph. (1) Rolling hinge support. (2) Loading jack. (3) Loading sensor. (4) Blade hinge support. (5) Trestle. (6) Displacement transducers. (7) Dial indicator. (8) Extensometer.
(a)
(b)Figure 4
Configuration of strain gauges. (a) Interior beam-column connection. (b) Exterior beam-column connection.
(a)
(b)Figure 5
Strain gauges attached along the notch. (a) Photograph. (b) Schematic.
(a)
(b)


## 3. Experimental Results

### 3.1. Global Behaviour of Test Specimens

Figure6 shows the variation in the load with respect to the vertical displacement of the test specimens in the loading process. All the specimens were observed to experience four stages: the appearance of the first major crack (Point A), yielding state (Point B), nominal ultimate limit state (Point C), and actual ultimate limit state (Point D). Among these, the yielding state is defined as the state when the strain of the tensile reinforcement at the critical section reaches the yield strain. The nominal flexural strength of the critical section is reached when the strain in the extreme compressed fibre reaches the ultimate strain [21], which is defined as the nominal ultimate limit state in this paper. Furthermore, the real ultimate limit state corresponds to the maximum load-carrying resistance of the specimens.Figure 6
Load versus displacement curve. (a) IA/B-C40-18. (b) IA/B-C40-20. (c) IA/B-C40-22. (d) IA/B-C50-18. (e) IA/B-C50-20. (f) IA/B-C50-22. (g) IA/B-C60-18. (h) IA/B-C60-20. (i) IA/B-C60-22. (j) EA/B-C40-18/22. (k) EA/B-C40-20. (l) EA/B-C50-18/22. (m) EA/B-C50-20. (n) EA/B-C60-18/22. (o) EA/B-C60-20.
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
(k)
(l)
(m)
(n)
(o)From the start of the test until Point A, the specimens did not crack and their deformations were linearly elastic. At Point A, first major cracks appeared at the section adjacent to the beam-column connection (Figure7(b)). With the increase in the load, more cracks gradually developed in the span (Figure 7(a)) and the beams behaved quite linearly in the deflection curves before Point B. After Point B, the deformation increased relatively quickly with the increase in the load. The number of cracks no longer increased; however, the width of cracks increased. It should be noted that the distances among the cracks are important for strain penetration in the shear span, which has been comprehensively studied by Megaloopikonomou et al. [2]. The region, ranging from the crack section toward the uncrack part of the shear span until the rebar strain coordinates with the deformation of the surrounding concrete cover, was defined as the “disturbed” region. In view of whether the next crack is formed in the “disturbed” region of the previous crack, different methods for evaluating the strain and slip of the reinforcement along the shear span have been proposed in the literature [2]. At Point C, a slight concrete compressive failure was observed at the critical cross section. Subsequently, more horizontal compressive cracks gradually developed at the compressive zone near the critical section (Figure 7(c)). However, the load was largely constant with the rapid increase in the deflection. It can be explained that the confined stirrups of the beams (the range of stirrup volumetric ratios is 1.2%∼1.9%) would improve the ultimate compressive strength and ultimate strain of the confined compression concrete to some extent, thereby improving the ductilities of the test beam. Until the peak Point D, the concrete was obviously crushed (Figure 7(d)) and the curves entered the descending stage that the load decreased with the increase in the deflection. As shown in Figure 6, the deflections of the east span beam and west span beam for the one specimen were largely symmetrical owing to their equal longitudinal steel ratios. For each comparison group with the same concrete grade and the same ratios of the tensile reinforcement, a very similar behaviour was observed before the yielding state (Point B). After Point B, the beams with a higher grade of reinforcement developed a higher flexural capacity. Tables 4 and 5 list the loads corresponding to the characteristic point of the specimens.Figure 7
Photographs from the experimental study. (a) Crack distribution in the shear span. (b) First crack at the section adjacent to the beam-column connection. (c) Horizontal compressive cracks developed at the compressive zone. (d) Compressive concrete was obviously crushed.
(a)
(b)
(c)
(d)Table 4
Load of the interior beam-column connection at characteristic points.
Specimen No.
Crack load (kN)
Yield load (kN)
Nominal ultimate load (kN)
Peak load (kN)
E
W
E
W
E
W
E
W
IA-400-C40-18
19.5
24
107
102
127
127
129
129
IA-400-C50-18
25.5
25.5
115
100
135
135
135
135
IA-400-C60-18
24
21
113
117
127
129
129
130
IA-600-C40-20
15
15
109
113
121
121
127
125
IA-600-C50-20
25.5
32
177
182
192
192
202
192
IA-600-C60-20
24
27
160
160
180
180
175
177
IA-800-C40-22
21
21
116
122
140
137
145
146
IA-800-C50-22
21
21
127
122
142
142
147
150
IA-800-C60-22
21
19.5
170
170
211
208
221
213
IB-400-C40-18
18
18
122
122
152
152
157
156
IB-400-C50-18
21
21
130
140
150
150
156
159
IB-400-C60-18
19.5
19.5
130
130
155
155
162
160
IB-600-C40-20
18
18
115
115
139
135
140
140
IB-600-C50-20
18
18
114
104
134
134
142
134
IB-600-C60-20
24
24
170
160
205
200
220
208
IB-800-C40-22
16.5
15
137
142
157
157
167
168
IB-800-C50-22
18
18
142
142
175
167
184
174
IB-800-C60-22
22.5
22.5
130
120
165
165
175
165
E represents the east span of the interior beam-column connection, andW represents the west span of the interior beam-column connection.Table 5
Load of the exterior beam-column connection at characteristic points.
Specimen No.
Crack load (kN)
Yield load (kN)
Nominal ultimate load (kN)
Peak load (kN)
EA-430-C40-18
22.5
122.0
137.0
140.0
EA-380-C50-18
18.0
124.0
140.0
146.0
EA-420-C50-20
21.0
160.0
180.0
188.0
EA-350-C60-18
21.0
91.0
136.0
158.0
EA-330-C40-20
18.0
102.0
114.0
122.8
EA-300-C50-20
18.0
140.0
180.0
190.0
EA-270-C60-20
24.0
125.0
170.0
171.7
EA-300-C60-22
16.5
86.0
121.0
135.0
EA-190-C40-20
18.0
99.0
114.0
126.1
EA-210-C40-22
18.0
122.0
137.0
137.0
EA-190-C50-22
18.0
124.0
140.0
154.1
EA-160-C60-20
16.5
145.0
170.0
174.7
EB-420-C40-18
27.0
150.0
170.0
176.8
EB-420-C50-18
19.5
125.0
150.0
186.0
EB-420-C50-20
18.0
116.0
131.0
146.0
EB-400-C60-18
22.5
150.0
170.0
175.0
EB-380-C40-20
21.0
105.0
140.0
145.0
EB-340-C50-20
18.0
126.0
146.0
157.5
EB-310-C60-20
21.0
180.0
215.0
215.0
EB-340-C60-22
22.5
130.0
155.0
164.0
EB-220-C40-20
21.0
130.0
145.0
149.4
EB-230-C40-22
16.5
130.0
150.0
170.0
EB-210-C50-22
16.5
140.0
175.0
189.0
EB-180-C60-20
21.0
165.0
190.0
215.0


### 3.2. Rebar Strain Distribution along the Embedment Length

Figures8 and 9 show the strain distribution (at the yielding and nominal ultimate limit states) of the straight embedment reinforcement in the interior beam-column connection and exterior beam-column connection, respectively. In Figure 8, the origin of the abscissa represents the midpoint of the continuous reinforcement through the interior beam-column connection, and the one in Figure 9 represents the free end near the headed part of the anchorage reinforcement in the exterior connection (consistent with Figure 4). The figures demonstrate the occurrence of strain penetration in the beam-column connection that the rebar strain gradually decreases from the critical section to the coordinate origin and consequently slippage at the beam-column interface. Moreover, for the same grade of reinforcement, the rebar strain at the coordinate origin decreases with the increase in the straight embedment length. A longer embedment length results in lower bond stresses near the coordinate origin; however, the accumulation of the bonding stresses along the embedment length increases, denoting a lower strain of reinforcement at the coordinate origin. At the nominal ultimate limit state, the rebar strains are concentrated near the beam-column interface, and they were observed to decrease sharply to the yield strain point and then decrease slowly until the coordinate origin.Figure 8
Strain distribution along the tensile reinforcement throughout the interior beam-column connection. Specimen type: (a) IA-C40; (b) IA-C50; (c) IA-C60; (d) IB-C40; (e) IB-C50; (f) IB-C60.
(a)
(b)
(c)
(d)
(e)
(f)Figure 9
Strain distribution along the tensile reinforcement anchored in the exterior beam-column connection. Specimen type: (a) EA-C40; (b) EA-C50; (c) EA-C60; (d) EB-C40; (e) EB-C50; (f) EB-C60.
(a)
(b)
(c)
(d)
(e)
(f)


### 3.3. Additional Fixed-End Rotation due to Strain Penetration

Figures10(a) and 10(b) illustrate the additional fixed-end rotation θslip at the beam-column interface due to the strain penetration of the tensile reinforcement inside the interior and exterior beam-column connections. θslip is equal to the slippage of the embedment reinforcement s divided by the depth of the tensile zone (d−xc) as follows:(1)θslip=sd−xc,where d is the effective depth of the section and xc is the depth of the neutral axis.Figure 10
Strain penetration of the longitudinal tensile reinforcement inside (a) interior beam-column connection and (b) exterior beam-column connection.
(a)
(b)As shown in Figure10(a), the local slip at the midpoint of the straight embedment reinforcement through the interior beam-column connection is zero when symmetrical loads are applied to the beam end. The embedment reinforcement can be considered to sustain the reverse symmetrical tensile force from the midpoint. If the concrete deformation is ignored, the slippage of the reinforcement s can be calculated by integrating the strain along half of the embedment length:(2)s=∫0lahεsxdx,where lah is half of the embedment length of the continuous reinforcement through the interior beam-column connection and εs is the rebar strain.As shown in Figure10(b), when hooked bars are used as longitudinal reinforcements in the exterior beam-column connection, a hook displacement occurs if the straight embedment length of the reinforcement is not sufficient. Hence, the slippage of the reinforcement s is the sum of the integral of the strain along the straight embedment length and the hook displacement as expressed in the following equation:(3)s=∫0lahεsxdx+δh,where lah is the straight lead length of the hooked bar and δh is the hook displacement.A model for the relationship between force resisted by the hook and hook displacement was proposed by Soroushian et al. [22] based on the experiments for the tensile behaviour of hook bars as shown in the following expressions:(4)Ph=Phuδh2.54,(5)Phu=2710.05db−0.25,(6)Phf=0.54Phu.The model shown in Figure11 is adopted here for predicting the hook displacement δh. The force resisted by the hook Ph can be calculated from the experimental results of the rebar strain at the free end of anchorage reinforcement combined with the stress-strain relationship of the reinforcement. Then, the hook displacement δh can be obtained using equations (4)–(6). Figure 12 shows the relationship between the relative straight embedment length lah/db and the ratio of the hook displacement δh to slippage s at the yielding and nominal ultimate limit states for each exterior beam-column connection. It can be seen that δh/s decreases with the increase in lah/db. The fitting curve shows that the ratio δh/s does not exceed 0.1 when lah is greater than 12db, which indicates that the effect of the hook displacement δh on s is negligible. The straight embedment length of the hooked bar or headed bar lah has been specified in most design specifications, as listed in Table 6. It can be known that the condition lah<12db rarely occurs in practice, thus the influence of δh is not considered in this paper. Similar to the hooked bars, when the headed bars are used as longitudinal reinforcements, the slip at the headed end of the bars is negligible.Figure 11
Hook force-hook deformation relationship.Figure 12
Relationship betweenlah/db and δh/s: (a) at the yielding state; (b) at the nominal ultimate state.
(a)
(b)Table 6
Design specifications for straight anchorage length of hooked or headed bar.
Code
Straight anchorage length of hooked or headed bar,lah
Commentary
ACI 318-14 [21]
l
ah
≥
0.02
ψ
e
f
y
/
λ
f
c
′
d
b
for hooked bar
l
ah
≥
0.016
ψ
e
f
y
/
λ
f
c
′
d
b
for headed bar
ψ
e = 1.2 for epoxy-coated reinforcement; ψe = 1.0 for other cases; λ = 0.75 for lightweight concrete; λ = 1.0 for other cases.
Chinese code (GB 50010-2010) [20]
l
ah
≥
0.4
l
ab
l
ab
=
α
f
y
/
f
t
d
b
f
y is the design value of the reinforcement tensile strength;ft is the design value of the concrete tensile strength;α = 0.14 for deformed bar; α = 0.16 for plain bar.
Eurocode 2-part 1-1 [23]
l
ah
≥
α
1
l
b,rqd
l
b,rqd
=
d
b
σ
sd
/
4
f
bd
f
bd
=
2.25
η
1
η
2
f
t
α
1 = 0.7 if cd > 3db; otherwise α1 = 1.0; σsd is the design stress of the bar at the position from where the anchorage is measured;η1 = 1.0 when “good” conditions are obtained;η1 = 0.7 for other cases; η2 = 1.0 for db ≤ 32 mm; η2 = (132−db)/100 for db > 32 mm.Based on the tensile strain distribution of the embedment reinforcement obtained from the test, the additional fixed-end rotation of the exterior and interior beam-column connections at the yielding and nominal ultimate limit states can be calculated by combining equations (1)–(3). The results are listed in Tables 7 and 8.Table 7
Additional fixed-end rotation of interior beam-column connection at yielding and nominal ultimate limit states.
Specimen no.
s
y (mm)
θ
y,slip (×10−3 rad)
s
u (mm)
θ
u,slip (×10−3 rad)
E
W
E
W
E
W
E
W
IA-400-C40-18
0.50
0.50
2.41
2.40
0.82
0.82
3.44
3.43
IA-400-C50-18
0.46
0.48
2.15
2.25
0.78
0.83
3.11
3.29
IA-400-C60-18
0.48
0.47
2.13
2.09
1.08
1.06
4.03
3.96
IA-600-C40-20
0.58
0.56
2.74
2.66
1.23
1.18
4.81
4.64
IA-600-C50-20
0.55
0.54
2.66
2.63
0.82
0.89
3.46
3.77
IA-600-C60-20
0.52
0.51
2.42
2.39
1.02
1.09
3.99
4.25
IA-800-C40-22
0.65
0.62
3.05
2.88
1.23
1.26
4.84
4.95
IA-800-C50-22
0.58
0.63
2.73
2.95
1.17
1.16
4.53
4.49
IA-800-C60-22
0.55
0.56
2.68
2.73
1.01
1.01
4.11
4.10
IB-400-C40-18
0.55
0.56
2.72
2.76
0.81
0.82
3.44
3.48
IB-400-C50-18
0.54
0.54
2.49
2.52
0.96
0.98
3.91
3.98
IB-400-C60-18
0.53
0.53
2.36
2.38
0.94
0.93
3.55
3.52
IB-600-C40-20
0.67
0.67
3.12
3.11
1.10
1.13
4.46
4.58
IB-600-C50-20
0.65
0.63
2.92
2.83
1.23
1.19
4.76
4.63
IB-600-C60-20
0.62
0.63
2.88
2.90
1.19
1.11
4.82
4.50
IB-800-C40-22
0.75
0.78
3.55
3.69
1.18
1.16
4.83
4.75
IB-800-C50-22
0.76
0.76
3.61
3.61
1.26
1.17
5.04
4.70
IB-800-C60-22
0.69
0.71
3.05
3.13
1.42
1.42
5.40
5.39Table 8
Additional fixed-end rotation of exterior beam-column connection at yielding and nominal ultimate states.
Specimen no.
s
y (mm)
θ
y,slip (×10−3 rad)
s
u (mm)
θ
u,slip (×10−3 rad)
EA-430-C40-18
0.70
3.37
1.16
4.83
EA-380-C50-18
0.68
3.28
1.23
4.94
EA-420-C50-20
0.78
3.90
1.26
5.43
EA-350-C60-18
0.67
2.98
1.23
4.68
EA-330-C40-20
0.69
3.24
1.27
4.95
EA-300-C50-20
0.67
3.36
1.09
4.70
EA-270-C60-20
0.58
2.72
1.03
4.11
EA-300-C60-22
0.62
2.77
1.09
4.09
EA-190-C40-20
0.46
2.14
0.88
3.45
EA-210-C40-22
0.43
2.10
0.80
3.22
EA-190-C50-22
0.43
2.00
0.95
3.74
EA-160-C60-20
0.43
2.00
0.77
3.08
EB-420-C40-18
0.80
3.84
1.25
5.28
EB-420-C50-18
0.77
3.60
1.25
5.10
EB-420-C50-20
0.80
3.80
1.28
5.00
EB-400-C60-18
0.71
3.17
1.26
4.81
EB-380-C40-20
0.82
3.92
1.40
5.91
EB-340-C50-20
0.70
3.15
1.20
4.67
EB-310-C60-20
0.67
3.11
1.22
4.95
EB-340-C60-22
0.75
3.34
1.26
4.78
EB-220-C40-20
0.59
2.81
1.09
4.61
EB-230-C40-22
0.58
2.86
0.96
4.03
EB-210-C50-22
0.54
2.55
0.97
3.89
EB-180-C60-20
0.50
2.30
0.80
3.24


## 3.1. Global Behaviour of Test Specimens

Figure6 shows the variation in the load with respect to the vertical displacement of the test specimens in the loading process. All the specimens were observed to experience four stages: the appearance of the first major crack (Point A), yielding state (Point B), nominal ultimate limit state (Point C), and actual ultimate limit state (Point D). Among these, the yielding state is defined as the state when the strain of the tensile reinforcement at the critical section reaches the yield strain. The nominal flexural strength of the critical section is reached when the strain in the extreme compressed fibre reaches the ultimate strain [21], which is defined as the nominal ultimate limit state in this paper. Furthermore, the real ultimate limit state corresponds to the maximum load-carrying resistance of the specimens.Figure 6
Load versus displacement curve. (a) IA/B-C40-18. (b) IA/B-C40-20. (c) IA/B-C40-22. (d) IA/B-C50-18. (e) IA/B-C50-20. (f) IA/B-C50-22. (g) IA/B-C60-18. (h) IA/B-C60-20. (i) IA/B-C60-22. (j) EA/B-C40-18/22. (k) EA/B-C40-20. (l) EA/B-C50-18/22. (m) EA/B-C50-20. (n) EA/B-C60-18/22. (o) EA/B-C60-20.
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
(k)
(l)
(m)
(n)
(o)From the start of the test until Point A, the specimens did not crack and their deformations were linearly elastic. At Point A, first major cracks appeared at the section adjacent to the beam-column connection (Figure7(b)). With the increase in the load, more cracks gradually developed in the span (Figure 7(a)) and the beams behaved quite linearly in the deflection curves before Point B. After Point B, the deformation increased relatively quickly with the increase in the load. The number of cracks no longer increased; however, the width of cracks increased. It should be noted that the distances among the cracks are important for strain penetration in the shear span, which has been comprehensively studied by Megaloopikonomou et al. [2]. The region, ranging from the crack section toward the uncrack part of the shear span until the rebar strain coordinates with the deformation of the surrounding concrete cover, was defined as the “disturbed” region. In view of whether the next crack is formed in the “disturbed” region of the previous crack, different methods for evaluating the strain and slip of the reinforcement along the shear span have been proposed in the literature [2]. At Point C, a slight concrete compressive failure was observed at the critical cross section. Subsequently, more horizontal compressive cracks gradually developed at the compressive zone near the critical section (Figure 7(c)). However, the load was largely constant with the rapid increase in the deflection. It can be explained that the confined stirrups of the beams (the range of stirrup volumetric ratios is 1.2%∼1.9%) would improve the ultimate compressive strength and ultimate strain of the confined compression concrete to some extent, thereby improving the ductilities of the test beam. Until the peak Point D, the concrete was obviously crushed (Figure 7(d)) and the curves entered the descending stage that the load decreased with the increase in the deflection. As shown in Figure 6, the deflections of the east span beam and west span beam for the one specimen were largely symmetrical owing to their equal longitudinal steel ratios. For each comparison group with the same concrete grade and the same ratios of the tensile reinforcement, a very similar behaviour was observed before the yielding state (Point B). After Point B, the beams with a higher grade of reinforcement developed a higher flexural capacity. Tables 4 and 5 list the loads corresponding to the characteristic point of the specimens.Figure 7
Photographs from the experimental study. (a) Crack distribution in the shear span. (b) First crack at the section adjacent to the beam-column connection. (c) Horizontal compressive cracks developed at the compressive zone. (d) Compressive concrete was obviously crushed.
(a)
(b)
(c)
(d)Table 4
Load of the interior beam-column connection at characteristic points.
Specimen No.
Crack load (kN)
Yield load (kN)
Nominal ultimate load (kN)
Peak load (kN)
E
W
E
W
E
W
E
W
IA-400-C40-18
19.5
24
107
102
127
127
129
129
IA-400-C50-18
25.5
25.5
115
100
135
135
135
135
IA-400-C60-18
24
21
113
117
127
129
129
130
IA-600-C40-20
15
15
109
113
121
121
127
125
IA-600-C50-20
25.5
32
177
182
192
192
202
192
IA-600-C60-20
24
27
160
160
180
180
175
177
IA-800-C40-22
21
21
116
122
140
137
145
146
IA-800-C50-22
21
21
127
122
142
142
147
150
IA-800-C60-22
21
19.5
170
170
211
208
221
213
IB-400-C40-18
18
18
122
122
152
152
157
156
IB-400-C50-18
21
21
130
140
150
150
156
159
IB-400-C60-18
19.5
19.5
130
130
155
155
162
160
IB-600-C40-20
18
18
115
115
139
135
140
140
IB-600-C50-20
18
18
114
104
134
134
142
134
IB-600-C60-20
24
24
170
160
205
200
220
208
IB-800-C40-22
16.5
15
137
142
157
157
167
168
IB-800-C50-22
18
18
142
142
175
167
184
174
IB-800-C60-22
22.5
22.5
130
120
165
165
175
165
E represents the east span of the interior beam-column connection, andW represents the west span of the interior beam-column connection.Table 5
Load of the exterior beam-column connection at characteristic points.
Specimen No.
Crack load (kN)
Yield load (kN)
Nominal ultimate load (kN)
Peak load (kN)
EA-430-C40-18
22.5
122.0
137.0
140.0
EA-380-C50-18
18.0
124.0
140.0
146.0
EA-420-C50-20
21.0
160.0
180.0
188.0
EA-350-C60-18
21.0
91.0
136.0
158.0
EA-330-C40-20
18.0
102.0
114.0
122.8
EA-300-C50-20
18.0
140.0
180.0
190.0
EA-270-C60-20
24.0
125.0
170.0
171.7
EA-300-C60-22
16.5
86.0
121.0
135.0
EA-190-C40-20
18.0
99.0
114.0
126.1
EA-210-C40-22
18.0
122.0
137.0
137.0
EA-190-C50-22
18.0
124.0
140.0
154.1
EA-160-C60-20
16.5
145.0
170.0
174.7
EB-420-C40-18
27.0
150.0
170.0
176.8
EB-420-C50-18
19.5
125.0
150.0
186.0
EB-420-C50-20
18.0
116.0
131.0
146.0
EB-400-C60-18
22.5
150.0
170.0
175.0
EB-380-C40-20
21.0
105.0
140.0
145.0
EB-340-C50-20
18.0
126.0
146.0
157.5
EB-310-C60-20
21.0
180.0
215.0
215.0
EB-340-C60-22
22.5
130.0
155.0
164.0
EB-220-C40-20
21.0
130.0
145.0
149.4
EB-230-C40-22
16.5
130.0
150.0
170.0
EB-210-C50-22
16.5
140.0
175.0
189.0
EB-180-C60-20
21.0
165.0
190.0
215.0


## 3.2. Rebar Strain Distribution along the Embedment Length

Figures8 and 9 show the strain distribution (at the yielding and nominal ultimate limit states) of the straight embedment reinforcement in the interior beam-column connection and exterior beam-column connection, respectively. In Figure 8, the origin of the abscissa represents the midpoint of the continuous reinforcement through the interior beam-column connection, and the one in Figure 9 represents the free end near the headed part of the anchorage reinforcement in the exterior connection (consistent with Figure 4). The figures demonstrate the occurrence of strain penetration in the beam-column connection that the rebar strain gradually decreases from the critical section to the coordinate origin and consequently slippage at the beam-column interface. Moreover, for the same grade of reinforcement, the rebar strain at the coordinate origin decreases with the increase in the straight embedment length. A longer embedment length results in lower bond stresses near the coordinate origin; however, the accumulation of the bonding stresses along the embedment length increases, denoting a lower strain of reinforcement at the coordinate origin. At the nominal ultimate limit state, the rebar strains are concentrated near the beam-column interface, and they were observed to decrease sharply to the yield strain point and then decrease slowly until the coordinate origin.Figure 8
Strain distribution along the tensile reinforcement throughout the interior beam-column connection. Specimen type: (a) IA-C40; (b) IA-C50; (c) IA-C60; (d) IB-C40; (e) IB-C50; (f) IB-C60.
(a)
(b)
(c)
(d)
(e)
(f)Figure 9
Strain distribution along the tensile reinforcement anchored in the exterior beam-column connection. Specimen type: (a) EA-C40; (b) EA-C50; (c) EA-C60; (d) EB-C40; (e) EB-C50; (f) EB-C60.
(a)
(b)
(c)
(d)
(e)
(f)


## 3.3. Additional Fixed-End Rotation due to Strain Penetration

Figures10(a) and 10(b) illustrate the additional fixed-end rotation θslip at the beam-column interface due to the strain penetration of the tensile reinforcement inside the interior and exterior beam-column connections. θslip is equal to the slippage of the embedment reinforcement s divided by the depth of the tensile zone (d−xc) as follows:(1)θslip=sd−xc,where d is the effective depth of the section and xc is the depth of the neutral axis.Figure 10
Strain penetration of the longitudinal tensile reinforcement inside (a) interior beam-column connection and (b) exterior beam-column connection.
(a)
(b)As shown in Figure10(a), the local slip at the midpoint of the straight embedment reinforcement through the interior beam-column connection is zero when symmetrical loads are applied to the beam end. The embedment reinforcement can be considered to sustain the reverse symmetrical tensile force from the midpoint. If the concrete deformation is ignored, the slippage of the reinforcement s can be calculated by integrating the strain along half of the embedment length:(2)s=∫0lahεsxdx,where lah is half of the embedment length of the continuous reinforcement through the interior beam-column connection and εs is the rebar strain.As shown in Figure10(b), when hooked bars are used as longitudinal reinforcements in the exterior beam-column connection, a hook displacement occurs if the straight embedment length of the reinforcement is not sufficient. Hence, the slippage of the reinforcement s is the sum of the integral of the strain along the straight embedment length and the hook displacement as expressed in the following equation:(3)s=∫0lahεsxdx+δh,where lah is the straight lead length of the hooked bar and δh is the hook displacement.A model for the relationship between force resisted by the hook and hook displacement was proposed by Soroushian et al. [22] based on the experiments for the tensile behaviour of hook bars as shown in the following expressions:(4)Ph=Phuδh2.54,(5)Phu=2710.05db−0.25,(6)Phf=0.54Phu.The model shown in Figure11 is adopted here for predicting the hook displacement δh. The force resisted by the hook Ph can be calculated from the experimental results of the rebar strain at the free end of anchorage reinforcement combined with the stress-strain relationship of the reinforcement. Then, the hook displacement δh can be obtained using equations (4)–(6). Figure 12 shows the relationship between the relative straight embedment length lah/db and the ratio of the hook displacement δh to slippage s at the yielding and nominal ultimate limit states for each exterior beam-column connection. It can be seen that δh/s decreases with the increase in lah/db. The fitting curve shows that the ratio δh/s does not exceed 0.1 when lah is greater than 12db, which indicates that the effect of the hook displacement δh on s is negligible. The straight embedment length of the hooked bar or headed bar lah has been specified in most design specifications, as listed in Table 6. It can be known that the condition lah<12db rarely occurs in practice, thus the influence of δh is not considered in this paper. Similar to the hooked bars, when the headed bars are used as longitudinal reinforcements, the slip at the headed end of the bars is negligible.Figure 11
Hook force-hook deformation relationship.Figure 12
Relationship betweenlah/db and δh/s: (a) at the yielding state; (b) at the nominal ultimate state.
(a)
(b)Table 6
Design specifications for straight anchorage length of hooked or headed bar.
Code
Straight anchorage length of hooked or headed bar,lah
Commentary
ACI 318-14 [21]
l
ah
≥
0.02
ψ
e
f
y
/
λ
f
c
′
d
b
for hooked bar
l
ah
≥
0.016
ψ
e
f
y
/
λ
f
c
′
d
b
for headed bar
ψ
e = 1.2 for epoxy-coated reinforcement; ψe = 1.0 for other cases; λ = 0.75 for lightweight concrete; λ = 1.0 for other cases.
Chinese code (GB 50010-2010) [20]
l
ah
≥
0.4
l
ab
l
ab
=
α
f
y
/
f
t
d
b
f
y is the design value of the reinforcement tensile strength;ft is the design value of the concrete tensile strength;α = 0.14 for deformed bar; α = 0.16 for plain bar.
Eurocode 2-part 1-1 [23]
l
ah
≥
α
1
l
b,rqd
l
b,rqd
=
d
b
σ
sd
/
4
f
bd
f
bd
=
2.25
η
1
η
2
f
t
α
1 = 0.7 if cd > 3db; otherwise α1 = 1.0; σsd is the design stress of the bar at the position from where the anchorage is measured;η1 = 1.0 when “good” conditions are obtained;η1 = 0.7 for other cases; η2 = 1.0 for db ≤ 32 mm; η2 = (132−db)/100 for db > 32 mm.Based on the tensile strain distribution of the embedment reinforcement obtained from the test, the additional fixed-end rotation of the exterior and interior beam-column connections at the yielding and nominal ultimate limit states can be calculated by combining equations (1)–(3). The results are listed in Tables 7 and 8.Table 7
Additional fixed-end rotation of interior beam-column connection at yielding and nominal ultimate limit states.
Specimen no.
s
y (mm)
θ
y,slip (×10−3 rad)
s
u (mm)
θ
u,slip (×10−3 rad)
E
W
E
W
E
W
E
W
IA-400-C40-18
0.50
0.50
2.41
2.40
0.82
0.82
3.44
3.43
IA-400-C50-18
0.46
0.48
2.15
2.25
0.78
0.83
3.11
3.29
IA-400-C60-18
0.48
0.47
2.13
2.09
1.08
1.06
4.03
3.96
IA-600-C40-20
0.58
0.56
2.74
2.66
1.23
1.18
4.81
4.64
IA-600-C50-20
0.55
0.54
2.66
2.63
0.82
0.89
3.46
3.77
IA-600-C60-20
0.52
0.51
2.42
2.39
1.02
1.09
3.99
4.25
IA-800-C40-22
0.65
0.62
3.05
2.88
1.23
1.26
4.84
4.95
IA-800-C50-22
0.58
0.63
2.73
2.95
1.17
1.16
4.53
4.49
IA-800-C60-22
0.55
0.56
2.68
2.73
1.01
1.01
4.11
4.10
IB-400-C40-18
0.55
0.56
2.72
2.76
0.81
0.82
3.44
3.48
IB-400-C50-18
0.54
0.54
2.49
2.52
0.96
0.98
3.91
3.98
IB-400-C60-18
0.53
0.53
2.36
2.38
0.94
0.93
3.55
3.52
IB-600-C40-20
0.67
0.67
3.12
3.11
1.10
1.13
4.46
4.58
IB-600-C50-20
0.65
0.63
2.92
2.83
1.23
1.19
4.76
4.63
IB-600-C60-20
0.62
0.63
2.88
2.90
1.19
1.11
4.82
4.50
IB-800-C40-22
0.75
0.78
3.55
3.69
1.18
1.16
4.83
4.75
IB-800-C50-22
0.76
0.76
3.61
3.61
1.26
1.17
5.04
4.70
IB-800-C60-22
0.69
0.71
3.05
3.13
1.42
1.42
5.40
5.39Table 8
Additional fixed-end rotation of exterior beam-column connection at yielding and nominal ultimate states.
Specimen no.
s
y (mm)
θ
y,slip (×10−3 rad)
s
u (mm)
θ
u,slip (×10−3 rad)
EA-430-C40-18
0.70
3.37
1.16
4.83
EA-380-C50-18
0.68
3.28
1.23
4.94
EA-420-C50-20
0.78
3.90
1.26
5.43
EA-350-C60-18
0.67
2.98
1.23
4.68
EA-330-C40-20
0.69
3.24
1.27
4.95
EA-300-C50-20
0.67
3.36
1.09
4.70
EA-270-C60-20
0.58
2.72
1.03
4.11
EA-300-C60-22
0.62
2.77
1.09
4.09
EA-190-C40-20
0.46
2.14
0.88
3.45
EA-210-C40-22
0.43
2.10
0.80
3.22
EA-190-C50-22
0.43
2.00
0.95
3.74
EA-160-C60-20
0.43
2.00
0.77
3.08
EB-420-C40-18
0.80
3.84
1.25
5.28
EB-420-C50-18
0.77
3.60
1.25
5.10
EB-420-C50-20
0.80
3.80
1.28
5.00
EB-400-C60-18
0.71
3.17
1.26
4.81
EB-380-C40-20
0.82
3.92
1.40
5.91
EB-340-C50-20
0.70
3.15
1.20
4.67
EB-310-C60-20
0.67
3.11
1.22
4.95
EB-340-C60-22
0.75
3.34
1.26
4.78
EB-220-C40-20
0.59
2.81
1.09
4.61
EB-230-C40-22
0.58
2.86
0.96
4.03
EB-210-C50-22
0.54
2.55
0.97
3.89
EB-180-C60-20
0.50
2.30
0.80
3.24


## 4. Parametric Study

A systematic parametric study on the additional fixed-end rotation at the yielding and nominal ultimate states was conducted based on the experimental results. The parameters that potentially affect the bond between concrete and reinforcement are explored, including the yield strength of the steel barfy, concrete tensile strength fct, diameter db, and straight embedment length lah of the reinforcement in the beam-column connection. Moreover, the depth of the neutral axis is taken into consideration, as it considerably affects the depth of the tensile zone and slippage of the embedment reinforcement at the critical section. When one parameter is studied, the other parameters are kept constant. Despite a certain fluctuation in the test results, the clear trends of the influence of each parameter are obtained.


### 4.1. Effect of Reinforcement Diameter

The diameter of the reinforcementdb is the main factor that affects the additional fixed-end rotation due to the strain penetration. As shown in Figure 13, consider the case where a reinforcing bar with a diameter db is anchored in concrete and a tensile force is applied at the loading end. The equilibrium equation for the bar with sufficient length is as follows:(7)Ft=∫0Ldπdb⋅τsxdx.Figure 13
Equilibrium of the anchorage reinforcement with development lengthLd.The rebar strain decreases along the development length because of the bond force between the concrete and reinforcement. For a constant tensile force, an increase indb leads to an increase in the bond surface area. Consequently, the bond force between the concrete and reinforcement decreases. Therefore, a slower reduction in the reinforcement stress occurs along the anchorage length. This implies that an increase in db increases the extent of yield penetration and is advantageous for increasing the additional fixed-end rotation. Generally, the effect of strain penetration is indirectly reflected in the strain penetration length. Tastani and Pasntazopoulou [13] established an analytical expression for the strain penetration length lsp, in which the influential factors of strain permeation length were considered comprehensively as follows:(8)lsp=εs0−εsy⋅dbEsh4fbres,where εs0 is the rebar strain at the critical section; εsy and Esh are the yielding strain and hardening modulus of the steel reinforcement; and fbres is the residual bond strength between the concrete and reinforcement. From equation (8), it can be known the effect of db on the strain penetration shows a linear relationship. There are also several empirical expressions of the strain penetration length, which have the same variation trend about the diameter, as listed in Table 9. In this paper, the variation in the additional fixed-end rotation with respect to db is considered to be consistent with previous studies.Table 9
Empirical expressions of strain penetration lengthLsp.
Reference
Strain penetration length,Lsp
Paulay and Priestley [19]
L
sp = 0.022fydb
Priestley and Park [24]
L
sp = 6db
Panagiotakos and Fardis [25]
L
sp = 0.021fydb
Eurocode 8-part 3 [26]
L
sp
=
0.24
f
y
/
f
c
′
d
b
L
sp
=
0.11
f
y
/
f
c
′
d
b


### 4.2. Effect of the Neutral Axis Depth

The effect of neutral axis depthxc on the additional fixed-end rotation should be considered in that it is related to both depth of the tensile zone and slippage of reinforcement at the critical section. To facilitate the application of design, the ratio ξ = λxc,u/d is investigated in this paper, where xc,u is the depth of the neutral axis when the strain in the extreme compressed fibre of the critical section reaches the ultimate strain, d is the effective depth of the section, and λ is a factor specified in the design code [23].The depth of the neutral axisxc can be calculated based on the two conditions of static equilibrium and strain compatibility of the critical section. Figure 14 presents the critical cross section reinforced with tensile and compressive steel bars, which is divided into a number of layers. According to the assumption that the strain in each layer is linearly proportional to its distance from the neural axis (Figure 14(b)) [21], as expressed in equation (9), the stresses in each layer can be obtained from the stress-strain relationships of the concrete and reinforcement. Then, the equilibrium between the compressive and tensile forces acting on the cross section shown in Figure 14(c) can be expressed by equation (10):(9)εi=xc−xid−xcεs,(10)∫0db⋅fcεidx+Es′εs′As′=EsεsAs,where b is the width of the section, fc(x) is the function of the concrete stress-strain relationship, Es and Es′ are the tensile and compressive modulus of the reinforcement, respectively.Figure 14
Force equilibrium of the reinforced concrete section. (a) Critical cross section. (b) Strain distribution. (c) Stress distribution.Combining the test results of the rebar strains with equations (9)–(10), the depth of the neutral axes xc,y and xc,u can be calculated, and the relationships between ξ and depth of the tensile zones xt,y and xt,u can be obtained as shown in Figure 15. The expressions of the fitting curves are as follows:(11)xt,y=d−xc,y=0.8d1−0.95ξ,(12)xt,u=d−xc,u=d1−1.25ξ.Figure 15
Relationship betweenξ and xt at (a) yielding and (b) nominal ultimate states.
(a)
(b)It is simple to understand thatxt clearly decreases with the increase in ξ. The key problem here is to investigate the effect of ξ on the slippage of the reinforcement. To eliminate the effects of the rebar diameters, the yield strength of reinforcement, and the concrete tensile strength on the slippage of different test specimens, the coefficient δ1=dbfy/fct was introduced. Three comparison groups were chosen from the test results, in which the relative embedment length lah/db in the beam-column connections was similar. For the yielding state, the relationship between sy/δ1 and ξ is shown in Figure 16(a). It can be seen that sy/δ1 is largely constant in each comparison group for ξ varying from 0.11 to 0.21, which means that the influence of ξ on sy is almost negligible. Combining equations (1) and (11), we see that an increase in ξ can increase θy,slip. For the nominal ultimate limit state, a reduction tendency of the power function su/δ1 is observed with the increase in ξ, as shown in Figure 16(b). The slippage is obtained by integrating the strain that gradually decreases along the embedment length, and the strain at the critical section εsu is the maximum. Under the same bond condition, εsu can be regarded to be positively related to slippage. Meanwhile, based on the equilibrium equation for the cross section, εsu decreases with an increase in ξ. Thus, an increase in ξ leads to a reduction in su. The curve of the power function, shown in Figure 16(b), was fitted as the coefficient δ2 to consider the influence of ξ on su as follows:(13)δ2=ξ−0.68.Figure 16
Effect ofξ on (a) sy/δ1 and (b) su/δ1.
(a)
(b)By combining equations (12) and (13), we find that the increase in ξ has a more significant influence on the decrease in su than the decrease in the depth of the tensile zone. As shown in Figure 17, θu,slip decreases with the increase in ξ.Figure 17
Effect ofξ on θu,slip/δ1.


### 4.3. Effect of Yield Strength of Reinforcement

Figure18 shows the variation in the slippage s with respect to the yield strength fy at the yielding and nominal ultimate states. The design parameters for each comparison group are the same except for fy, as shown in the legend. As fy increases from 540 MPa to 654 MPa, an increasing trend of sy and su/δ2 is observed. According to statistics, sy and su increase by an average of 17.4% and 12.2%, respectively. The increase in fy accelerates the bond failure between the reinforcement and the concrete at the yielding and nominal ultimate states and in turn improves the ability of the strain penetration, thus leading to an increase in additional fixed-end rotation. A comparison between Figures 18(a) and 18(b) shows that the slopes of the trendlines in Figure 18(a) are greater than those in Figure 18(b). This implies that the growth rate of sy is faster than that of su with the increase in fy. As a result, the influence of the strain penetration on the additional fixed-end rotation at the early stages before the yielding should be given special attention when high-strength steel bars are used as the tensile reinforcement in beam-column connections.Figure 18
Effect offy on (a) sy and (b) su/δ2.
(a)
(b)


### 4.4. Effect of Concrete Tensile Strength

The following are the three components of the bond forces between reinforcement and concrete: adhesion on the reinforcement surface, friction due to concrete shrinkage, and mechanical interlocking between lugs and concrete. The increase in the tensile strength of the concreteft improves the adhesion and mechanical interlocking forces and delays the cracking of the tensile concrete around the reinforcement. Experimental studies have shown that the ultimate bond strength between deformed steel bars and concrete increases is in proportion with the concrete tensile strength ft [27]. Consequently, an increase in ft will result in a faster decline in the rebar strain along the embedment length and subsequently decrease the slippage at the beam-column interface. From the experimental results presented in this paper, the variations in slippage sy and su with the concrete tensile strength ft are shown in Figure 19, where a slightly decreased trend is observed. Because of the discrete characteristics and the relatively close grade of the concrete, a certain fluctuation existed in the results and the extent of decrease was not significant.Figure 19
Effect offct on (a) sy and (b) su/δ2.
(a)
(b)


### 4.5. Effect of Straight Embedment Length of Reinforcement

The straight embedment length of the reinforcement in beam-column connection is another factor that is believed to effect the additional fixed-end rotation. A related study conducted by Sezen and Setzler [12] concluded that the steel bars with various embedment lengths would behave similarly in a certain length range and the minimum embedment length was later determined. As mentioned in Section 3.3, 12db is considered the lower limit of the embedment length in this paper. From the test results, the effect of the relative straight embedment length lah/db on the slippage s is obtained, as shown in Figure 20. When the values of the other parameters are fixed, sy and su tend to increase as a power function as lah/db varies from 8 to 24. The reason for the same is given in Figure 20.Figure 20
Effect oflah/db on (a) sy and (b) su/δ2.
(a)
(b)As shown in Figure13, the rebar strain decreases from maximum at the beam-column interface to zero at the unloaded end along the development length Ld. However, the embedded length in practical design is usually no greater than Ld. In these cases, the unloaded end is stressed. Certain values of the strain at the end of the bars (the middle point of the continuous steel bars embedded in the interior beam-column connection sustained by the symmetrical load and the free-end point of the steel bars anchored in the exterior beam-column connection) are obtained, as shown in Figures 8 and 9. Although the reinforcement strain attenuates along the embedment length, the contribution of the rebar strain near the unloaded end to the slippage cannot be ignored. Based on equations (2) and (3), an increase in lah/db enlarges the upper limit of the strain integration and consequently increases the slippage of reinforcement. However, when it exceeds the development length, the redundant embedment length is invalid. In summary, increasing lah/db within a certain range is beneficial to the additional fixed-end rotation.


## 4.1. Effect of Reinforcement Diameter

The diameter of the reinforcementdb is the main factor that affects the additional fixed-end rotation due to the strain penetration. As shown in Figure 13, consider the case where a reinforcing bar with a diameter db is anchored in concrete and a tensile force is applied at the loading end. The equilibrium equation for the bar with sufficient length is as follows:(7)Ft=∫0Ldπdb⋅τsxdx.Figure 13
Equilibrium of the anchorage reinforcement with development lengthLd.The rebar strain decreases along the development length because of the bond force between the concrete and reinforcement. For a constant tensile force, an increase indb leads to an increase in the bond surface area. Consequently, the bond force between the concrete and reinforcement decreases. Therefore, a slower reduction in the reinforcement stress occurs along the anchorage length. This implies that an increase in db increases the extent of yield penetration and is advantageous for increasing the additional fixed-end rotation. Generally, the effect of strain penetration is indirectly reflected in the strain penetration length. Tastani and Pasntazopoulou [13] established an analytical expression for the strain penetration length lsp, in which the influential factors of strain permeation length were considered comprehensively as follows:(8)lsp=εs0−εsy⋅dbEsh4fbres,where εs0 is the rebar strain at the critical section; εsy and Esh are the yielding strain and hardening modulus of the steel reinforcement; and fbres is the residual bond strength between the concrete and reinforcement. From equation (8), it can be known the effect of db on the strain penetration shows a linear relationship. There are also several empirical expressions of the strain penetration length, which have the same variation trend about the diameter, as listed in Table 9. In this paper, the variation in the additional fixed-end rotation with respect to db is considered to be consistent with previous studies.Table 9
Empirical expressions of strain penetration lengthLsp.
Reference
Strain penetration length,Lsp
Paulay and Priestley [19]
L
sp = 0.022fydb
Priestley and Park [24]
L
sp = 6db
Panagiotakos and Fardis [25]
L
sp = 0.021fydb
Eurocode 8-part 3 [26]
L
sp
=
0.24
f
y
/
f
c
′
d
b
L
sp
=
0.11
f
y
/
f
c
′
d
b


## 4.2. Effect of the Neutral Axis Depth

The effect of neutral axis depthxc on the additional fixed-end rotation should be considered in that it is related to both depth of the tensile zone and slippage of reinforcement at the critical section. To facilitate the application of design, the ratio ξ = λxc,u/d is investigated in this paper, where xc,u is the depth of the neutral axis when the strain in the extreme compressed fibre of the critical section reaches the ultimate strain, d is the effective depth of the section, and λ is a factor specified in the design code [23].The depth of the neutral axisxc can be calculated based on the two conditions of static equilibrium and strain compatibility of the critical section. Figure 14 presents the critical cross section reinforced with tensile and compressive steel bars, which is divided into a number of layers. According to the assumption that the strain in each layer is linearly proportional to its distance from the neural axis (Figure 14(b)) [21], as expressed in equation (9), the stresses in each layer can be obtained from the stress-strain relationships of the concrete and reinforcement. Then, the equilibrium between the compressive and tensile forces acting on the cross section shown in Figure 14(c) can be expressed by equation (10):(9)εi=xc−xid−xcεs,(10)∫0db⋅fcεidx+Es′εs′As′=EsεsAs,where b is the width of the section, fc(x) is the function of the concrete stress-strain relationship, Es and Es′ are the tensile and compressive modulus of the reinforcement, respectively.Figure 14
Force equilibrium of the reinforced concrete section. (a) Critical cross section. (b) Strain distribution. (c) Stress distribution.Combining the test results of the rebar strains with equations (9)–(10), the depth of the neutral axes xc,y and xc,u can be calculated, and the relationships between ξ and depth of the tensile zones xt,y and xt,u can be obtained as shown in Figure 15. The expressions of the fitting curves are as follows:(11)xt,y=d−xc,y=0.8d1−0.95ξ,(12)xt,u=d−xc,u=d1−1.25ξ.Figure 15
Relationship betweenξ and xt at (a) yielding and (b) nominal ultimate states.
(a)
(b)It is simple to understand thatxt clearly decreases with the increase in ξ. The key problem here is to investigate the effect of ξ on the slippage of the reinforcement. To eliminate the effects of the rebar diameters, the yield strength of reinforcement, and the concrete tensile strength on the slippage of different test specimens, the coefficient δ1=dbfy/fct was introduced. Three comparison groups were chosen from the test results, in which the relative embedment length lah/db in the beam-column connections was similar. For the yielding state, the relationship between sy/δ1 and ξ is shown in Figure 16(a). It can be seen that sy/δ1 is largely constant in each comparison group for ξ varying from 0.11 to 0.21, which means that the influence of ξ on sy is almost negligible. Combining equations (1) and (11), we see that an increase in ξ can increase θy,slip. For the nominal ultimate limit state, a reduction tendency of the power function su/δ1 is observed with the increase in ξ, as shown in Figure 16(b). The slippage is obtained by integrating the strain that gradually decreases along the embedment length, and the strain at the critical section εsu is the maximum. Under the same bond condition, εsu can be regarded to be positively related to slippage. Meanwhile, based on the equilibrium equation for the cross section, εsu decreases with an increase in ξ. Thus, an increase in ξ leads to a reduction in su. The curve of the power function, shown in Figure 16(b), was fitted as the coefficient δ2 to consider the influence of ξ on su as follows:(13)δ2=ξ−0.68.Figure 16
Effect ofξ on (a) sy/δ1 and (b) su/δ1.
(a)
(b)By combining equations (12) and (13), we find that the increase in ξ has a more significant influence on the decrease in su than the decrease in the depth of the tensile zone. As shown in Figure 17, θu,slip decreases with the increase in ξ.Figure 17
Effect ofξ on θu,slip/δ1.


## 4.3. Effect of Yield Strength of Reinforcement

Figure18 shows the variation in the slippage s with respect to the yield strength fy at the yielding and nominal ultimate states. The design parameters for each comparison group are the same except for fy, as shown in the legend. As fy increases from 540 MPa to 654 MPa, an increasing trend of sy and su/δ2 is observed. According to statistics, sy and su increase by an average of 17.4% and 12.2%, respectively. The increase in fy accelerates the bond failure between the reinforcement and the concrete at the yielding and nominal ultimate states and in turn improves the ability of the strain penetration, thus leading to an increase in additional fixed-end rotation. A comparison between Figures 18(a) and 18(b) shows that the slopes of the trendlines in Figure 18(a) are greater than those in Figure 18(b). This implies that the growth rate of sy is faster than that of su with the increase in fy. As a result, the influence of the strain penetration on the additional fixed-end rotation at the early stages before the yielding should be given special attention when high-strength steel bars are used as the tensile reinforcement in beam-column connections.Figure 18
Effect offy on (a) sy and (b) su/δ2.
(a)
(b)


## 4.4. Effect of Concrete Tensile Strength

The following are the three components of the bond forces between reinforcement and concrete: adhesion on the reinforcement surface, friction due to concrete shrinkage, and mechanical interlocking between lugs and concrete. The increase in the tensile strength of the concreteft improves the adhesion and mechanical interlocking forces and delays the cracking of the tensile concrete around the reinforcement. Experimental studies have shown that the ultimate bond strength between deformed steel bars and concrete increases is in proportion with the concrete tensile strength ft [27]. Consequently, an increase in ft will result in a faster decline in the rebar strain along the embedment length and subsequently decrease the slippage at the beam-column interface. From the experimental results presented in this paper, the variations in slippage sy and su with the concrete tensile strength ft are shown in Figure 19, where a slightly decreased trend is observed. Because of the discrete characteristics and the relatively close grade of the concrete, a certain fluctuation existed in the results and the extent of decrease was not significant.Figure 19
Effect offct on (a) sy and (b) su/δ2.
(a)
(b)


## 4.5. Effect of Straight Embedment Length of Reinforcement

The straight embedment length of the reinforcement in beam-column connection is another factor that is believed to effect the additional fixed-end rotation. A related study conducted by Sezen and Setzler [12] concluded that the steel bars with various embedment lengths would behave similarly in a certain length range and the minimum embedment length was later determined. As mentioned in Section 3.3, 12db is considered the lower limit of the embedment length in this paper. From the test results, the effect of the relative straight embedment length lah/db on the slippage s is obtained, as shown in Figure 20. When the values of the other parameters are fixed, sy and su tend to increase as a power function as lah/db varies from 8 to 24. The reason for the same is given in Figure 20.Figure 20
Effect oflah/db on (a) sy and (b) su/δ2.
(a)
(b)As shown in Figure13, the rebar strain decreases from maximum at the beam-column interface to zero at the unloaded end along the development length Ld. However, the embedded length in practical design is usually no greater than Ld. In these cases, the unloaded end is stressed. Certain values of the strain at the end of the bars (the middle point of the continuous steel bars embedded in the interior beam-column connection sustained by the symmetrical load and the free-end point of the steel bars anchored in the exterior beam-column connection) are obtained, as shown in Figures 8 and 9. Although the reinforcement strain attenuates along the embedment length, the contribution of the rebar strain near the unloaded end to the slippage cannot be ignored. Based on equations (2) and (3), an increase in lah/db enlarges the upper limit of the strain integration and consequently increases the slippage of reinforcement. However, when it exceeds the development length, the redundant embedment length is invalid. In summary, increasing lah/db within a certain range is beneficial to the additional fixed-end rotation.


## 5. Proposed Model of Additional Fixed-Rotation at Yielding and Nominal Ultimate States

Based on the development trend of the parameters analysed in the parametric study above, a three-dimensional coordinate system is established withdbfy/ft, lah/db as the horizontal axis, and s as the vertical axis. The test data points are incorporated in the coordinate system, as shown in Figure 21. The fitting surfaces in terms of the slippage s at the yielding and nominal ultimate states are obtained from the multivariable regression analysis considering all the main parameters. The expressions of the fitting surfaces are as follows, wherein 12db ≤ lah ≤ 24db is based on the experimental results:(14)sy=4.770×10−5dbfyfctlahdb0.5117,(15)su=3.191×10−5ξ0.68dbfyfctlahdb0.4195.Figure 21
Fitting curves of (a)sy and (b) su.
(a)
(b)Then, the additional fixed-rotationsθy,slip and θu,slip can be determined with equations (11)–(15):(16)θy,slip=syd−xc,y=4.770×10−5dbfy/fctlah/db0.51170.8d1−0.95ξ,(17)θu,slip=sud−xc,u=3.191×10−5dbfy/fctlah/db0.4195ξ0.68d1−1.25ξ.The parameters considered in the proposed models are widely used in engineering design, thus making the expression more simple and practical. To investigate the applicability of the proposed model, the test results of the ten specimens [3, 28, 29] are provided for comparison. The properties of these specimens are summarized in Table 10. As most of the tests were pullout tests and were terminated soon after the reinforcement yielded at the loaded end, only the slippage of the reinforcement at the yielding state was compared. Figure 22 compares the predictions of sy and su with the experimental results. The proposed model exhibits reasonable accuracy.Table 10
Results of slippagesy in the literatures.
No.
f
y (MPa)
f
ct (MPa)
d
b (mm)
l
ah (mm)
s
y (mm)
Reference
1
350.3
2.29
19.1
762
0.5
Shima et al. [28]
2
610.2
2.29
19.1
762
0.9
3
819.8
2.29
19.1
762
1.6
4
708.8
2.69
12.7
355.6
0.8
Mathey and Wastein [29]
5
537.8
2.77
25.4
711.2
1.0
6
414.3
2.31
32.3
610
1.2
Ueda et al. [3]
7
331.6
2.20
32.3
610
0.9
8
414.3
2.36
32.3
375
1.1
9
468.8
2.48
25.4
457
0.9
10
438.5
2.84
19.1
610
0.6Figure 22
Comparison between calculation and experiment results of (a)sy and (b) su.
(a)
(b)


## 6. Conclusion

An accurate and simple determination of the additional fixed-end rotation at the beam-column interface due to the strain penetration can provide evidence for investigating the rotation of the plastic hinges. A series of reinforced concrete beam-column connections with variable design parameters were constructed and tested by applying a monotonic load at the beam end. A parametric study was carried out to study the effects of the yield strength of the reinforcementfy, tensile strength of the concrete fct, diameter db, and embedment length lah of the reinforcement in the beam-column connection on the additional fixed-end rotation. From the experiment results, the following conclusions can be drawn:(1)
The rebar strain distribution along the embedment length in the beam-column connection demonstrated the occurrence of strain penetration in the beam-column connection. A clear strain concentration could be observed near the beam-column interface at the nominal ultimate state. For different specimens with variable parameters under monotonic loading, the additional fixed-end rotation at the ultimate state was approximately 1.26–1.89 times greater than that at the yielding state.(2)
The additional fixed-end rotation increased with the increase infy and with the decrease in fct. As fy increased from 540 MPa to 654 MPa, sy and su increased by averages of 17.4% and 12.2%, respectively. It indicated that when high-strength steel bars were used as the tensile reinforcement in beam-column connections, the effect of strain penetration on fixed-end rotation was more obvious before the yielding state.(3)
Aslah/db varied from 12 to 24, sy and su tended to increase as a power function. Increasing lah/db within a certain range was found to be beneficial to the additional fixed-end rotation.(4)
The depth of the neutral axis had almost no effect onsy; however, a power function reduction tendency of su was observed with the increase in the depth of the neutral axis. Along with the variation in the tensile zone depth, it was found from overall consideration that the increase in the depth of the neutral axis led to an increase in θy,slip but slightly decreased θu,slip.(5)
A simple calculation model of the additional fixed-end rotation was proposed for interior and exterior beam-column connections under monotonic loading at the yielding and nominal ultimate states. Parameters widely used in engineering design were considered in the model. The comparison between the prediction and experimental results showed good agreement.



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