# Behavior of RBS Beams Reinforced by Stiffeners Subjected to Cyclic Loading

Authors: Iori Kanao; Tianrui He; Zheng Yu; Kiyotaka Morisako
Journal: Journal of Engineering
 (2018)

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## Abstract

This paper presents a numerical study of reduced beam section (RBS) beams with vertical and horizontal stiffeners. For RBS beams, it is speculated that strength deterioration will be caused by lateral buckling and local buckling. Supplemental lateral bracing (SLB) can prevent lateral buckling but not prevent local buckling in the RBS portion. In the previous research, the effect of vertical or horizontal stiffeners in RBS portion was shown to restrain local buckling of the RBS portion. But RBS with vertical stiffeners causes stress concentration at flange, and strength of RBS with horizontal stiffeners is lower than RBS with vertical stiffeners. In this paper, various patterns of placing stiffeners at the RBS portion are presented. The effect of vertical stiffeners and horizontal stiffeners arranged at the RBS portion is discussed based on length. It is confirmed that, without placing supplemental lateral bracing (SLB), vertical and horizontal stiffeners can delay the occurrence of local buckling and prevent stress concentration. Moreover, the strength can be sustained above0.8Mp.


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## Body

## 1. Introduction

In Northridge earthquake and Kobe earthquake, serious damage occurred. Damage of beam-to-column joints of steel structures was especially critical. From the damage investigation, Reduced Beam Section (RBS) has been proposed for improving the plastic rotation capacity of the beam-to-column joints. The high plastic rotation capacity of RBS has been shown experimentally, and the design code has been proposed (Engelhardt and Sabol [1], Uang and Fan [2]). However, it is speculated that lateral buckling or local buckling might be easier to occur, because of deterioration of stiffness of the RBS portion. In design code, arrangement of supplemental lateral bracings is provided for lateral buckling, but there is no provision for local buckling. For preventing strength degradation due to local buckling, Li et al. [3] proposed placing vertical stiffeners within the RBS portion. However, placing vertical stiffener tends to increase stress in RBS portion of the flange. Alternatively, Yu et al. [4] proposed placing horizontal stiffeners. The RBS beam with horizontal stiffeners certainly prevents stress concentration, but its strength is lower than RBS beam with vertical stiffeners.This paper presents the effect of the vertical and horizontal stiffener at the RBS portion on the basis of [3–5] and proposes the method for sustaining the deformation capacity of RBS beam.


## 2. Deformation Capacity of RBS Beams with Stiffeners Subjected to Cyclic Loading

### 2.1. Analysis Model

In this study, a general finite-element method (FEM) program MSC. MARC 2013 was used. As shown in Figure1(a), the analysis model is a half-span length (L/2) cantilever beam with a concentration load at the free-end.Figure 1
Beam modeling: (a) cantilever representation and discretization ([4]); (b) loading history ([4]) and definition of beam-end rotation; (c) details of the RBS portion and the RBS beam with supplemental lateral bracings ([4]); (d) detail of the RBS beam with vertical stiffeners ([3, 4]); (e) detail of the RBS beam with horizontal stiffeners; and (f) definition of strength measures ([4]).The beam cross sections areW24 × 76, W30 × 99, and W36 × 194. The slenderness ratio of the three beams is 73.2, because the slenderness ratio (L/ry) of RBS beam should be less than 77 (according to ANSI/AISC 341-10 [6]). The cross section properties are shown in Table 1. At the fixed-end section, all displacements and rotations of all nodes are restrained. At the free-end section, only Y-displacement of the central node is restrained. The elements of flange and web are four-node thick-shell elements, and a plate is set at the free-end modeled by eight-node solid elements. The portion near the fixed-end and a range about 1.2 times the beam height that sustains plastic deformation is divided into 25 mm × 25 mm elements, and the other portion is divided into about 50 mm × 50 mm. Young’s modules of the material is 2.1 × 105 MPa. The stress-strain relation adopted a bilinear model, in which the second stiffness is E/100 and the yield stress is 235 MPa. As shown in Figure 1(b), the beam is loaded cyclically with increasing beam-end rotation amplitude (θy = w/(L/2)) of 0.015, 0.030, and 0.045 rad, performing each load-amplitude in two cycles. According to the ANSI/AISC358-10 [7], supplemental lateral bracing (SLB) has to be located in the range of 0.5h from the end of the RBS that is farthest from the column face (Figure 1(c)). Figure 1(d) shows RBS beam with vertical stiffeners (Li et al. [3]), and Figure 1(e) shows RBS beam with horizontal stiffeners (Yu et al. [4]). In Li et al. [3], the accuracy of the FEM predictions of significant local buckling was assessed by comparing the FEM results to a physical test of a full-scale beam-column subassemblage by Engelhardt [8]. The analysis condition in this paper is according to Li et al. [3].Table 1
Properties of beam.
I x (mm4) r y (mm) L (mm) Width-thickness ratio a (mm) b (mm) c (mm) W24 × 76 8.50 × 108 48.91 3580 52.2 114 494 57 W30 × 99 1.62 × 109 53.66 3928 55.3 132 621 66 W36 × 194 4.96 × 109 65.8 4816 45.4 154 773 77In the following observations, the maximum strength during the whole loading history (Mmax) and the strength at the each cycle named “last strength” (Mlast) in this paper are adopted as the strength index (Figure 1(f)). When the moment of cross section of RBS portion is full plastic moment, the beam-end moment is 0.8Mp. Mp is the full plastic moment for full section.


### 2.2. Behavior of RBS Beam without Stiffener, Vertical Stiffener, and Horizontal Stiffeners

Figure2 shows the relationship between the beam-end moment (M) and the beam-end rotation forW36 × 194 beams. The beam-end rotation is calculated by the vertical displacement of loading point divided by beam length (L/2). Figure 2(a) is the graph of beam without SLB and stiffeners (called “Standard RBS”), (b) is the beam braced by SLB (called “RBS-SLB”), (c) is the beam with vertical stiffeners (called “VSTF”), and (d) is the beam with horizontal stiffeners (called “HSTF”). The beam-end moment is normalized by the full plastic moment (Mp). The strength reduces subsequently after the occurrence of local buckling in all models. In these figures, an open circle (○) indicates the local buckling point, and filled circle (●) indicates the peak point. The strength deterioration is observed in all analysis models. The local buckling point was determined by visually checking the deformed shape of FEM.Figure 2
The hysteresis loop of beam-end moment inW36 × 194 RBS beams: (a) Standard RBS; (b) RBS-SLB; (c) VSTF ([3]); (d) HSTF.
(a) (b) (c) (d)Figure3 shows the relationship between the last strength (Mlast) of each loading cycle. Figure 3(a) isW24 × 76, (b) isW30 × 99, and (c) isW36 × 194. It shows that almost all models with SLB or stiffeners have the last strength more than 0.8Mp. For Standard RBS, the last strength (Mlast) is less than 0.8Mp. Comparing the last strength of first cycle (0.015 rad) with the last strength of sixth cycle (0.045 rad), it is indicated that for theW24 × 76 andW36 × 194 of Standard RBS beam, the last strength of the sixth cycle is about 20% less than the last strength of first cycle. For theW30 × 99 beam, the strength reduced significantly by 67% of the last strength of first cycle. For the RBS-SLB beam, it shows that the last strength (0.045 rad) exceeds 0.8Mp. ForW30 × 99, the strength reduced by 26% of the maximum strength eventually.Figure 3
The last strength of each cycle: (a)W24 × 76; (b)W30 × 99; and (c) W36 × 194.
(a) (b) (c)SLB is effective in lateral buckling, and the strength degradation of beam is due to local buckling. The strength of HSTF (the beam with horizontal stiffeners) and VSTF (the beam with vertical stiffeners) is higher than Standard RBS. The stiffeners are effective for local buckling. The occurrence of local buckling is delayed by stiffeners, but the stiffeners cannot completely restraint local buckling.


## 2.1. Analysis Model

In this study, a general finite-element method (FEM) program MSC. MARC 2013 was used. As shown in Figure1(a), the analysis model is a half-span length (L/2) cantilever beam with a concentration load at the free-end.Figure 1
Beam modeling: (a) cantilever representation and discretization ([4]); (b) loading history ([4]) and definition of beam-end rotation; (c) details of the RBS portion and the RBS beam with supplemental lateral bracings ([4]); (d) detail of the RBS beam with vertical stiffeners ([3, 4]); (e) detail of the RBS beam with horizontal stiffeners; and (f) definition of strength measures ([4]).The beam cross sections areW24 × 76, W30 × 99, and W36 × 194. The slenderness ratio of the three beams is 73.2, because the slenderness ratio (L/ry) of RBS beam should be less than 77 (according to ANSI/AISC 341-10 [6]). The cross section properties are shown in Table 1. At the fixed-end section, all displacements and rotations of all nodes are restrained. At the free-end section, only Y-displacement of the central node is restrained. The elements of flange and web are four-node thick-shell elements, and a plate is set at the free-end modeled by eight-node solid elements. The portion near the fixed-end and a range about 1.2 times the beam height that sustains plastic deformation is divided into 25 mm × 25 mm elements, and the other portion is divided into about 50 mm × 50 mm. Young’s modules of the material is 2.1 × 105 MPa. The stress-strain relation adopted a bilinear model, in which the second stiffness is E/100 and the yield stress is 235 MPa. As shown in Figure 1(b), the beam is loaded cyclically with increasing beam-end rotation amplitude (θy = w/(L/2)) of 0.015, 0.030, and 0.045 rad, performing each load-amplitude in two cycles. According to the ANSI/AISC358-10 [7], supplemental lateral bracing (SLB) has to be located in the range of 0.5h from the end of the RBS that is farthest from the column face (Figure 1(c)). Figure 1(d) shows RBS beam with vertical stiffeners (Li et al. [3]), and Figure 1(e) shows RBS beam with horizontal stiffeners (Yu et al. [4]). In Li et al. [3], the accuracy of the FEM predictions of significant local buckling was assessed by comparing the FEM results to a physical test of a full-scale beam-column subassemblage by Engelhardt [8]. The analysis condition in this paper is according to Li et al. [3].Table 1
Properties of beam.
I x (mm4) r y (mm) L (mm) Width-thickness ratio a (mm) b (mm) c (mm) W24 × 76 8.50 × 108 48.91 3580 52.2 114 494 57 W30 × 99 1.62 × 109 53.66 3928 55.3 132 621 66 W36 × 194 4.96 × 109 65.8 4816 45.4 154 773 77In the following observations, the maximum strength during the whole loading history (Mmax) and the strength at the each cycle named “last strength” (Mlast) in this paper are adopted as the strength index (Figure 1(f)). When the moment of cross section of RBS portion is full plastic moment, the beam-end moment is 0.8Mp. Mp is the full plastic moment for full section.


## 2.2. Behavior of RBS Beam without Stiffener, Vertical Stiffener, and Horizontal Stiffeners

Figure2 shows the relationship between the beam-end moment (M) and the beam-end rotation forW36 × 194 beams. The beam-end rotation is calculated by the vertical displacement of loading point divided by beam length (L/2). Figure 2(a) is the graph of beam without SLB and stiffeners (called “Standard RBS”), (b) is the beam braced by SLB (called “RBS-SLB”), (c) is the beam with vertical stiffeners (called “VSTF”), and (d) is the beam with horizontal stiffeners (called “HSTF”). The beam-end moment is normalized by the full plastic moment (Mp). The strength reduces subsequently after the occurrence of local buckling in all models. In these figures, an open circle (○) indicates the local buckling point, and filled circle (●) indicates the peak point. The strength deterioration is observed in all analysis models. The local buckling point was determined by visually checking the deformed shape of FEM.Figure 2
The hysteresis loop of beam-end moment inW36 × 194 RBS beams: (a) Standard RBS; (b) RBS-SLB; (c) VSTF ([3]); (d) HSTF.
(a) (b) (c) (d)Figure3 shows the relationship between the last strength (Mlast) of each loading cycle. Figure 3(a) isW24 × 76, (b) isW30 × 99, and (c) isW36 × 194. It shows that almost all models with SLB or stiffeners have the last strength more than 0.8Mp. For Standard RBS, the last strength (Mlast) is less than 0.8Mp. Comparing the last strength of first cycle (0.015 rad) with the last strength of sixth cycle (0.045 rad), it is indicated that for theW24 × 76 andW36 × 194 of Standard RBS beam, the last strength of the sixth cycle is about 20% less than the last strength of first cycle. For theW30 × 99 beam, the strength reduced significantly by 67% of the last strength of first cycle. For the RBS-SLB beam, it shows that the last strength (0.045 rad) exceeds 0.8Mp. ForW30 × 99, the strength reduced by 26% of the maximum strength eventually.Figure 3
The last strength of each cycle: (a)W24 × 76; (b)W30 × 99; and (c) W36 × 194.
(a) (b) (c)SLB is effective in lateral buckling, and the strength degradation of beam is due to local buckling. The strength of HSTF (the beam with horizontal stiffeners) and VSTF (the beam with vertical stiffeners) is higher than Standard RBS. The stiffeners are effective for local buckling. The occurrence of local buckling is delayed by stiffeners, but the stiffeners cannot completely restraint local buckling.


## 3. Behavior of RBS Beam with Vertical Stiffeners and Horizontal Stiffeners

### 3.1. Length of Vertical Stiffeners

In order to prevent the strength degradation caused by local buckling, vertical and horizontal stiffeners were positioned as in Figure4. To restrain stress concentration at flange, vertical stiffeners are shorter than beam depth. The stiffeners do not touch with flange. Because only vertical short stiffeners cannot sustain strength, arrangement of short vertical stiffeners and horizontal stiffeners is proposed. Figure 5 shows the analysis result of RBS beam with vertical stiffeners shorter than beam depth (W24 × 76). The strength deteriorates gradually, and last strength is lower than 0.8Mp.Figure 4
The arrangement of vertical and horizontal stiffeners in RBS beam ([5]): (a) VHSTF-1/3; (b) VHSTF-1/2; and (c) VHSTF-4/5.
(a) (b) (c)Figure 5
The hysteresis loop of beam-end moment inW24 × 76 RBS beams with vertical short stiffeners.Figure6 shows the relationship between the beam-end moment (M/Mp) and the beam-end rotation (θ) of beams with vertical and horizontal stiffeners forW36 × 194. The beam-end rotation is calculated by the vertical displacement of loading point divided by beam length (L/2). Parameter is length of vertical stiffeners. The length of vertical stiffener is d/2 (called “VHSTF-1/2”), d/3 (called “VHSTF-1/3”), and 4d/5 (called “VHSTF-4/5”). However last strength of Standard RBS is 0.75Mp; last strength of VHSTF-4/5 is over 0.8Mp. Vertical and horizontal stiffeners are effective for local buckling.Figure 6
The hysteresis loop of beam-end moment inW36 × 194 RBS beams: (a) Standard RBS; (b) VHSTF-1/3; (c) VHSTF-1/2; (d) VHSTF-4/5.
(a) (b) (c) (d)Figure7 shows the relationship between the last strength and cycle. The vertical axis is the beam-end moment (M/Mp), and the horizontal axis is cycle. From Figure 7 VHSTF-4/5 sustains 0.8Mp, but last strengths of VHSTF-1/2 and VHSTF-1/3 are less than 0.8Mp at sixth cycle. Evidently, the strength deterioration becomes smaller with the increase of the length of vertical stiffener. VHSTF-4/5 is most effective.Figure 7
The last strength of each cycle: (a)W24 × 76; (b)W30 × 99; and (c)W36 × 194 ([5]).
(a) (b) (c)


### 3.2. Stress Distribution

From the preceding analysis, it is confirmed that sixth last strength of RBS beam locating H shaped form of vertical and horizontal stiffeners in 1/3 length of RBS (b/3) can maintain almost the same strength with the RBS-SLB beams or above 0.8Mp. However, stress concentration may occur around the stiffener. In addition, because the RBS section was reinforced by horizontal stiffeners, the stress around beam-to-column Joint may increase. Therefore, it is necessary to examine the stress state at the fixed beam-end and central part of RBS portion. Here VHSTF-1/3, VHSTF-1/2, and VHSTF-4/5 are discussed and compared with Standard RBS beams and RBS-SLB.Figure8 shows the Von Mises stress distribution at the fixed-end and the RBS central portion of the 6th cycle forW36 × 194 beams. Figures 8(a) and 8(b) show the stress distribution of upper flange and lower flange on the fixed-end section, and (c) and (d) show the result of RBS portion. The vertical axis is the stress normalized by the yield stress, and the horizontal axis is the position of monitoring nodes, shown in Figure 8(e).Figure 8
The stress distribution at the lower and upper flange of the fixed-end and RBS portion (W36 × 194): (a) upper flange at fix end; (b) lower flange at fix end; (c) upper flange at RBS portion; (d) lower flange at RBS portion; (e) the stress monitoring points.
(a) (b) (c) (d) (e)Figure8 shows that the stress at the fixed-end tends to increase, and the stress at the RBS portion tends to decrease by placing stiffener. As shortening the length of the vertical stiffener, the stress around the beam-end reduced, and the stress at RBS portion increased. Similar maximum stress to RBS-SLB is observed at VHSTF-4/5.Table2 is the maximum stress at the fixed-end and RBS portion for three sections at the maximum amplitude of sixth cycle. ForW24 × 76, the stress increase at the beam-end is greater than that of RBS-SLB. At the RBS portion, maximum stress ratio of VHSTF-4/5 is 1.80. ForW30 × 99 andW36 × 194, the stress at the fixed-end increases to 1.51σy and 1.85σy in VHSTF-4/5, but the stress is smaller than that of RBS-SLB.Table 2
The maximum stress at the maximum displacement of the RBS beams during the sixth cycle.
RBS SLB VSTF HSTF VHSTF-1/3 VHSTF-1/2 VHSTF-4/5 W24 × 76 Fixed end 1.10 1.12 1.20 1.13 1.13 1.20 1.19 RBS section 1.63 1.56 2.06 1.65 1.77 1.77 1.80  W30 × 99 Fixed end 1.15 1.21 1.12 1.26 1.21 1.22 1.18 RBS section 1.43 1.76 1.83 1.51 1.55 1.50 1.51  W36 × 194 Fixed end 1.15 1.21 1.35 1.23 1.16 1.22 1.23 RBS section 1.90 2.20 2.07 1.90 2.00 1.93 1.85Although the maximum stress of VSTF is twice yield stress (the study of Li et al. [3]), the influence of vertical and horizontal stiffeners on the flange of RBS portion is smaller than VSTF. Moreover the maximum stress of HSTF is similar to that of VHSTF.From the above results, the method to satisfy strength and performance capacity is using 2 pairs of H shaped stiffeners of length of 4d/5.


## 3.1. Length of Vertical Stiffeners

In order to prevent the strength degradation caused by local buckling, vertical and horizontal stiffeners were positioned as in Figure4. To restrain stress concentration at flange, vertical stiffeners are shorter than beam depth. The stiffeners do not touch with flange. Because only vertical short stiffeners cannot sustain strength, arrangement of short vertical stiffeners and horizontal stiffeners is proposed. Figure 5 shows the analysis result of RBS beam with vertical stiffeners shorter than beam depth (W24 × 76). The strength deteriorates gradually, and last strength is lower than 0.8Mp.Figure 4
The arrangement of vertical and horizontal stiffeners in RBS beam ([5]): (a) VHSTF-1/3; (b) VHSTF-1/2; and (c) VHSTF-4/5.
(a) (b) (c)Figure 5
The hysteresis loop of beam-end moment inW24 × 76 RBS beams with vertical short stiffeners.Figure6 shows the relationship between the beam-end moment (M/Mp) and the beam-end rotation (θ) of beams with vertical and horizontal stiffeners forW36 × 194. The beam-end rotation is calculated by the vertical displacement of loading point divided by beam length (L/2). Parameter is length of vertical stiffeners. The length of vertical stiffener is d/2 (called “VHSTF-1/2”), d/3 (called “VHSTF-1/3”), and 4d/5 (called “VHSTF-4/5”). However last strength of Standard RBS is 0.75Mp; last strength of VHSTF-4/5 is over 0.8Mp. Vertical and horizontal stiffeners are effective for local buckling.Figure 6
The hysteresis loop of beam-end moment inW36 × 194 RBS beams: (a) Standard RBS; (b) VHSTF-1/3; (c) VHSTF-1/2; (d) VHSTF-4/5.
(a) (b) (c) (d)Figure7 shows the relationship between the last strength and cycle. The vertical axis is the beam-end moment (M/Mp), and the horizontal axis is cycle. From Figure 7 VHSTF-4/5 sustains 0.8Mp, but last strengths of VHSTF-1/2 and VHSTF-1/3 are less than 0.8Mp at sixth cycle. Evidently, the strength deterioration becomes smaller with the increase of the length of vertical stiffener. VHSTF-4/5 is most effective.Figure 7
The last strength of each cycle: (a)W24 × 76; (b)W30 × 99; and (c)W36 × 194 ([5]).
(a) (b) (c)


## 3.2. Stress Distribution

From the preceding analysis, it is confirmed that sixth last strength of RBS beam locating H shaped form of vertical and horizontal stiffeners in 1/3 length of RBS (b/3) can maintain almost the same strength with the RBS-SLB beams or above 0.8Mp. However, stress concentration may occur around the stiffener. In addition, because the RBS section was reinforced by horizontal stiffeners, the stress around beam-to-column Joint may increase. Therefore, it is necessary to examine the stress state at the fixed beam-end and central part of RBS portion. Here VHSTF-1/3, VHSTF-1/2, and VHSTF-4/5 are discussed and compared with Standard RBS beams and RBS-SLB.Figure8 shows the Von Mises stress distribution at the fixed-end and the RBS central portion of the 6th cycle forW36 × 194 beams. Figures 8(a) and 8(b) show the stress distribution of upper flange and lower flange on the fixed-end section, and (c) and (d) show the result of RBS portion. The vertical axis is the stress normalized by the yield stress, and the horizontal axis is the position of monitoring nodes, shown in Figure 8(e).Figure 8
The stress distribution at the lower and upper flange of the fixed-end and RBS portion (W36 × 194): (a) upper flange at fix end; (b) lower flange at fix end; (c) upper flange at RBS portion; (d) lower flange at RBS portion; (e) the stress monitoring points.
(a) (b) (c) (d) (e)Figure8 shows that the stress at the fixed-end tends to increase, and the stress at the RBS portion tends to decrease by placing stiffener. As shortening the length of the vertical stiffener, the stress around the beam-end reduced, and the stress at RBS portion increased. Similar maximum stress to RBS-SLB is observed at VHSTF-4/5.Table2 is the maximum stress at the fixed-end and RBS portion for three sections at the maximum amplitude of sixth cycle. ForW24 × 76, the stress increase at the beam-end is greater than that of RBS-SLB. At the RBS portion, maximum stress ratio of VHSTF-4/5 is 1.80. ForW30 × 99 andW36 × 194, the stress at the fixed-end increases to 1.51σy and 1.85σy in VHSTF-4/5, but the stress is smaller than that of RBS-SLB.Table 2
The maximum stress at the maximum displacement of the RBS beams during the sixth cycle.
RBS SLB VSTF HSTF VHSTF-1/3 VHSTF-1/2 VHSTF-4/5 W24 × 76 Fixed end 1.10 1.12 1.20 1.13 1.13 1.20 1.19 RBS section 1.63 1.56 2.06 1.65 1.77 1.77 1.80  W30 × 99 Fixed end 1.15 1.21 1.12 1.26 1.21 1.22 1.18 RBS section 1.43 1.76 1.83 1.51 1.55 1.50 1.51  W36 × 194 Fixed end 1.15 1.21 1.35 1.23 1.16 1.22 1.23 RBS section 1.90 2.20 2.07 1.90 2.00 1.93 1.85Although the maximum stress of VSTF is twice yield stress (the study of Li et al. [3]), the influence of vertical and horizontal stiffeners on the flange of RBS portion is smaller than VSTF. Moreover the maximum stress of HSTF is similar to that of VHSTF.From the above results, the method to satisfy strength and performance capacity is using 2 pairs of H shaped stiffeners of length of 4d/5.


## 4. Comparison between VSTF, HSTF, and VHSTF-4/5

Figure9 shows the relationship between the last strength (M/Mp) and cycle. Figure 9(a) isW24 × 76, (b) isW30 × 99, and (c) isW36 × 194. HSTF and VHST are almost the same. The strengths ofW24 × 75 andW30 × 99 are similar to RBS-SLB. VHSTF-4/5 is more effective than VHST. Because of the local buckling of flange, the strength of VSTF decreases. ForW36 × 194, the strength of VHSTF-4/5 is lower than that of RBS-SLB, but strength requirement is satisfied.Figure 9
Comparison of the last strength of each cycle ([5]): (a)W24 × 76; (b)W30 × 99; and (c)W36 × 194.
(a) (b) (c)Figure10 shows deformation of VSTF, HSTF, and VHSTF-4/5 at the sixth cycle. The deformation at flange of VHSTF-4/5 is smaller than that of VSTF. The deformation at RBS portion of VHSTF-4/5 is smaller than that of HSTF.Figure 10
A comparison of deformation in RBS portion at the sixth cycle (W36 × 194) ([5]): (a) VSTF; (b) HSTF; (c) VHSTF-4/5.
(a) (b) (c)From the above results, the strength of VHSTF-4/5 is similar to that of VSTF and HSTF, but deformation of VHSTF-4/5 is smaller than that of VSTF and HSTF.


## 5. Conclusions

This paper presents a numerical study of local instability and the effect of vertical and horizontal stiffeners on RBS beams subjected to cyclic loading. The major findings obtained from this study are summarized as follows:(1)
Arranging H shaped vertical and horizontal stiffeners at RBS portion is effective in preventing local instability as vertical stiffeners (VSTF, Li et al. [3]) and horizontal stiffeners (HSTF, Yu et al. [4]). The effective length of vertical stiffener is 80% beam depth (VHSTF-4/5).(2)
Though the strengths of VSTF, HSTF, and VHSTF-4/5 are almost the same, deformation of VHSTF-4/5 is smallest among the 3 types.(3)
The stress at flange of VHSTF-4/5 is not so large; the maximum stress of RBS-SLB and VHSTF-4/5 is almost same.



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*Source: 6173873-2018-03-01.xml*