Research Article  Open Access
Jilong Li, Yanan Tang, Xuanming Liu, "Research on Dissipation and Fatigue Capacity of Nonstiffener Shear Panel Dampers", Advances in Civil Engineering, vol. 2015, Article ID 191359, 13 pages, 2015. https://doi.org/10.1155/2015/191359
Research on Dissipation and Fatigue Capacity of Nonstiffener Shear Panel Dampers
Abstract
Passive energy dissipation control system can effectively control structure response under seismic action. As a form of passive energy dissipation control, yielding steel shear panel dampers can dissipate energy of the ground motion very well with the plastic deformation. By monotonic cyclic loading, hysteretic performance of the 15 mm thick coreboard nonstiffener shear panel damper is tested, and the test shows that the damper has a superior hysteretic performance. Using finite element analysis software ABAQUS, and taking height to thickness ratio of the coreboard as variable, the qualitative analysis on the damper is carried out, and results show that the critical height to thickness ratio of shear panel damper is between 30 and 35. Three groups of 15 mm thick coreboard nonstiffener shear panel dampers are tested by constant amplitude cyclic loading under different amplitudes; the results show that the fatigue performance is fine and the damper is a good energy dissipation device.
1. Introduction
Research and application of structure vibration control in civil engineering has been carried out more than 40 years ago [1], which is brought up by the Japanese scholars Kobori and Minai [2] and the American scholar Yao [3], respectively, in the 60s and 70s of 20th century, and then a large number of scholars have made further researches on it. In recent years, many structural vibration control devices have been applied to the wind, waves, and seismic response control. Structure vibration control mainly includes three aspects: base isolation, passive vibration isolation [4, 5], and active and semiactive intelligent control. Although the base isolation is able to control the structure vibration, once it is damaged or reaches fatigue limit, the replacement is difficult and expensive. Active, semiactive, and intelligent control is an ideal mode of vibration control; however, the complex control system and large energy driving pattern make the application greatly inconvenient. Passive energy dissipation damper does well in controlling the vibration of the structure; with its low cost, convenience to be replaced, and simple control system, it is an ideal vibration control mean in recent years.
Passive energy dissipation damper is to install energy dissipation elements of nonstructural component [6] in the structure, thus dissipating the energy of structure vibration and reducing the structural vibration response. Energy dissipation components in general can be divided into three kinds [5]: displacement related type, speed related type, and tuned vibration absorption type. Shear panel damper is a kind of displacement related type energy dissipation component, which dissipates the energy via elasticplastic deformation of metal materials [7]. In recent years, the shear panel damper has been widely used in building structures [8], of which there are two kinds of arrangements, brace type and column type, as shown in Figure 1. In the early years, the coreboard is mainly made of structural steel (mild steel) with the lower yield, such as North America A36, Japan SS400, and China Q235. These mild steels have the yield stress between 235 MPa and 300 MPa, whose ductility can reach about 30%. Test and actual application show that mild steel damper has the higher yield strength, and damping effect is not obvious during the small earthquake and wind vibration. To solve the problem, researches have been made in Japan firstly to use ultralow yield stress steel with the yield strength less than 100 MPa [9, 10] as seismic dampers [11, 12] and obtain good effect [13, 14]. The damper made of low yield point will yield firstly and absorb energy with repeated deformation to protect major structure when suffering the earthquake [15]. In China [16–18], the development and application of lowyieldpoint steel did not start until 2005; Shanghai Baosteel independently developed ultralow yield strength steel with the yield stress between 100 MPa and 225 MPa, including BLY100, BLY160, and BLY225. Since then domestic lowyieldpoint steel basically reaches the performance requirements of Japanese production. Figure 2 illustrates the comparison of stressstrain relationship between BLY100, SS400 (Q235), and SM400 (Q345).
(a) Brace type
(b) Column type
Nowadays, the research on lowyieldpoint steel shear panel damper is mainly focused on the theory analysis and finite simulation; the experimental research is still rare, especially in the study on fatigue performance. Since 2009, Zhongshuang [19, 20] tests the performance of shear panel damper made of low point steel; the results based on the skeleton curve and equivalent viscous damping coefficient show that this type of damper is an ideal equipment of energy dissipation. With this premise, two batches of nonstiffened shear panel damper are made of domestic lowyieldpoint steel. One batch is used to test hysteretic performance through monotonic cyclic loading, and the other batch is used to test fatigue performance through constant amplitude cyclic loading. By using finite element analysis software ABAQUS, with the height to thickness ratio of coreboard as variable, combined hardening model is chosen to simulate shear panel damper to determine the critical height to thickness ratio of shear panel dampers.
2. Test Research on Hysteretic Performance
2.1. Components Size and Material Properties
The shear panel damper specimen consists of three parts: top and bottom flange plates, left and right flange plates, and coreboard, as shown in Figure 3. The top and bottom flange plates are 37 mm thick steel plates made of Q345, providing rigid constraints for the coreboard and preventing torsion of damper, so that the stress state of coreboard is more close to pure shear. Left and right flange plates are 12 mm thick steel plates made of Q345 that prevent the excessive outofplane buckling of coreboard. The coreboard is 15 mm thick steel plate made of lowyieldpoint steel LYP100. The detailed dimension is illustrated in Figure 4.
In this paper, monotonic tensile tests were firstly conducted with the standard tensile specimen made of LYP100 and Q345. The properties of steels used in dampers are shown in Table 1.

2.2. Introduction of Experiment
The test is carried out on the reactingforce wall in the Structure and Seismic Experiment Center in School of Civil Engineering in Harbin Institute of Technology (HIT). In the test, articulated frame provides the constraints for dampers and hydraulic jack provides lateral force for the framework, as shown in Figure 5.
(a) Articulated frame
(b) Hydraulic jack
In the test, the displacement measurement mainly includes relative displacement of the top and bottom flange plates, outofplane buckling displacement of coreboard, and lateral displacement of the articulated framework. Displacement is measured by the Linear Variable Differential Transformer (LVDT). Figure 6 shows arrangement of displacement transducers. Two transducers, number 3 and number 4, are arranged on the top flange plates to measure torsion of damper in the loading process. Along the diagonal of coreboard, number 5, number 6, and number 7 transducers are arranged to measure outofplane buckling of the coreboard.
The loading history of hysteretic performance test consists of elastic stage and postyielding stage. In the elastic stage, two cycles are performed for each force level under the 0.5and 0.75 (is calculated by formula (1)). After that, the specimens are loaded cyclically according to the loading process in Figure 7 [12]. Here, is defined as the horizontal displacement at the top of the specimen relative to bottom divided by the clear height of corebored. There are 11 loading levels, with each level cycle being carried out twice. The loading is continued until the damper is damaged in the last level. The standard of damage is the bearing capacity of damper decrease by 10% or excessive outofplane buckling and cracks occurring in the coreboard [19, 20].
2.3. Analysis of Experiment Result
By monotonic cyclic loading, the hysteretic curves of damper LP15CY, whose coreboard is 15 mm thick, are obtained and shown in Figure 8. Normalized horizontal force () versus shear angle () relationship is obtained according to the following formula and shown in Figure 9:
Here,is the crosssectional area of the coreboard (not including left and right flange sections). is the yield stress of the coreboard material; MPa in this experiment.
Skeleton curve and the equivalent viscous damping coefficient [21] are important parameters to study damper seismic response. Skeleton curve is connection of the peak point of each hysteretic loop. Equivalent viscous damping coefficient is shown in Figure 10, whose calculating formula is as follows:
Here, is the area of one cycle hysteretic loop. According to the conception of skeleton curve and equivalent viscous damping coefficient, we can get two curves, as shown in Figures 11 and 12.
The hysteretic curve of LP15CY is very full with no pinching phenomenon, which means good plastic deformation ability, and the peak bearing capacity reaches 1200 kN meaning that the damper has high bearing capacity reserves. The skeleton curve shows a trend of rising without strength degradation phenomenon. The equivalent viscous damping coefficient curve also shows a trend of rising in the process of loading, which suggests that the hysteretic curve is getting fuller and fuller and the energy dissipation performance is getting better and better with the increase of loading displacement. Hysteretic curve, skeleton curve, and equivalent viscous damping coefficient curve have the same trend, indicating that the 15 mm thick coreboard damper has fine and stable performance. This damper is an ideal equipment of energy dissipation.
3. Finite Element Simulation
The experiments can test various properties of dampers, but the price of tests is expensive and the tests are also with low efficiency. Hence more analyses are performed with finite element analysis software ABAQUS. Firstly, some simulation analyses have been performed to make contrast with test results to find out reasonable models. Then various parameters analyses are performed on the basis of existing models to obtain properties of dampers.
3.1. Finite Element Model
On the basis of experiment model, a 1 : 1 finite element model is built. In this model, top and bottom flange plates are built with discrete rigid body elements; left and right flange plates and coreboard are built with shell elements, as shown in Figure 13.
(a) Geometric model
(b) Finite element model
3.2. Material Model
This paper uses the combined hardening model [22] to simulate the coreboard and the isotropic hardening model [22] to simulate the flange plates. The constitutive models of materials are obtained from the monotonic tensile tests. The nominal stressstrain curves obtained from tests are translated into the true stressstrain curves. The constitutive models of lowyieldpoint steel used in coreboard and Q345 steel used in flange plates are presented in Figures 14 and 15.
3.3. Analysis of Finite Element Simulation Results
On the basis of experiment loading history, the simulation analysis of hysteretic test is performed and then simulation hysteretic curves are obtained. According to the method used before, normalized force and displacement curves are shown in Figure 16. Figure 17 shows the comparison of test result and simulation result. Then the skeleton curve and equivalent viscous damping coefficient curve and comparison with test results are obtained and shown in Figures 18 and 19, respectively.
Through the analyses above, hysteretic curve, skeleton curve, and equivalent viscous damping coefficient curve of simulation results matched well with experiment results. From hysteretic and skeleton curves, when it comes to the positive loading, the peak value of each loop basically coincided with test result. Under the reverse loading, the peak value of each loop in simulation result is greater than the test result, but they have the same trend and no strength degradation phenomenon occurs. From the equivalent viscous damping coefficient curves, the trends of simulation result and test result are the same in general, both rising gradually. The increasing rate of test result is greater than simulation result. When it comes to the ninth level loading in simulation, the curve becomes horizontal, but the test curve keeps increasing through the whole loading history with no horizontal section. It is related to the unobvious cyclic hardening phenomenon in simulation. In conclusion, the finite element model can present the actual property of damper. So the model can be used for qualitative analysis of this kind of damper.
3.4. Height to Thickness Ratio
Height to thickness ratio [23, 24] is defined as the ratio value between height and thickness of coreboard. It is an important parameter in designing dampers. When designing a damper, the property of damper should be given priority and then comes the economic factor. So the ideal dampers should meet both the property and the economic requirements. Finding the critical height to thickness ratio of coreboard is very important. With the height to thickness ratio as variable, simulation analyses are performed with the model introduced before. Basic parameters of simulation are shown in Table 2.

Through the simulation, four normalized hysteretic curves with different height to thickness ratios are obtained and shown in Figure 20. According to the method put forward before, the skeleton and equivalent viscous damping coefficient curves obtained from hysteretic curves and the comparison of four curves are shown in Figures 21 and 22, respectively.
(a) LP1
(b) LP2
(c) LP3
(d) LP4
Through the analysis of hysteretic curves, skeleton curves, and equivalent viscous damping coefficient curves, with the decrease of height to thickness ratio, the hysteretic curves become more and more satiating. The hysteretic curves of LP1, LP2, and LP3 are all having pinching phenomenon; the curve of LP4 shows no pinching. From the skeleton and equivalent viscous damping coefficient curves, LP1, LP2, and LP3 all have decreasing trend after several loading steps, but LP4 has no decreasing stage with a stable energy dissipation performance. It can be concluded that the critical height to thickness ratio of coreboard is in the range of 30 and 35.
4. Experimental Study on Fatigue Property
4.1. Size of Specimens and Loading System
Fatigue property is an important factor in the design of shear panel dampers. An ideal damper should not only have good energy dissipation performance, but also have well fatigue property. This paper presents experiments on three nonstiffener shear panel dampers with 15 mm thick coreboard made of lowyieldpoint steel. The tests are with constant amplitude cyclic load to investigate the relationship between fatigue performance and the size of amplitude. The sizes of specimens used in the fatigue tests are the same as those in the hysteretic test. The serial number, basic parameters of specimens, and loading methods of experiments are shown in Table 3.

4.2. Result Analysis of Fatigue Experiments
The three dampers are tested under constant amplitude loading with the amplitude of 20 mm, 45 mm, and 60 mm, respectively. Then normalized hysteretic curves under different amplitudes are obtained and shown in Figures 23–25. According to the forcedisplacement hysteretic curve, every lap of energy dissipation for each damper under the corresponding amplitude is figured out, and the comparison between them is shown in Figure 26. Figure 27 shows the contrast of accumulated energy dissipation versus cyclic number about three dampers in different working conditions. The accumulated energy dissipation curves are the sum of every lap of energy dissipation. In the elastic stage of loading history, the test is conducted under two different force levels in order to measure the initial elastic stiffness of specimen. According to the test results, the initial elastic stiffness of specimen is fitted as shown in Table 4. Figure 28 presents the fitting initial elastic stiffness curves of specimen.

(a) Initial elastic stiffness fitting curves of 20 mm amplitude
(b) Initial elastic stiffness fitting curves of 45 mm amplitude
(c) Initial elastic stiffness fitting curves of 60 mm amplitude
Having cyclic loading with the amplitude of 20 mm, the hysteretic curves remain stable before 28 cycles. The hysteretic loops are full, with no pinching phenomenon, and the lap energy dissipation curves stay horizontal. The damper is with stable energy dissipation performance. After 28 cycles, the hysteretic loops start pinching. With the increase of cycles, the pinching phenomenon becomes more and more obvious; the distortion occurs and aggravates gradually. The lap energy dissipation curve shows a trend of decrease. Energy dissipation performance of the damper begins to degenerate. When it comes to 46 cycles, cracks appear in the middle of coreboard and the weld joint is failure between flange plates and coreboard. The failures are shown in Figure 29.
(a) Cracks of coreboard
(b) Weld failure
(c) Global deformation
Having cyclic loading with the amplitude of 45 mm, the hysteretic curves stay stable before 9 cycles. The hysteretic loops are full, with no pinching, and the lap energy dissipation curves keep horizontal. The damper is with stable energy dissipation performance. After 9 cycles, the hysteretic loops start pinching and the distortion occurs in the coreboard; with the increasing of cycles, the pinching and distortion are increasingly severe. Lap energy dissipation curve begins to decrease, and the decrease speed is faster than the test under the amplitude of 20 mm. Energy dissipation of the damper is starting to degenerate. When it comes to 16 cycles, the damper becomes failure. The failure is similar to the test with amplitude of 20 mm, as shown in Figure 30.
(a) Cracks of coreboard
(b) Weld failure
(c) Global deformation
Having cyclic loading with the amplitude of 60 mm, the hysteretic curves hold steady before 4 cycles. The hysteretic loops are full, with no pinching, and the lap energy curve is increasing with the cycle numbers. The damper has fine energy dissipation property. After 4 cycles, the distortion and pinching in coreboard appear and are more severe than the other two dampers analyzed before. When it comes to 11 cycles, the damper becomes failure. Figure 31 shows the failure mode of the damper; the cracks in the coreboard are more evident than the other two tests and it shows greater lateral buckling.
(a) Cracks of coreboard
(b) Weld failure
(c) Global deformation
According to all the analyses above, the shear panel dampers with 15 mm thick coreboard present fine fatigue capacity under small amplitude cyclic loading. With the increase of amplitude, the fatigue performance of dampers is getting worse and worse. From the accumulated energy dissipation curves, no matter what the amplitude size is, all the energies dissipated by the dampers are approaching each other. The initial elastic stiffness fitting curves show that the initial elastic stiffness is relatively large, indicating that the damper increases the structure total stiffness to some extent.
5. Conclusion
This paper has made an indepth investigation of the nonstiffener shear panel made of lowyieldpoint steel. According to hysteretic experiment, finite element simulation, and fatigue performance tests, the major findings of this study can be briefly generalized as follows:(1)Nonstiffener shear panel damper with 15 mm thick coreboard made of lowyieldpoint steel has a good hysteretic property. Under the cyclic loading with small amplitude, the property of the shear panel damper is stable, and the damper performs a fine fatigue property. This type of damper is an ideal energy consumption equipment.(2)It can be found that the critical height to thickness ratio of this type of nonstiffener shear panel damper is between 30 and 35 by using the finite element simulation. The range of the height to thickness ratio can be a reference of the damper design.(3)According to the constant amplitude cyclic loading test, failure modes of the three dampers are similar to each other. They all have the presentations as follows: cracks appearing in the middle of coreboard, break of the weld joint between flange plates and corebored, and major lateral buckling in the coreboard. The deformation of coreboard is not only in shear but also in distortion of plate. In the subsequent design, reducing the lateral buckling, distortion of plate, and the influence of weld joint should be taken into consideration.(4)From the every lap energy dissipation and accumulated energy dissipation curves, it can be concluded that this type of damper has a stable energy dissipation capacity and can dissipate large amounts of energy. Under cyclic loading with the amplitude of 20 mm, the hysteretic curves remain stable before 28 cycles and the hysteretic loops are full, indicating that the damper can function effectively for the smaller vibration. It can be a fine energy dissipation device of structural vibration control.
Disclaimer
The results, opinions, and conclusion expressed in the paper are all on behalf of the authors.
Conflict of Interests
The authors declare that there is no conflict of interests regarding the publication of this paper.
Acknowledgments
The work presented herein is part of a study in progress at Harbin Institute of Technology (HIT) under Grant no. 51478156 from the National Science Foundation of China (General Program), Grant no. E2015018 from the National Science Foundation of Heilongjiang, China (General Program), and Grant no. 51078118 from the National Science Foundation of China (General Program). Jilong Li as the NSFC Program Director thanks the members of the program, Yanan Tang, Xuanming Liu, and so forth, for their test researches and simulation analyses.
References
 O. Jinping, Structural Vibration Control—Active, SemiActive and Intelligent Control, Science Press, 2003 (Chinese).
 T. Kobori and R. Minai, “Analytical study on active seismic response control,” Transactions of the Architectural Institute of Japan, vol. 66, 1960. View at: Google Scholar
 J. T. P. Yao, “Concept of structural control,” ASCE Journal of Structure Division, vol. 98, no. 7, pp. 1567–1574, 1972. View at: Google Scholar
 J. P. Ou, B. Wu, and T. T. Soong, “Recent advances in research on and application of passive energy dissipation systems,” Earthquake Engineering and Engineering Vibration, vol. 16, no. 3, pp. 72–96, 1996. View at: Google Scholar
 T. T. Soong and G. F. Dargush, Passive Energy Dissipation Systems in Structural Engineering, John Wiley & Sons, London, UK, 1997.
 J. M. Kelly, R. I. Skinner, and A. J. Heine, “Mechanisms of energy absorption in special devices for use in earthquake resistant structures,” Bulletin of the New Zealand Society for Earthquake Engineering, vol. 5, no. 3, pp. 63–88, 1972. View at: Google Scholar
 Z.Y. Chen, H.B. Ge, T. Usami, and Y. Yuan, “Ultimate shear strength of shear panel damper under cyclic load,” Journal of Shenyang University of Technology, vol. 33, no. 2, pp. 219–225, 2011 (Chinese). View at: Google Scholar
 M. Nakashima, S. Iwai, M. Iwata et al., “Energy dissipation behaviour of shear panels made of low yield steel,” Earthquake Engineering & Structural Dynamics, vol. 23, no. 12, pp. 1299–1313, 1994. View at: Publisher Site  Google Scholar
 K. Otani, “Recent trend of technology for steel plates used in building construction,” Nippon Steel Technical Report, vol. 54, pp. 27–36, 1992. View at: Google Scholar
 M. Aohashi, H. Mochizuki, T. Yamaguchi et al., “Development of new steel plates for building structural use,” Steel Research, no. 334, pp. 17–28, 1989. View at: Google Scholar
 T. Yamaguchi, T. Takeuchi, T. Nagao et al., “Seismic control devices using lowyieldpoint steel,” Nippon Steel Technical Report, no. 77, pp. 65–72, 1998. View at: Google Scholar
 M. Nakashima, “Strainhardening behavior of shear panels made of lowyield steel. I: test,” Journal of Structural Engineering, vol. 121, no. 12, pp. 1742–1749, 1995. View at: Publisher Site  Google Scholar
 H. Tamai, H. Takenaka, T. Nakano, O. Kojima, K. Kondoh, and M. Hanai, “On hysteretic damper using lowyield stress steel plate installed in Kbraced frame,” in Proceedings of the Annual Meeting of Architectural Institute of Japan, pp. 1447–1450, Tokyo, Japan, September 1991 (Japanese). View at: Google Scholar
 M. Izumi, N. Kani, H. Narihara, Y. Kawamata, K. Ogura, and O. Hosozawa, “Low cycle fatigue test on shear yielding type lowyield stress steel hysteretic damper for response control, part 1 and 2,” in Proceedings of the Annual Meeting of the Architectural Institute of Japan, pp. 1333–1336, Tokyo, Japan, 1992 (Japanese). View at: Google Scholar
 L. Fu, Y.Q. Zhang, Y.R. Luo, Q. Yu, M.T. Li, and X.G. Zeng, “Low cycle fatigue properties of steel BLY160 with low yield point for damper,” Journal of Iron and Steel Research, vol. 27, no. 3, pp. 65–69, 2015. View at: Publisher Site  Google Scholar
 S. Fengming, W. Donghui, L. Zigang, and B. Mingzhuo, “Application and development of low yield point steel,” Material & Heat Treatment, vol. 37, no. 6, pp. 85–89, 2008 (Chinese). View at: Google Scholar
 S. Gong, G. Sheng, D. Yao, S. Li, and Q. Chen, “Research on steels for earthquake damping device,” Iron and Steel, vol. 36, no. 9, pp. 55–57, 2001. View at: Google Scholar
 D. Wen, F. Song, Z. Li et al., “Develop and performance study on low yield point steel used in earthquake control building,” (Chinese), http://www.chinabaike.com/z/yj/554590.html. View at: Google Scholar
 S. Zhongshuang, Research on behaviors of energy dissipation of shear panels dampers made of lowyield steel [M.S. thesis], Harbin Institute of Technology, Harbin, China, 2013.
 Z. Song, H. Li, L. Han et al., “Experimental study on hysteretic behavior of shear panel dampers made of steel with low yield point,” Journal of Disaster Prevention and Mitigation Engineering, vol. 34, no. 3, pp. 289–295, 2014. View at: Google Scholar
 W. Bin, Testing, analysis and design approaches of hysteretic energy dissipation systems [Ph.D. thesis], Harbin University of Civil Engineering and Architecture, 1998 (Chinese).
 H.F. Chen, Elasticity and Plasticity, China Architecture & Building Press, Beijing, China, 2004, (Chinese).
 S.J. Chen and C. Jhang, “Cyclic behavior of low yield point steel shear walls,” ThinWalled Structures, vol. 44, no. 7, pp. 730–738, 2006. View at: Publisher Site  Google Scholar
 C. Zhang, Z. Zhang, and J. Shi, “Development of high deformation capacity low yield strength steel shear panel damper,” Journal of Constructional Steel Research, vol. 75, pp. 116–130, 2012. View at: Publisher Site  Google Scholar
Copyright
Copyright © 2015 Jilong Li et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.