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Applied mathematics in Engineering, Management and Technology 2 (6) 2014:608-621
www.amiemt-journal.com
608
Abstract
After North rich (1994) earthquake, many ideas were offered about manner of
design and perform steel structures like juncture shaft with slotted web-reduced
flange. In this article, we discuss specification of this juncture for manners of shaft
with upper and beneath flange which juncture to pier and reduced section is
considered by slotting. Number and diameter of slots and lacking or existing flanges
is one of the parameters that are considered. For this, juncture suggested is analyzed
by cycling method and after drawing hysteresis method, it's beneath surface shows
scale of energy waste, is determined. In all models, non linear behaviors are
considered.
Keywords: Slotted Web-Reduced Flange, Correlated Flange, Cycling Loading, Wasted
Energy, Hysteresis Chart
1- Introduction
North rich earthquake at 1994 showed that moment steel system with welding junctures is in the rank of
formatting structure systems and have many disadvantages. After that event, it was showed that many buildings
exposed to fracture in juncture area, thus, many researches were performed for finding defects and restore
cycling behavior by moment's junctures.
In generally, researchers concentrated on two ideas. Some of them were following to removing situation of
plastic joint. Flange juncture with RBS and flange with SBW were formed based on second method.
In RBS method, with cutting flange section, flange is transmitted to proximity column. Lab studies were
performed on it and confirmed that this juncture can change non elastic shapes and obtains acceptable plastic
cycles.
One of the parameters which have many effects on fracture of flanges is plasticity of juncture stream. The
discussion showed that weak juncture stream confronts to great wear shapes which is derived from fracture
mode in juncture area. Since weak juncture stream has high ability for wasting energy but it is not advised to
use weak juncture stream. ( 5-4)
Also, although strong juncture stream reduces fracture potential but in other word, increases probable of
instability especially for juncture flange with RBS. According to lab discussions, it was recognized that medium
juncture stream has suitable performance ( 7-6)
RBS was cited as restored steel structure by SSDA of America in 1997 (8). This juncture is regarded as
combination of concreted junctures because in one section, body of flange is void and enhances juncture area by
wear plate. In this juncture, wear force is omitted and side- curvature event is minimized. Richard and et al 9,
confirmed its performance with experiments on this juncture.
Maleki and et al 10, discussed RBS and SBS in direct juncture for flange to column. They concluded that in this
manner, time performance is obtained when juncture stream is considered as weak.
As for said, in this article, RBS and SBW will be considered for Cloven juncture by upper and beneath flanges
when the flange is reduced by slotting.
2- Numerical Study on Juncture
For discussion effective parameters on juncture behavior, a numerical study was performed. As figure 1
displayed, models of one flange with IPE 300 and column with section HE200B were formed in Europe. Upper
and beneath flanges are designed by regulations of AISC-2010.(11)
Analytic Discussion of Juncture Behavior Stocked with Punctured
and Cloven Wing as well as Upper and Beneath Flange
Ali Ahmadi, Hamzeh Keakha, Mahmoodreza Tabatabai
Islamic Azad University Branch Of Zahedan
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Free ends of the shaft show changing shape of shaft in original form, beneath column is as joint and in upper
section, rolling base is considered.
The aim is obtainable by two steps, in first step; all models are analyzed by system and by 8 points, maxim
place of obeisance of elastic model is determined. This place shows crisis point.
In second step, juncture is located by cycling loading and is evaluated by Langer- Doran chart derived from
analysis and in all analysis, non linear behavior is considered.
In numerical models, number and diameter of slot, effect of correlation flange is considered too.
Figure 1- General model of Juncture
Details of models are as following:
2.1. Controlling Points
As displayed above, for discussion maximum points of obeisance of elastic model, 8 controls points are
considered in wing of flange. Figure 2 shows place of locating these points. And table 1 shows its
specifications.
Figure 2- Place of Controlling Points in Limited Element Model
Table 1- Specifications of controlling points for determining Elastic obeisance points
Specification
(mm)
No. of controlling
point
(0,0,150) 0
(100,0, 150) 1
(200,0, 150) 2
(220,0, 150) 3
(250,0, 150) 4
(280,0, 150) 5
(380,0, 150) 6
(480,0, 150) 7
2.2. Area leaned for flange
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In this area, slotting is sued for weakening wing of flange. Figure 3 shows details, similarly, the numbers are
shown in table 2.
Figure 3- Details of Slots in wings of flange
In this juncture, slots with diameters 1, 2, 3 cm have minimum 2D distances are evaluated. In this part, D shows
slots in wing of flange.
Table 2- scales of Slots mm
Beam a b C tf tw bf d
IPE 80 200 35 10.7 7.1 150 300
2.3. Upper and Beneath Flange
Dimensions of upper plates are determined as 200×170×15 and dimensions of beneath plates as 200×200×15.
2.4.Correlation Plates
Effect of correlation plates is discussed in seismic performance. In numerical models, thick of upper and
beneath plates are considered.
2.5.Incision Plate
Scale of incision plate is considered as 200×250×20 in all charts.
2.6.Details of Slotted
Plane of slotted with use of results from other researches was performed by seismic institute of America 8.
Based on it, in all models, width of slot to end of incision plate equals to 3/2 mm and from end of incision plate
to end section is 6/4 mm. Figure 4 shows end of slot with diameter 21 mm.
Its aim is to transit plastic from place of juncture to column and make a crisis place in remote place. Based on
researches, length of 280 cm is considered for this part. 10.
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Figure 4- Details of Juncture SBW
3- Analysis of limited Parts
For modeling and analysis on non linear models, Abacus commercial software is used. 12
3.1.Elements and Meshing
The samples are modeled by nodal element 4-shell as integrating reduced. Shell element has strength, wear,
curvature and axial resistance and its behavior shows bend and crest. This element cause to change its shape out
of page because of hardening by cycling. Shell element can change plasticity of materials, change of shapes and
great obeisance. This element has freedom degree 6: place change in straight x, y,z and turning around axels
x,y,z.
3.2.Modeling of Materials
Non linear behavior of materials is obtained by Kinematic- isotropic hardening with use of Ziegler. Figure 5
shows obeisance chart of consumable materials ASTM A527, elasticity model is MPa6101.2 and poison
coefficient is 0/3.
3.3.Loading Protocol
A sample loading are as control by place change and is acted to the end of beam. In analysis, all models in
loading 120 kn. In discussion cycling juncture, SAC is used. Figure 6.
In this manner, all models are loading to cycling angel 0.04. 13
Figure 6- Loading Protocol
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Figure 7- Tension – obeisance steel curvature
4- Nomenclature of Models
Table 4 shows summary of models. Model nomenclature is based on diameter and number of slots and lacking
correlation plates.
Table 4- Nomenclature of Samples analyzed
5- Analysis Results
Models described are recognized under loading and the results are compared by end of juncture with similar
specifications.
No. of slots Diameter of
slot (cm) Continuity plate Specimen
2 1 With continuity plate CPD1N2
3 1 With continuity plate CPD1N3
4 1 With continuity plate CPD1N4
2 1 Without continuity plate NCPD1N2
3 1 Without continuity plate NCPD1N3
4 1 Without continuity plate NCPD1N4
2 2 With continuity plate CPD2N2
3 2 With continuity plate CPD2N3
4 2 With continuity plate CPD2N4
2 2 Without continuity plate NCPD2N2
3 2 Without continuity plate NCPD2N3
4 2 Without continuity plate NCPD2N4
2 3 With continuity plate CPD3N2
3 3 With continuity plate CPD3N3
4 3 With continuity plate CPD3N4
2 3 Without continuity plate NCPD3N2
3 3 Without continuity plate NCPD3N3
4 3 Without continuity plate NCPD3N4
With continuity plate NORMAL FLANGE-CP
Without continuity plate NORMAL FLANGE-NCP
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Figure 7- Obeisance of controlling points in pressure beam for decorating slots with diameter 1 cm
6- Discussion of Elastic obeisance charts
After performing analysis, equal elastic obeisance is obtained in controlling points. Figure 7, 9, 11. Since we
can obtain place of elastic obeisance point, this area shows that plastic joint is located in this point and thus, it
can remove by juncture point because of welding joints.
Figure 7 shows results of models with number and diameter 1 cm with and without plates. As displayed, place
of more obeisance is located at all charts. This problem shows that place of plastic joint is on welding point.
As for figure 7, about effect of correlation plates, we can cite that if the more elastic obeisance is happened in
two points, but correlation points show their effective performance in points two and five. Difference is about
lacking use of more correlation plates.
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Figure 8. Hysteresis response with different decorations with diameter 1 cm
Figure 9 shows results for slots with diameter 2 cm. as for charts, we know that more obeisances are variable
between controls points like two and five. In this section, we see role of correlation plates in juncture function.
As for figures 9a, 9b, 9c, if we use continued plates, crisis area is transmitted to control point 5. Figures 10d, 10
e and 10f show that lacking use of continuity plates can locate maxim point on point two. Thus, continuity
plates influences on plastic joint positively.
Figure 11 shows charts from covered analysis from samples with diameter 3 cm. as for charts, it was seen that
with increasing slot diameter to 3 cm, place of occurrence locates in point 5. Also, the charts show that
continuity plates have a few effects on situation of maxim obeisance.
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Figure 9. Controlling points obeisance in pressure wing of beam for decorating different slots with diameter 2
cm
7- Discussion of hysteresis Charts
Hysteresis responses of numerical models are shown in figures 10, 18, 12. Beam anchor is calculated from
column level and rotation values are calculated from dividing place change by its length. Beneath level of the
charts show scales of energy wastes. Table 5 shows hysteresis curvatures.
As for results, the samples have stable hysteresis instead the manner of the slots with diameter 3 cm is used for
weakening it. As for charts 12a, 12b, 12c, it is displayed that with increasing drift to 0/04 radian, we see
weakening resistance and hardening.
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Figure 10. Juncture hysteresis response with different decorations of slots with diameter 2 cm
As for hysteresis charts and it's beneath level which show energy wastes, we can conclude that if we use
continuity plates, energy wasted is so more than before.
Figure 11. Controlling point obeisance in pressure wing for different decoration slots with diameter 3 cm
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Figure 12. Juncture hysteresis response with different decoration for slots with diameter 3 cm
CPD3N4
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NCPD3N2 NCPD3N3
NCPD3N4
8- Normal Juncture Charts
For better comprehension of effect of slots in wing, the models are considered with same elements in wing and
elastic obeisance charts are obtained. Figures 13 and 14 show the charts obtained from analysis. As displayed,
although hysteresis charts show stable behavior but place of obeisance occurrence is on place of juncture of
beam to column.
Figure 13. Controlling point obeisance in pressure wing of beam with current juncture
Normal connection WCP
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Normal Connection WOCP
Figure 14. Hysteresis Response for current beam
Normal Connection WCP
Normal Connection WOCP
The results are as summary on table 5.
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Table 5. General Results for sample analysis
Equal controlling point for more
obeisance elastic
More Elastic Equal
Obeisance E(KN.m) Specimen
2 0.00281402 20.793 CPD1N2
2 0.00249142 20.782 CPD1N3
2 0.00269419 20.711 CPD1N4
2 0.00271735 19.101 NCPD1N2
2 0.00251738 19.015 NCPD1N3
2 0.00261742 18.764 NCPD1N4
5 0.00262733 20.744 CPD2N2
5 0.00271823 20.705 CPD2N3
5 0.00276894 20.691 CPD2N4
2 0.00261784 18.826 NCPD2N2
2 0.00243777 18.97 NCPD2N3
2 0.00231456 18.934 NCPD2N4
5 0.00251281 18.951 CPD3N2
5 0.00261753 18.855 CPD3N3
5 0.00261767 19.019 CPD3N4
5 0.00228984 18.82 NCPD3N2
5 0.00231888 18.713 NCPD3N3
5 0.00259859 18.645 NCPD3N4
2 0.00281373 20.677 NORMAL
FLANGE-CP
2 0.00271691 18.93 NORMAL
FLANGE-NCP
9.Concluding
One of methods for amending junctures applied is to use momentum SWRF which is derived from combination
of RBS and SBW. One of the weakest points is to cut wing beam. Because, this case can weaken concentration
tension on point and also, needs to professional workers for it. For removing these problems, it is suggested that
to use slots for weakening wing beam and for reaching to it, juncture behavior is evaluated by analysis and
cycling loading.
As for results obtained from analysis, it is seen that slots with diameter 1 cm are not suitable, because place of
obeisance is on place of juncture beam that can make dangerous area. Slots with diameter 2 cm is acceptable
when use as well as continuity plates, since lacking use of continuity plates, we see elastic equal in juncture of
beam to column.
Similarly for samples with diameter 3 cm, the result for elastic obeisance is better and continuity plates don’t
influence on crisis area.
In other word, hysteresis behavior show that slots with diameter 3 cm have downfall pressure in change places
with 0.04 rad, whereas, hysteresis for samples without plates is stable.
Although, hysteresis behavior for slotted models with diameter 3 cm is stable without continuity plates but it is
pointed that few energy waste is sensible for slotted samples with diameter 2 cm.
As for said contents, optimized decoration for weakening wing beam in SBW is to perform slots with diameter
2 cm with continuity plates.
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