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1,2,3,4
(CB1, CB2&CB3)
(CB8, CB9 and CB10)
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Group A
DGroup
(IDARC-4& ANSYS-10)
Group Parametric study Specimen
A Type of column reinforcement CB1,CB2&CB3CB8,CB9&CB10
Size of column CB1&CB8
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AD
ACI 318-95
A
CB2&CB9CB3&CB10
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D
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All
in dimensions
mm.Fusion Bonded Steel Bars (FS).
Epoxy Coated Steel Bars (ES).
Normal High Grade Steel Bars (NS).
COLUMNBEAM
SPECIMEN
SERIAL
ReinforcementsCross-sectionReinforcementsCross-
section
Typeofcoat
Stir
rups
Stir
rups
Typeofcoat
Longitudinal
Longitudinal
De
pth
Width
Stirrups
Typeofcoat
Bottom
Top
De
pth
Width
NS
8mm
FS
4
16mm
300mm
200mm
8mm
NS
3
16mm
3
16mm
400mm
200mm
CB11
NSESCB22
NSNSCB33
NSFS
8
16mm
200
mm
200
mm
CB84
NSESCB95
NSNSCB106
Cement Fine Aggregate
(Sand)
Coarse Aggregate
(Gravel)
Water/Cement
Ratio
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Strain GaugesLinear Variable Displacement Transducer (L V D T)Data Acquisition
1 1.75 3.5 0.55
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Fig (5): Theoritical Displacement History,
-80
-60
-40
-20
0
20
40
60
80
0 5 10 15 20 25 30 35 40
Cycle No.
Displacement(cm)
(CB3)
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-8
-6
-4
-2
0
2
4
6
8
-60 -40 -20 0 20 40 60
Displacement(mm)
Load(tons)
Load versus
Displacement Hysteresis loop,(CB2)
Stiffness Degradation, (C B 1)
0
0.2
0.4
0.6
0.8
1
1.2
1 3 5 7 9 11 13 15 17
Cycle No.
Stiffness
Energy Dissipation Capacity, (CB1)
0
200
400
600
800
1000
1200
1 3 5 7 9 11 13 15 17
Cycle No.
EnergyDissipation(ton.mm)
Stiffness Degradation & Energy Capacity , (CB1)
Specimens
Groups
Yield Displacement Displacement
at Failure
f(cm)
y (cm)
Compression
y (cm)
Tension
y (cm)
Considered
Group
(A)
CB1 1.15 1.2 1.175 3.5
CB2 1.0 0.9 0.95 3.8
CB3 1.2 1.0 1.0 3.6
Group CB8 1.5 1.1 1.1 4.5
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-5
-4
-3
-2
-1
0
1
2
3
4
5
-0.01 -0.005 0 0.005 0.01 0.015
Joint Shear Deformation (Rad)
Load(tons)
*
, (CB10)Applied Load Versus Joint Shear Deformation
Strain in Beam Top Rft. of (CB1)
-8
-6
-4
-2
0
2
4
6
8
-10 -5 0 5 10 15 20 25 30
Steel Strain,( )
Load,
(tons)
Strain in Beam Transverse Rft. of (CB1)
-8
-6
-4
-2
0
2
4
6
8
-10 -5 0 5 10 15 20 25 30
Steel Strain,( )
Load,
(tons)
, (CB1)Strain in Beam Reinforcement
,
(D) CB9 1.1 1.23 1.1 4.5
CB10 1.1 1.0 1.05 5.2
Groups Specimens
DisplacementDuctility
Factor
( f /y)
Maximum
Drift Ratio
(f/L)
Group
(A)
CB1 2.98 2.8
CB2 4.0 3.04
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(Displacement Ductility Factor andDrift Ratios.)
)(Yield and Ultimate Displacements.
0
1
2
3
4
5
6
7
Load(tans)
1 2 3 4 5 6 7 8 9 1 0
Number of Specimens (CBN)
Fig.(13):Comparison betwe en Ultimate Load and crack load for Different Specimens.
Crack Load
Ultimat load
(Comparison between UltimateLoad and Crack Load).
Ultimate Lateral Load for Compression and Tension.
CB1,CB2&CB3
(CB8,CB9&CB10CB3)(A
CB3 3.6 2.88
Group
(D)
CB8 4.09 3.6
CB9 4.09 3.6
CB10 4.95 4.16
GroupsSpecime
ns
Ultimate Lateral
Load(ton)Failure
cycle
Failure
Load(ton)Compress
ion
side
Tensio
n side
Group
(A)
CB1 6.557 6.846 15 4.338
CB2 5.717 5.558 15 3.512
CB3 6.56 6.85 15 3.204
Group
(D)
CB8 4.323 4.07 15 2.95
CB9 4.087 4.024 15 3.022
CB10 3.812 4.027 17 3.153
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Hysteresis Loop Envelope Of Load
Versus Displacement,
for (Group-A),(CB1,CB2,CB3).
-8
-6
-4
-2
0
2
4
6
8
-60 -40 -20 0 20 40 60
Displacement (mm)
Load(tons)
CB1 (F.S. Reinf.)
CB2 (E.S. Reinf.)
CB3 (N.S. Reinf.)
Hysteresis Loop Envelope of Load
Versus Displacement,
for(Group-A),(CB8,CB9,CB10)
-5
-4
-3
-2
-1
0
1
2
3
4
5
-80 -60 -40 -20 0 20 40 60 80
Displacement (mm)
Load(tons)
CB8 (F.S. Reinf.)
CB9 (E. S. Reinf.)
CB10 (N. S. Reinf.)
(Hysteresis Loop Envelope of Load Displacement, for (Group-A)).
Stiffness Degradation for Different
Specimens,
for (Group-A), (CB1,CB2,CB3)
0
0.2
0.4
0.6
0.8
1
1.2
1 3 5 7 9 11 13 15 17
Cycle No.
Stiffness
CB1(F. S. Reinf.)
CB2 (E. S. Reinf.)
CB3 (N. S. Reinf.)
Stiffness Degradation for Different
Specimens,
for(Group-A),(CB8,CB9,CB10)
0
0.2
0.4
0.6
0.8
1
1.2
1 3 5 7 9 11 13 15 17
Cycle No.
Stiffness
CB8 (F. S. Reinf. )
CB9 (E. S. Reinf. )
CB10 (N. S. Reinf.)
(Stiffness Degradation for Different Specimens, for (Group-A))
Energy Dissipation Capacity for Different
Specimens,
for(Group-A),(CB1,CB2,CB3).
0
200
400
600
800
1000
1200
1 3 5 7 9 11 13 15 17
Cycle No.
EnergyDissipation
(ton.mm)
CB1 (F. S. Reinf.)CB2(E. S. Reinf.)CB3(N. S. Reinf.)
Energy Dissipation Capacity for Different
Specimens,
for(Group-A),(CB8,CB9,CB10)
0
100
200
300
400
500
600
700
800
900
1 3 5 7 9 11 13 15 17 19
Cycle No.
EnergyDissipation
(ton.mm)
CB8 (F. S. Reinf. )
CB9 (E. S. Reinf. )CB10 (N. S. Reinf. )
(Energy Dissipation Capacity for Different Specimens, for (Group-A))
CB1&CB8(CB2&CB9)
(CB3&CB10(D
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Hysteresis Loop Envelope of Load Versus
Displacement, (Group-D),
(CB1,CB2,CB3,CB8,CB9 & CB10)
-8
-6
-4
-2
0
2
4
6
8
-80 -60 -40 -20 0 20 40 60 80
Displacement (mm)
Load(ton)
CB1(F.S.Reinf.)(col.30*30)
CB8(F.S.Reinf.)(col.20*20)
CB2(E.S.Reinf.)(col.30*30)
CB9(E.S.Reinf.)(col.20*20)
CB3(N.S.Reinf.)(col30*30)
CB10(N.S.Reinf.)(col.20*20)
Energy Dissipation Capacity for Different
Specimens, (Group-D).
0
200
400
600
800
1000
1200
1 3 5 7 9 11 13 15 17 19
Cycle No.
EnergyDissipation
(ton.mm)
CB1(F.S.Reinf.)(col.30*30)
CB8(F.S.Reinf.)(col.20*20)
CB2(E.S.Reinf.)(col.30*30)
CB9(E.S.Reinf.)(col.20*20)
CB3(N.S.Reinf)(col.30*30)
CB10(N.S.Reinf.)(col.20*20)280
Stiffness Degradation for Different
Specimens, ( Group-D)
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
1 3 5 7 9 11 13 15 17
Cycle No.
Stiffness
CB1(F.S.Reinf.)(col.30*30) CB8(F.S.Reinf.)(col.20*20)
CB2(E.S.Reinf.)(col.30*30) CB9(E.S.Reinf.)(col.20*20)
CB3(N.S.Reinf.)(col.30*30) CB10(N.S.Reinf.)(col.20*20)
(Comparison between Hysteresis Loop Envelope of Load Displacement, StiffnessDegradation, and Energy Dissipation Capacity for Different Specimens, for (Group-D))
IDARC
IDARC
Theoritical Hysteresis Loop Envelope
of Load VersusDisplacement,(CB10)(by
IDARC)
-8
-6
-4
-2
0
2
4
6
8
-100 -80 -60 -40 -20 0 20 40 60 80 100
Displacement (mm)
Load(tonS)
Theoritical
Experimental
Theoritical Vertical Load-Displacement
Hysteresis Loop,(CB10)(by IDARC).
-60
-40
-20
0
20
40
60
-80 -60 -40 -20 0 20 40 60 80
Disblacement(mm)
Load(tons)
3
2
5
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(Analytical Hysteresis Loop Envelope of Load Versus Displacement, andComparison between Experimental and Analytical Results).
(ANSYS)ANSYS10
(Finite Element Mesh , and Overall Load of Specimens).
(Comparison between Experimental and Analytical Results)
Ana./Exp.
Analytical
Results
Experimental
ResultsSpecimens
Pult (Ton)Pult (Ton)
0.803.2254.03ve(CB10)
Column
(20x20) 0.823.1253.81ve
(ANSYS) /AnalyticalAnalyticalSpecimens
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Analytical Load Versus Displacement
Hysteresis Loop(CB10) (by ANSYS).
-4
-3
-2
-1
0
1
2
3
4
-60 -40 -20 0 20 40 60
Displacement(mm)
Load(tons)
-5
-4
-3
-2
-1
0
1
2
3
4
5
-80 -60 -40 -20 0 20 40 60 80
Displacement(mm)
Load(tons)
Experimental
Theoritical
3
3
6
(Analytical Hysteresis Loop Envelope of Load Versus Displacement, and
Comparison between Experimental and Analytical Results).
(ANSYS)(IDARC)
(Plastic
Hingeslippage
Fusion Bonded Steel Bars
Epoxy Coated Steel Bars
( IDARC)
Results
(ANSYS)Results
(IDARC)
Pult (Ton)Pult (Ton)
0.563.2255.75ve(CB10)
Column
(20x20) 0.5563.1255.62ve
( Comparison between Analytical Results (ANSYS and IDARC))
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(ANSYS)
6. References:
1- ACI-ASCE Committee 352, "Recommendations for Design of Beam- ColumnJoints in Monolithic Reinforced Concrete Structures.", ACI Journal, Vol.82, No.3, May-June 1995
2- A. J. Kappos, "Dynamic Loading and Design of Structures" Published by SponPress , London, 2003.
3- ASTM (1989),"Standard Specification for Epoxy-Coated Reinforcing SteelBars,"(ASTM A 775M-89a) 1989 Annual Book for ASTM Standards, Vol. 1.04,
ASTM, Philadelphia , pp. 555-559.
4-
Belong, Z. and Yuzhou, C., "Behavior of Exterior Reinforced Concrete Beam-Column Joints Subjected to Bi-Directional Cyclic Loading" , ACI SP-123(3) : Design of
Beam-Column Joints for Seismic Resistance, Special Publication of the American
Concrete Institute Detroit, Michigan, 1991, pp. 69-96.
5- ECP-1995 "Egyptian Code of Practice for Reinforced Concrete Structure",Housing and Building Research Center, Egypt 2006.
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6- Park, Y. J., Ang, A.-S., and Wen, Y.K., "Seismic Damage Analysis and Damage-Limiting Design of R/C Building" Civil Engineering Studies, Technical Report No. SRS
516, University of Illinois, Urbana 1995.
7- Park, Y. J., Reinhorn A. M., Kunnath S. k., "IDARC: Inelastic Damage Analysisof Reinforced Concrete Frame-Shear-Wall Structures" Technical Report NCEER-87-
0008, State University of New York at Buffalo1998.
"Effect of Column Characteristic on Seismic Behaviorof Beam-Column Connection with Different
Types of Coated Steel Bars"
M. TALAT MOSTAFA1, SHADIA NAGA ELIBIARI
2,
AHMED MOHAMED FARAHAT3ANDHOSSAM EL-DIN HASSAN FOUAD AHMED ADBEL-
WAHID4
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1 Professor of Concrete Structures Faculty of Engineering, Cairo University.2
Professor of Concrete Structures National Center of Housing and Building Research.3
Professor of Concrete Structures Faculty of Engineering, Cairo University.
4Doctor in civil Engineering, Housing and Development Bank, E- mail
[email protected] :During the past few years the attention had increased to real estate
wealth due to not doing the needed maintenance to reserve the
hypothetical age of the structure .
One of the most effective factors on the age of the structure and its
safety is corrosion of reinforcing steel . Therefore, the is a need toresist this destructive factor. There are many factors to resist corrosion
of reinforcing steel but the economic way that is recommended to used
in codes but under special conditions which is covering the reinforcing
steel through epoxy-coated bars between it and the factors causing the
corrosion. Using the epoxy materials as a prevention between the
reinforcing steel and concrete affects connection and to reduce this
effect, the connection is increasing between them by mechanic
connection by increasing the length of the skewers. It was common
that before 1992 Earthquake , the lower-mid buildings highness are
designed based on bearing the vertical loads regardless the horizontal
loads. In the situation of Earthquake , cracks and collapses occur in
many buildings and many of these cracks occur according to defects inthe joints between the column and the beam whether design defects or
details defects , so its necessary to take the loads into consideration .
Keywords : Corrosion of reinforcing steel , Beam-Column Connection
, Seismic , Coated Steel Bars.
mailto:[email protected]:[email protected]