in-plane shear behavior of reinforced concrete elements with...
TRANSCRIPT
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공학석사 학위논문
In-Plane Shear Behavior of
Reinforced Concrete Elements with
High-Strength Materials
고강도 재료가 사용된
철근콘크리트 요소의 면내 전단 거동
2014년 2월
서울대학교 대학원
건설환경공학부 구조전공
배 광 민
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In-Plane Shear Behavior of
Reinforced Concrete Elements with
High-Strength Materials
지도 교수 조 재 열
이 논문을 공학석사 학위논문으로 제출함
2014 년 1 월
서울대학교 대학원
건설환경공학부 구조전공
배 광 민
배광민의 석사 학위논문을 인준함
2014 년 1 월
위 원 장 (인)
부위원장 (인)
위 원 (인)
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Abstract
In-Plane Shear Behavior of Reinforced Concrete Elements with
High-Strength Materials
Bae, Gwang-Min
Department of Civil and Environmental Engineering
The Graduate School
Seoul National University
This thesis presents the results of twelve reinforced concrete elements
subjected to shear and biaxial stresses. These elements were constructed by
one-third scale of real nuclear power plant wall elements. And the load
conditions were determined by considering earthquake and accidental inner
pressure when the nuclear power plant is overheated. Elements were loaded
until failure using University of Toronto’s Shell Element Tester. The concrete
compressive strength, steel yield strength and reinforcement ratio of APR
1400 that is current model of nuclear power plant in Korea were used for
reference element. And the high strength concrete, high yield strength steel
and decreased reinforcement ratio were used for other elements to compare
with the shear behavior of reference elements. On the other hand, in recent
years, design codes have incorporated compression field theory for the design
of reinforced concrete structures subjected to shear. Especially the Modified
Compression Field Theory has become the basis of the shear provisions in
CSA Standards, AASHTO LRFD, fib Model code and Eurocode 2. It is
expected that ASME, ACI 318 and ACI 349 design codes that commonly used
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in the design of nuclear power plant structures will implement Modified
Compression Field Theory based provisions in the near future. The ultimate
load was accurately predicted with a mean test to predicted ratio of 1.03 and a
coefficient of variation of 6.4 %. The shear strains at peak shear stress were
also accurately predicted with a mean test to predicted ratio of 1.04 and a
coefficient of variation of 13.5 %. The Modified Compression Field Theory
also well predicted the cracked shear stiffness of elements. These results show
the applicability of the Modified Compression Field Theory to shear design of
nuclear power plant wall. And the new tension stiffening equation for large
reinforced concrete elements is proposed based on the test results.
Keywords: Concrete Shear, High-Strength Materials, Nuclear Power
Plant, Modified Compression Field Theory, Tension Stiffening
Student Number: 2011-20982
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Contents
Chapter 1 Introduction........................................................... 1
1.1 General ................................................................................ 1
1.2 Modified Compression Field Theory .................................... 4
1.3 Objective and Scope............................................................. 9
Chapter 2 Experimental Program ........................................ 10
2.1 Test Variables ..................................................................... 10
2.2 Specimen Descriptions ....................................................... 16
2.3 Shell Element Tester .......................................................... 21
2.4 Instrumentation .................................................................. 24
Chapter 3 Experimental Results .......................................... 30
3.1 N420A Series ..................................................................... 32
3.2 N550B Series ..................................................................... 41
3.3 N550A Series ..................................................................... 50
3.4 H550B Series ..................................................................... 58
3.5 H550A Series ..................................................................... 66
Chapter 4 Observations and Analysis .................................. 74
4.1 Applicability of High-Strength Materials............................ 74
4.2 Applicability of Modified Compression Field Theory......... 79
4.3 Modification of Tension Stiffening Equation ...................... 88
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Chapter 5 Conclusion ........................................................ 124
References ......................................................................... 125
Abstract ............................................................................. 128
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List of Tables
Table 2.1 Reinforcement ratio of APR 1400 NPP wall ............................. 11
Table 2.2 Test variables ........................................................................... 12
Table 2.3 Instrumentation for data acquisition per each specimen ............. 24
Table 3.1 Summary of experimental results.............................................. 31
Table 4.1 Comparison of N420A-PS and N550B-PS ................................ 76
Table 4.2 Comparison of N420A-PS, N550B-PS and H550B-PS ............. 78
Table 4.3 Comparsion of observed and MCFT predicted values ............... 84
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List of Figures
Figure 1.1 Reinforcing bars in construction field of nuclear power plant ...... 1
Figure 1.2 RC element and NPP containment structure ................................ 2
Figure 1.3 Compression softening effect of concrete ................................... 4
Figure 1.4 Tension stiffening effect of concrete ........................................... 5
Figure 1.5 Secant stiffness in the direction of principal tension of concrete .. 5
Figure 1.6 Secant stiffness in the direction of principal compression of
concrete ..................................................................................... 6
Figure 1.7 Secant stiffness in the direction of reinforcement ........................ 6
Figure 2.1 RC element and NPP containment structure .............................. 10
Figure 2.2 Previous in-plane shear tets of RC elements.............................. 14
Figure 2.3 Large RC element specimen ..................................................... 16
Figure 2.4 A Series reinforcement mesh .................................................... 18
Figure 2.5 B Series reinforcement mesh .................................................... 19
Figure 2.6 Shell Element Tester ................................................................. 21
Figure 2.7 The principle of Shell Element Tester ....................................... 22
Figure 2.8 LVDTs locations....................................................................... 25
Figure 2.9 LEDs locations ......................................................................... 27
Figure 2.10 Real pictures of LVDTs and LEDs ............................................ 28
Figure 2.11 ERSGs locations ...................................................................... 29
Figure 3.1 Experimental results of N420A Series ...................................... 40
Figure 3.2 Experimental results of N550B Series ...................................... 49
Figure 3.3 Experimental results of N550A Series ...................................... 57
Figure 3.4 Experimental results of H550B Series ...................................... 65
Figure 3.5 Experimental results of H550A Series ...................................... 73
Figure 4.1 Shear stress – shear strain of N420A and N550B Series ............ 75
Figure 4.2 Shear stress – maximum crack width of N420A and N550B
Series ....................................................................................... 77
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Figure 4.3 Shear stress – average crack width of N420A and N550B
Series ....................................................................................... 77
Figure 4.4 Shear stress – shear strain of N420A-PS, N550B-PS and H550B-
PS ............................................................................................ 78
Figure 4.5 Comparison of predicted and observed shear stress – shear
strain ........................................................................................ 83
Figure 4.7 Tension stiffening denominator versus bond parameter ............. 88
Figure 4.8 Tension stiffening denominator of individual Toronto Large
Elements experiments versus bond parameter ........................... 89
Figure 4.9 Comparison of predicted and observed principal tensile stress –
principal tensile strain with Bentz tension stiffening equation ... 90
Figure 4.10 Comparison of test, Bentz, and modified Bentz with A = 8.0 in
principal tensile behavior........................................................ 101
Figure 4.11 Comparison of test, Bentz, and Eq. (4.4) with best coefficient A
for each speciemen ................................................................. 112
Figure 4.12 Tension stiffening denominator versus bond parameter by new
equation ................................................................................. 113
Figure 4.13 Comparison of test, Bentz, and proposed equation in this
study ...................................................................................... 123
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Chapter 1 Introduction
1.1 General
Design codes for nuclear power plant such as ASME Sec.III Div. 2, ACI 349,
and ACI 318 restrict the yield strength of reinforcing bars to 420 MPa. For
these reasons, excessive amount of reinforcing bars are used for construction
of nuclear power plant (NPP) as shown in Fig. 1.1. Due to using of excessive
amount of reinforcing bars, many problems are occurred such as poor
constructability, careful quality control of concrete, and uneconomical design.
To solve these problems, high-strength materials are required for nuclear
power plant structures.
Fig. 1.1 Reinforcing bars in construction field of nuclear power plant
But, due to high levels of conservatism and cautiousness for design and
construction of nuclear power plant structure, a lot of researches are required
to apply high-strength materials such as beam shear and torsion test, headed
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bar test, wall test, column shear test, reinforcing bar development test, and
crack behavior test. This study focused on the shear behavior evaluation of
nuclear power plant containment wall that is applied with high-strength rebars
and high-strength concrete.
To investigate the shear behavior of nuclear power plant containment
structures, in-plane shear tests of reinforced concrete element from the shear
critical region of nuclear power plant wall as shown in Fig. 1.2 were
conducted. Structures like nuclear power plant containment can be considered
as an assemblage of reinforced concrete elements. And the shear behavior of a
reinforced concrete element is the basis for the prediction of shear behavior of
whole structures by finite element analysis.
Fig. 1.2 RC element and NPP containment structure
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On the other hand, in recent years, design codes have implemented
compression field approaches for the design of reinforced concrete structures
subjected to shear. In particular, the Modified Compression Field Theory
(MCFT) has become the basis of the shear design such as CSA Standard,
AASHTO LRFD, fib Model Code, and Eurocode 2. It is expected that codes
used for the design of nuclear power plant structures, such as ASME, ACI 349,
and ACI 318 will adopt MCFT based shear design in the near future.
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1.2 Modified Compression Field Theory
MCFT regards the cracked concrete as an orthotropic material by smeared
cracking. In smeared cracking model, cracked concrete is assumed to remain a
continuum. Cracks are assumed an average deformation spread out over an
area. And MCFT uses rotating cracking model. In rotating cracking model, the
crack direction rotates as loading conditions change. New cracking and crack
extensions result in a change in direction of total crack condition.
MCFT considered the compression softening effect of concrete when
tension stresses existed in the direction of principal tension as shown in Fig.
1.3.
Fig. 1.3 Compression softening effect of concrete
From a lot of test data, cracked concrete in compression has a reduced
strength and stiffness compared to a uniaxially compressed concrete. This
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behavior is known as the compression softening effect.
MCFT also considered the tension stiffening effect of concrete. From a
lot of test data, concrete between cracks resist tensile stresses because of bond
effects with the reinforcement as shown in Fig. 1.4.
Fig. 1.4 Tension stiffening effect of concrete
Fig. 1.5 Secant stiffness in the direction of principal tension of concrete
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Fig. 1.6 Secant stiffness in the direction of principal compression of concrete
Fig. 1.7 Secant stiffness in the direction of reinforcement
MCFT uses secant stiffness of each material in shear analysis of
reinforced concrete elements as shown in Fig. 1.5 to 1.7. Then, shear secant
stiffness of concrete is calculated like Eq. (1.1) because MCFT regards
concrete as an orthotropic material.
1 2
1 2
c cc
c c
E EG
E E
×=
+ (1.1)
From secant stiffness in the direction of principal tension, principal
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compression, and shear secant stiffness of concrete, material secant stiffness
of concrete like Eq. (1.2) can be constructed.
1
2
0 0
[ ] 0 0
0 0
c
c c
c
E
D E
G
é ùê ú¢ = ê úê úë û
(1.2)
In the same manner, material secant stiffness of reinforcement can be
constructed like Eq. (1.3).
0 0
[ ] 0 0 0
0 0 0
si si
si
E
D
ré ùê ú¢ = ê úê úë û
(1.3)
By using of transpose matrix like Eq. (1.4) where y = the angle of the
direction of principal tension of concrete for transpose matrix for concrete
and y = the angle of the direction of each reinforcement from x axis for
transpose matrix for reinforcement, secant stiffness matrix of reinforced
concrete element like Eq. (1.5) can be constructed.
2 2
2 2
2 2
cos sin cos sin
[ ] sin cos cos sin
2cos sin 2cos sin cos sin
T
y y y y
y y y y
y y y y y y
é ùê ú
= -ê úê ú- -ë û
(1.4)
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[ ] [ ] [ ] [ ]
[ ] [ ] [ ] [ ]
[ ] [ ] [ ]
Tc c c c
Tsi si si si
c si
D T D T
D T D T
D D D
¢=
¢=
= +å
(1.5)
From the secant stiffness matrix of reinforced concrete element, in-plane
strains of reinforced concrete element can be achieved under any in-plane
stresses like Eq. (1.6) by typically 20 to 30 iterations.
1{ } [ ]
x x
y y
xy xy
f
D f
v
e
e e
g
-
ì ü ì üï ï ï ï
= =í ý í ýï ï ï ïî þ î þ
(1.6)
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1.3 Objective and Scope
The objective of this thesis is investigation of the influence of 550 MPa high
design yield strength rebars on the shear behavior of reinforced concrete
nuclear power plant wall elements subjected to in-plane shear and axial
stresses. And an investigation of the applicability of 70 MPa high design
compressive strength concrete with 550 MPa reinforcing bars in the nuclear
power plant design will be discussed.
Also, an investigation of the applicability of Modified Compression Field
Theory for the shear behavior of reinforced concrete elements with high-
strength materials will be discussed and modification of MCFT formulation
will be conducted if needed.
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Chapter 2 Experimental Program
2.1 Test Variables
Fig. 2.1 RC element and NPP containment structure
When a seismic event occurred to NPP containment structure, huge shear
stress will be induced near the base of the NPP containment wall that is shear
critical region. In the event that a nuclear reactor overheats, large pressures
can build inside the containment structure inducing biaxial tension into the
RC element of NPP containment wall. And also the existence of biaxial
compression is common since large amounts of prestressing are often used in
both the vertical and horizontal direction. So the test specimens are
constructed by considering the RC elements of NPP low level wall which
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shear and biaxial stresses are induced when a seismic event occurred as shown
in Fig 2.1.
RC element test specimens’ reinforcement ratio is decided by that of APR
1400 NPP containment low level wall which is shear critical region. APR
1400 is current NPP model of Shin-Kori NPP 3 and 4 units that are being
constructed in Korea. The vertical and horizontal reinforcement ratio of APR
1400 NPP wall is shown in Table 2.1.
Table 2.1 Reinforcement ratio of APR 1400 NPP wall
Location Reinforcements
Reinforcement ratio
(%)
Vertical Horizontal Vertical Horizontal
Dome Inside #14 @0.9˚ #14 @0.9˚
0.56 0.56 Outside #11 @0.9˚ #11 @0.9˚
Wall (Spring line)
Inside #14 & #18 @
0.9˚
#11 & #18 @
12" 1.84 1.93
Outside #14 & #18 @
0.9˚
#11 & #18 @
12"
Wall
(Mid. level)
Inside #14 @0.9˚ #18 @12" 0.66 1.39
Outside #14 @0.9˚ #18 @12"
Wall
(Low level)
Inside 2-#18 & #14
@0.9˚ #18 @12"
2.10 1.39
Outside #18 @0.9˚ #18 @12"
Vertically 2.10 % and horizontally 1.39 % reinforcement ratio of APR
1400 NPP low level wall are considered to RC element test specimens.
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Table 2.2 Test variables
Specimens fn / v fc'
(MPa)
fyx
(MPa)
fyy
(MPa)
ρx
(%)
ρy
(%)
ρxfyx
(MPa)
ρyfyy
(MPa) Remarks
N420A-PS 0 35.2
448 477 2.09 1.35 9.36 6.44 Reference specimens N420A-SBT +0.4 35.2
N420A-SBC -0.4 35.2
N550B-PS 0 35.2
631 631 1.56 1.04 9.84 6.56 Increased fy
with ρfy maintained N550B-SBT +0.4 39.0
N550B-SBC -0.4 39.0
N550A-PS 0 39.0 631 653 2.09 1.35 13.19 8.82
Increased fy
with the same ρ N550A-SBT +0.4 39.0
H550B-PS 0 55.8 631 631 1.56 1.04 9.84 6.56
Increased fy and fc'
with ρfy maintained H550B-SBC -0.3 55.8
H550A-PS 0 55.8 631 653 2.09 1.35 13.19 8.82
Increased fy and fc'
with the same ρ H550A-SBC -0.2 55.8
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Considering the APR 1400 NPP low level wall reinforcement ratio and
the loading conditions of RC element of NPP wall when seismic event occur,
twelve RC elements shown in Table. 2.2 were constructed. Considering size
effect of concrete, 1626 × 1626 mm square and 355 mm thick large RC
elements were constructed. 355 mm thick is almost one third scale of APR
1400 NPP wall thickness 1.2 m.
The major test variables for the in-plane shear tests of RC elements are
concrete compressive strength, rebar yield strength, reinforcement ratio, and
loading conditions. For the concrete compressive strength, 42 MPa and 70
MPa concrete design compressive strength were used. 42 MPa concrete
strength is currently being used in APR 1400 NPP structures, and 70 MPa
concrete strength was used to represent high-strength concrete. For the rebar
yield strength, 420 MPa and 550 MPa design yield strength were used. 420
MPa yield strength is currently being used in NPP structure and 550 MPa
yield strength is the goal of this study. Longitudinally (x) 2.09 % and
transversely (y) 1.35 % reinforcement ratio was chosen to represent the APR
1400 NPP’s vertically 2.10 % and horizontally 1.39 % reinforcement ratio
respectively. And longitudinally 1.56 % and transversely 1.04 %
reinforcement ratio that are reduced by 420 / 550 were used. 420 / 550 is the
ratio of rebar yield strength to represent the applying high-strength rebar and
reduced reinforcement ratio. For the loading conditions, pure shear, shear and
biaxial tension, and shear and biaxial compression are used.
Specimens labelled ‘N’ used 42 MPa normal design compressive
concrete strength, while specimens labelled ‘H’ used 70 MPa high design
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compressive strength concrete. The ‘420’ label indicates that 420 MPa normal
design yield strength rebar, while the ‘550’ label indicates that 550 MPa high
design yield strength rebar. The ‘A’ label indicates that the specimens were
constructed with 2.09 % reinforcement ratio in the longitudinal direction and
1.35 % reinforcement ratio in the transverse direction to represent the
reinforcement ratio of APR 1400 NPP low level wall. The ‘B’ label indicates
that the specimens were constructed with 1.56 % reinforcement ratio in the
longitudinal direction and 1.04 % reinforcement ratio in the transverse
direction. The label ‘PS’ indicates pure shear, the label ‘SBT’ indicates shear
and biaxial tension, and the label ‘SBC’ indicates shear and biaxial
compression. The specimens were divided into five series: N420A, N550B,
N550A, H550B, and H550A.
Fig. 2.2 Previous in-plane shear tests of RC elements
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Selected test variables are not duplicated to those variables tested
previously. 890 × 890 mm square and 70 mm thick small RC elements and
1626 × 1626 mm square and 216 to 310 mm thick large RC elements were
tested with certain concrete compressive strength and rebar yield strength as
shown in Fig. 2.2. Especially, large RC elements with high-strength rebar in-
plane shear tests were not performed so far.
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2.2 Specimen Descriptions
To perform in-plane shear test of RC elements representing one third scale of
NPP low level wall, 1626 × 1626 × 355 mm large RC element specimens like
Fig. 2.3 were constructed.
(mm)
Fig. 2.3 Large RC element specimen
All specimens have same dimensions and two orthogonally welded
reinforcement meshes were embedded in the concrete for each specimen. And
twenty anchor blocks are required for each reinforcement mesh.
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(a) A Series reinforcement mesh of bottom layer
(b) A Series reinforcement mesh of top layer
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(c) A Series reinforcement drawing
Fig. 2.4 A Series reinforcement mesh
(a) B Series reinforcement mesh of bottom layer
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(b) B Series reinforcement mesh of top layer
(c) B Series reinforcement drawing
Fig. 2.5 B Series reinforcement mesh
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Twenty anchor blocks were placed in the edge of reinforcement mesh and
rebars were welded to the anchor blocks. For A Series specimens, 2 layers of
#5 rebars were reinforced to the longitudinal direction spaced at 54 mm, and 2
layers of #4 rebars were reinforced to the transverse direction spaced at 54
mm as shown in Fig. 2.4. For B Series specimens, 2 layers of #5 rebars were
reinforced to the both longitudinal direction spaced at 72 mm, and 2 layers of
#5 rebars were reinforced to the transverse direction spaced at 108 mm as
shown in Fig. 2.5.
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2.3 Shell Element Tester
To apply uniform stress to the RC element specimens, the Shell Element
Tester at the University of Toronto, shown in Fig. 2.6, was used. The Shell
Element Tester is capable of loading 1626 × 1626 mm square and 200 to 400
mm thick large scale reinforced concrete elements.
Fig. 2.6 Shell Element Tester
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( ) / 2h vv f f= + , ( ) / 2n h vf f f= -
Fig. 2.7 The principle of Shell Element Tester
The reinforcement in a specimen was oriented at 45 degrees to the
direction of applied principal stresses, so the elements are subjected to in-
plane shear and biaxial stresses to the direction of reinforcement (x, y
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directions). By adjusting the magnitude of horizontal and vertical stresses, a
variety of normal stress to shear stress ratio can be achieved as shown in Fig.
2.7.
Furthermore, the tester can apply any combination of the eight shell
stress resultants that are three in-plane forces, three moments and two out-of-
plane shear forces. The tester consists of forty in-plane double acting
hydraulic jacks and twenty out-of-plane double acting hydraulic jacks. The in
–plane jacks are used to apply in-plane forces and are arranged in two layers
to apply bending moments. The out-of-plane jacks are used to apply torsional
moment and out-of-plane shear. A more detailed description is presented in
the theses of Khalifa (1986) and Kirschner (1986).
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2.4 Instrumentation
To obtain strain information of RC element, 12 linearly variable differential
transformers (LVDTs), 35 light emitting diodes (LEDs), and 16 electrical
resistance strain gauges (ERSGs) were installed to each specimen as shown
in Table 2.3.
Table 2.3 Instrumentation for data acquisition per each specimen
Type Description Amount Interval Purpose
LVDT
Linearly variable
differential transformers
0.001 mm resolution
12 EA 10 Hz Observe the strains
of elements
LED
Light emitting diode
three dimensional
position tracking targets
35 EA 10 Hz
Observe the strains
of elements and
measure several
crack widths
ERSG Electrical resistance
strain gauges 16 EA 10 Hz
Observe the strains
of longitudinal and
transverse rebars
LVDTs were installed both on northface and southface of the specimens
as shown in Fig. 2.8. On each face of the specimen, two LVDTs were installed
in the horizontal direction, two in the vertical direction, one in the longitudinal
(x) direction, and one in the transverse (y) direction. ‘N’ indicates northface,
‘S’ indicates southface, ‘H’ indicates horizontal, ‘V’ indicates vertical, ‘D’
indicated diagonal, ‘T’ indicates top, ‘B’ indicates bottom, ‘E’ indicates east,
and ‘W’ indicates west.
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(a) 6 LVDTs on northface
(b) 6 LVDTs on southface
Fig. 2.8 LVDTs locations
35 LEDs were installed only on the southface per each specimen. 25
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LEDs were arranged in a grid of 5 × 5 spaced 300 mm apart. After cracking,
the remaining 10 LEDs were attached across cracks in 5 pairs as shown in Fig.
2.9. The LVDTs and the grid of 25 LEDs were used to obtain the average
strains of each specimen and the 5 pairs of LEDs were used to continuously
measure several crack widths. 16 ERSGs were attached to selected rebars of
each specimen. For each top and bottom reinforcement layers, 4 ERSGs were
attached to longitudinal rebars and 4 ERSGs were attached to transverse
rebars as shown in Fig. 2.11. After first cracking and at the key intervals, the
loading was halted and the loads were reduced by about 10 % so that cracks
could be safely marked and measured with crack sheets. During these load
stages photographs were also taken.
(a) A grid of 25 LEDs on southface
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(b) 5 pairs of LEDs on southface beside several cracks
Fig. 2.9 LEDs locations
(a) 6 LVDTs on northface
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(b) 6 LVDTs and 35 LEDs on southface
Fig. 2.10 Real pictures of LVDTs and LEDs
(a) ERSGs on A Series specimen’s top and bottom reinforcement layers
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(b) ERSGs on B Series specimen’s top and bottom reinforcement layers
Fig. 2.11 ERSGs locations
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Chapter 3 Experimental Results
All RC element specimens were tested by increasing the shear stress in
increments of 0.1 MPa. The biaxial stresses were increased in certain
proportion to the shear stress for each specimen. Load cells mounted at the
base of each hydraulic actuator were used to determine the applied stress
magnitude. LVDTs, LEDs, and ERSGs were continuously measured strains
during for each test at 10 Hz interval. Specimen’s northface were recorded by
digital camcorder and its photographs were continuously taken during the
tests. At four to six load stages, including right after first cracking, the loading
was halted and the loads were reduced by about 10 %. During load stages,
cracks were marked and measured, and detailed photographs of specimen
were taken. Although the tests were intended to be monotonic, some
specimens were unloaded and the out-of-plane alignment was adjusted to
minimize second order effects. Some specimens also were unloaded
intentionally after the peak load to capture the post peak behavior.
The specimens were divided into five series by concrete compressive
strength, rebar yield strength, and reinforcement ratio. The five series of tests
will be called as N420A, N550B, N550A, H550B, and H550A Series. For
each series of tests, two to three RC elements were tested, one in pure shear
(PS) and the remainder with different combinations of shear and biaxial
tension (SBT) or shear and biaxial compression (SBC). Table 3.1 summarizes
the experimental results of the twelve specimens.
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Table 3.1 Summary of experimental results
Specimens fn / v vcr
(MPa)
vu
(MPa)
fnu
(MPa)
Strains at vu (×10-3) fc1
(MPa)
fc2
(MPa)
θuε
(Deg.)
θuσ
(Deg.) εx εy γxy ε1 ε2
N420A-PS 0 2.10 7.70 0 2.58 5.43 10.95 9.66 -1.65 -0.06 -15.7 37.7 39.7
N420A-SBT +0.4 1.60 5.87 2.35 3.28 13.90 17.34 18.75 -1.58 0.37 -11.6 29.3 38.0
N420A-SBC -0.4 3.07 9.56 -3.82 1.68 2.42 7.09 5.61 -1.51 -0.58 -20.1 42.0 44.2
N550B-PS 0 2.01 7.68 0 2.64 4.30 9.64 8.36 -1.42 -0.15 -15.1 40.1 41.9
N550B-SBT +0.4 1.29 5.97 2.39 3.61 15.21 21.65 21.69 -2.87 -0.10 -12.0 30.9 37.3
N550B-SBC -0.4 2.78 10.47 -4.19 2.29 3.04 8.26 6.81 -1.48 0.32 -21.4 42.4 43.9
N550A-PS 0 1.88 9.64 0 2.60 4.21 9.98 8.46 -1.65 0.25 -19.5 40.4 42.0
N550A-SBT +0.4 1.39 6.93 2.77 2.62 4.57 8.29 7.85 -0.66 -0.44 -14.1 38.4 40.6
H550B-PS 0 1.29 8.08 0 3.85 10.86 17.94 16.99 -2.28 -0.13 -16.4 34.4 39.3
H550B-SBC -0.3 1.39 10.48 -3.14 3.61 5.83 12.56 11.10 -1.66 -0.58 -22.0 40.0 40.6
H550A-PS 0 1.58 9.84 0 3.03 6.08 11.43 10.47 -1.36 0.04 -20.8 37.6 39.5
H550A-SBC -0.2 1.59 11.27 -2.25 3.09 4.26 10.16 8.79 -1.44 -0.74 -24.6 41.7 39.8
-
32
3.1 N420A Series
N420A Series are reference specimens which are representative of APR 1400
nuclear power plant’s low level wall element. 42 MPa design compressive
strength concrete and 420 MPa design yield strength rebar were used to
construct N420A Series specimens. The actual concrete strength is 35.2 MPa
and the actual rebar yield strength for longitudinal (x) direction is 448 MPa
and for transverse (y) direction is 477 MPa. #5 rebar of ASTM A615 is used
for longitudinal direction spaced at 54 mm, #4 rebar of ASTM A615 is used
for transverse direction spaced at 54 mm. The reinforcement ratio is almost
same with that of APR 1400 nuclear power plant’s low level wall which is
shear critical region.
Fig. 3.1 shows the shear stress – shear strain, principal concrete
compressive stress – principal compressive strain, principal concrete tensile
stress – principal tensile strain, shear stress – shear strain by LVDTs, shear
stress – shear strain by LEDs, shear stress – longitudinal strain, shear stress –
transverse strain, shear stress – maximum crack width, and shear stress –
average crack width graphs of N420A Series. The shear strain obtained by
LVDTs and LEDs are coincided each other. Especially prior to failure, the
LVDTs and LEDs measurements showed excellent agreement. The LEDs data
of N420A-SBC was lost.
-
33
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A Series
ρx = 2.09% fyx = 448 MPa
ρy = 1.35% fyy = 477 MPa
sx = 54 mm sy = 54 mm
fc' = 35.2 MPa ag = 20 mm
N420A-SBC: fn/v = -0.4
N420A-SBT: fn/v = +0.4
N420A-PS: fn/v = 0
(a) Shear stress – shear strain of N420A Series
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A Series
ρx = 2.09% fyx = 448 MPa
ρy = 1.35% fyy = 477 MPa
sx = 54 mm sy = 54 mm
fc' = 35.2 MPa ag = 20 mm
N420A-SBC: fn/v = -0.4
N420A-SBT: fn/v = +0.4
N420A-PS: fn/v = 0
(b) Shear stress – shear strain of N420A Series with unloading part deleted
-
34
(c) Principal concrete compressive stress – principal compressive strain of
N420A Series
(d) Principal concrete tensile stress – principal tensile strain of N420A-PS
-
35
(e) Principal concrete tensile stress – principal tensile strain of N420A-SBT
(f) Principal concrete tensile stress – principal tensile strain of N420A-SBC
-
36
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-PS
Average
Northface
Southface
(g) Shear stress – shear strain by LVDTs of N420A-PS
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-SBT
Average
Northface
Southface
(h) Shear stress – shear strain by LVDTs of N420A-SBT
-
37
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-SBC
Average
Northface
Southface
(i) Shear stress – shear strain by LVDTs of N420A-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-PS
LVDT
LED
(j) Shear stress – shear strain by LVDTs and LEDs of N420A-PS
-
38
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-SBT
LVDT
LED
(k) Shear stress – shear strain by LVDTs and LEDs of N420A-SBT
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N420A-SBC
LVDT
LED
(l) Shear stress – shear strain by LVDTs and LEDs of N420A-SBC (The LEDs
data of N420A-SBC was lost)
-
39
(m) Shear stress – longitudinal strain of N420A Series
0 4 8 12 16
Transverse Strain, mm/m
0
2
4
6
8
10
12
N420A SeriesLVDT
ERSG Average
ERSG Top
ERSG Bottom
N420A-PS: fn/v = 0
N420A-SBT: fn/v = +0.4
N420A-SBC: fn/v = -0.4
(n) Shear stress – transverse strain of N420A Series
-
40
(o) Shear stress – maximum crack width of N420A Series
(p) Shear stress – average crack width of N420A Series
Fig. 3.1 Experimental results of N420A Series
-
41
3.2 N550B Series
N550B Series specimens used 550 MPa high design yield strength rebars and
reduced reinforcement ratio according to 420 / 550. So, N550B Series
specimens’ ρfy values are similar with those of N420A Series specimens.
N550B Series specimens are constructed to research the behavior when high-
strength rebar used and reinforcement ratio decreased according to inverse
ratio of increased rebar yield strength. 42 MPa design compressive strength
concrete and 550 MPa design yield strength rebar were used to construct
N550B Series specimens. The actual concrete strength is 39.0 MPa except
N550B-PS and the actual rebar yield strength for longitudinal (x) direction is
631 MPa and for transverse (y) direction is 631 MPa. The actual concrete
strength of N550B-PS is 35.2 MPa that is same with N420A Series. N420A
Series and N550B-PS used same concrete batch. N550B-SBT, N550B-SBC
and N550A Series used same concrete batch. #5 rebar of ASTM A615 is used
for longitudinal direction spaced at 72 mm, #5 rebar of ASTM A615 is used
for transverse direction spaced at 108 mm. The reinforcement ratio is
decreased by 420 / 550 ratio than N420A Series specimens.
Fig. 3.2 shows the shear stress – shear strain, principal concrete
compressive stress – principal compressive strain, principal concrete tensile
stress – principal tensile strain, shear stress – shear strain by LVDTs, shear
stress – shear strain by LEDs, shear stress – longitudinal strain, shear stress –
transverse strain, shear stress – maximum crack width, and shear stress –
average crack width graphs of N550B Series.
-
42
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B Series
ρx = 1.56 % fyx = 631 MPa
ρy = 1.04 % fyy = 631 MPa
sx = 72 mm sy = 108 mm
fc' = 39.0 MPa ag = 20 mm
N550B-PS: fc' = 35.2 MPa
N550B-PS: fn/v = 0
N550B-SBT: fn/v = +0.4
N550B-SBC: fn/v = -0.4
(a) Shear stress – shear strain of N550B Series
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B Series
ρx = 1.56 % fyx = 631 MPa
ρy = 1.04 % fyy = 631 MPa
sx = 72 mm sy = 108 mm
fc' = 39.0 MPa ag = 20 mm
N550B-PS: fc' = 35.2 MPa
N550B-PS: fn/v = 0
N550B-SBT: fn/v = +0.4
N550B-SBC: fn/v = -0.4
(b) Shear stress – shear strain of N550B Series with unloading part deleted
-
43
(c) Principal concrete compressive stress – principal compressive strain of
N550B Series
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-PS
(d) Principal concrete tensile stress – principal tensile strain of N550B-PS
-
44
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-SBT
(e) Principal concrete tensile stress – principal tensile strain of N550B-SBT
(f) Principal concrete tensile stress – principal tensile strain of N550B-SBC
-
45
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-PS
Average
Northface
Southface
(g) Shear stress – shear strain by LVDTs of N550B-PS
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-SBT
Average
Northface
Southface
(h) Shear stress – shear strain by LVDTs of N550B-SBT
-
46
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-SBC
Average
Northface
Southface
(i) Shear stress – shear strain by LVDTs of N550B-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-PS
LVDT
LED
(j) Shear stress – shear strain by LVDTs and LEDs of N550B-PS
-
47
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-SBT
LVDT
LED
(k) Shear stress – shear strain by LVDTs and LEDs of N550B-SBT
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550B-SBC
LVDT
LED
(l) Shear stress – shear strain by LVDTs and LEDs of N550B-SBC
-
48
(m) Shear stress – longitudinal strain of N550B Series
0 4 8 12 16
Transverse Strain, mm/m
0
2
4
6
8
10
12
N550B SeriesLVDT
ERSG Average
ERSG Top
ERSG Bottom
N550B-PS: fn/v = 0
N550B-SBT: fn/v = +0.4
N550B-SBC: fn/v = -0.4
(n) Shear stress – transverse strain of N550B Series
-
49
(o) Shear stress – maximum crack width of N550B Series
(p) Shear stress – average crack width of N550B Series
Fig. 3.2 Experimental results of N550B Series
-
50
3.3 N550A Series
N550A Series specimens used 550 MPa high design yield strength rebars and
same reinforcement ratio with N420A Series. N550A Series specimens are
constructed to research the behavior when high-strength rebar used with same
reinforcement ratio of current APR 1400 nuclear power plant wall. 42 MPa
design compressive strength concrete and 550 MPa design yield strength rebar
were used to construct N550A Series specimens. The actual concrete strength
is 39.0 MPa and the actual rebar yield strength for longitudinal (x) direction is
631 MPa and for transverse (y) direction is 653 MPa. N550B-SBT, N550B-
SBC and N550A Series used same concrete batch. #5 rebar of ASTM A615 is
used for longitudinal direction spaced at 54 mm, #4 rebar of ASTM A615 is
used for transverse direction spaced at 54 mm. The reinforcement ratio is
same with N420A Series specimens.
Fig. 3.3 shows the shear stress – shear strain, principal concrete
compressive stress – principal compressive strain, principal concrete tensile
stress – principal tensile strain, shear stress – shear strain by LVDTs, shear
stress – shear strain by LEDs, shear stress – longitudinal strain, shear stress –
transverse strain, shear stress – maximum crack width, and shear stress –
average crack width graphs of N550A Series. N550A-SBT specimen suffered
from edge failure.
-
51
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A Series
ρx = 2.09 % fyx = 631 MPa
ρy = 1.35 % fyy = 653 MPa
sx = 54 mm sy = 54 mm
fc' = 39.0 MPa ag = 20 mm
N550A-PS: fn/v = 0
N550A-SBT: fn/v = +0.4
edge failure
(a) Shear stress – shear strain of N550A Series
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A Series
ρx = 2.09 % fyx = 631 MPa
ρy = 1.35 % fyy = 653 MPa
sx = 54 mm sy = 54 mm
fc' = 39.0 MPa ag = 20 mm
N550A-PS: fn/v = 0
N550A-SBT: fn/v = +0.4
edge failure
(b) Shear stress – shear strain of N550A Series with unloading part deleted
-
52
(c) Principal concrete compressive stress – principal compressive strain of
N550A-Series
(d) Principal concrete tensile stress – principal tensile strain of N550A-PS
-
53
(e) Principal concrete tensile stress – principal tensile strain of N550A-SBT
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A-PS
Average
Northface
Southface
(f) Shear stress – shear strain by LVDTs of N550A-PS
-
54
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A-SBT
Average
Northface
Southface
edge failure
(g) Shear stress – shear strain by LVDTs of N550A-SBT
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A-PS
LVDT
LED
(h) Shear stress – shear strain by LVDTs and LEDs of N550A-PS
-
55
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12N550A-SBT
LVDT
LED
(i) Shear stress – shear strain by LVDTs and LEDs of N550A-SBT
(j) Shear stress – longitudinal strain of N550A Series
-
56
0 4 8 12 16
Transverse Strain, mm/m
0
2
4
6
8
10
12
N550A SeriesLVDT
ERSG Average
ERSG Top
ERSG Bottom
N550A-PS: fn/v = 0
N550A-SBT: fn/v = +0.4
(k) Shear stress – transverse strain of N550A Series
(l) Shear stress – maximum crack width of N550A Series
-
57
(m) Shear stress – average crack width of N550A Series
Fig. 3.3 Experimental results of N550A Series
-
58
3.4 H550B Series
H550B Series specimens used 550 MPa high design yield strength rebars and
70 MPa high design compressive strength concrete with 420 / 550 decreased
reinforcement ratio to N420A Series. H550B Series specimens are constructed
to research the behavior when high-strength rebar and high-strength concrete
used with decreased reinforcement ratio. The actual concrete strength is 55.8
MPa and the actual rebar yield strength for longitudinal (x) direction is 631
MPa and for transverse (y) direction is 631 MPa. H550B and H550A Series
used same concrete batch. #5 rebar of ASTM A615 is used for longitudinal
direction spaced at 72 mm, #5 rebar of ASTM A615 is used for transverse
direction spaced at 108 mm. The reinforcement ratio is decreased by 420 / 550
to those of N420A Series specimens.
Fig. 3.4 shows the shear stress – shear strain, principal concrete
compressive stress – principal compressive strain, principal concrete tensile
stress – principal tensile strain, shear stress – shear strain by LVDTs, shear
stress – shear strain by LEDs, shear stress – longitudinal strain, shear stress –
transverse strain, shear stress – maximum crack width, and shear stress –
average crack width graphs of H550B Series.
-
59
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B Series
ρx = 1.56 % fyx = 631 MPa
ρy = 1.04 % fyy = 631 MPa
sx = 72 mm sy = 108 mm
fc' = 55.8 MPa ag = 20 mm
H550B-PS: fn/v = 0
H550B-SBC: fn/v = -0.3
(a) Shear stress – shear strain of H550B Series
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B Series
ρx = 1.56 % fyx = 631 MPa
ρy = 1.04 % fyy = 631 MPa
sx = 72 mm sy = 108 mm
fc' = 55.8 MPa ag = 20 mm
H550B-PS: fn/v = 0
H550B-SBC: fn/v = -0.3
(b) Shear stress – shear strain of H550B Series with unloading part deleted
-
60
(c) Principal concrete compressive stress – principal compressive strain of
H550B Series
(d) Principal concrete tensile stress – principal tensile strain of H550B-PS
-
61
(e) Principal concrete tensile stress – principal tensile strain of H550B-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B-PS
Average
Northface
Southface
(f) Shear stress – shear strain by LVDTs of H550B-PS
-
62
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B-SBC
Average
Northface
Southface
(g) Shear stress – shear strain by LVDTs of H550B-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B-PS
LVDT
LED
(h) Shear stress – shear strain by LVDTs and LEDs of H550B-PS
-
63
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550B-SBC
LVDT
LED
(i) Shear stress – shear strain by LVDTs and LEDs of H550B-SBC
(j) Shear stress – longitudinal strain of H550B Series
-
64
0 4 8 12 16
Transverse Strain, mm/m
0
2
4
6
8
10
12
H550B SeriesLVDT
ERSG Average
ERSG Top
ERSG Bottom
H550B-PS: fn/v = 0
H550B-SBC: fn/v = -0.4
(k) Shear stress – transverse strain of H550B Series
(l) Shear stress – maximum crack width of H550B Series
-
65
(m) Shear stress – average crack width of H550B Series
Fig. 3.4 Experimental results of H550B Series
-
66
3.5 H550A Series
H550A Series specimens used 550 MPa high design yield strength rebars and
70 MPa high design compressive strength concrete with same reinforcement
ratio of N420A Series. H550A Series specimens are constructed to research
the behavior when high-strength rebar and high-strength concrete used with
same reinforcement ratio with APR 1400 nuclear power plant wall. The actual
concrete strength is 55.8 MPa and the actual rebar yield strength for
longitudinal (x) direction is 631 MPa and for transverse (y) direction is 653
MPa. H550B and H550A Series used same concrete batch. #5 rebar of ASTM
A615 is used for longitudinal direction spaced at 54 mm, #4 rebar of ASTM
A615 is used for transverse direction spaced at 54 mm. The reinforcement
ratio is same with N420A Series specimens.
Fig. 3.5 shows the shear stress – shear strain, principal concrete
compressive stress – principal compressive strain, principal concrete tensile
stress – principal tensile strain, shear stress – shear strain by LVDTs, shear
stress – shear strain by LEDs, shear stress – longitudinal strain, shear stress –
transverse strain, shear stress – maximum crack width, and shear stress –
average crack width graphs of H550A Series. H550A-PS specimen suffered
from edge failure.
-
67
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A Series
ρx = 2.09% fyx = 631 MPa
ρy = 1.35% fyy = 653 MPa
sx = 54 mm sy = 54 mm
fc' = 55.8 MPa ag = 20 mm
H550A-PS: fn/v = 0
H550A-SBC: fn/v = -0.2
edge failure
(a) Shear stress – shear strain of H550A Series
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A Series
ρx = 2.09 % fyx = 631 MPa
ρy = 1.35 % fyy = 653 MPa
sx = 54 mm sy = 54 mm
fc' = 55.8 MPa ag = 20 mm
H550A-PS: fn/v = 0
H550A-SBC: fn/v = -0.2
edge failure
(b) Shear stress – shear strain of H550A Series with unloading part deleted
-
68
(c) Principal concrete compressive stress – principal compressive strain of
H550A Series
(d) Principal concrete tensile stress – principal tensile strain of H550A-PS
-
69
(e) Principal concrete tensile stress – principal tensile strain of H550A-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A-PS
Average
Northface
Southface
edge failure
(f) Shear stress – shear strain by LVDTs of H550A-PS
-
70
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A-SBC
Average
Northface
Southface
(g) Shear stress – shear strain by LVDTs of H550A-SBC
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A-PS
LVDT
LED
(h) Shear stress – shear strain by LVDTs and LEDs of H550A-PS
-
71
0 20 40 60 80
Shear Strain, mm/m
0
2
4
6
8
10
12H550A-SBC
LVDT
LED
(i) Shear stress – shear strain by LVDTs and LEDs of H550A-SBC
(j) Shear stress – longitudinal strain of H550A Series
-
72
0 4 8 12 16
Transverse Strain, mm/m
0
2
4
6
8
10
12
H550A SeriesLVDT
ERSG Average
ERSG Top
ERSG Bottom
H550A-PS: fn/v = 0
H550A-SBC: fn/v = -0.4
(k) Shear stress – transverse strain of H550A Series
(l) Shear stress – maximum crack width of H550A Series
-
73
(m) Shear stress – average crack width of H550A Series
Fig. 3.5 Experimental results of H550A Series
-
74
Chapter 4 Observations and Analysis
4.1 Applicability of High-Strength Materials
To investigate the applicability of high-strength materials to shear design of
nuclear power plant structure, the twelve specimens were divided into five
series. Among them, N420A Series, N550B Series and H550B Series were
compared in more detail in this chapter. N420A Series specimens are
representative of APR 1400 nuclear power plant low level wall element that
currently used in the field. N420A Series used 42 MPa design compressive
strength concrete, 420 MPa design yield strength rebar and APR 1400 nuclear
power plant low level wall reinforcement ratio. N550B Series used 42 MPa
design compressive strength concrete, 550 MPa high design yield strength
rebar and decreased reinforcement ratio according to the ratio of 420 over 550.
H550B Series used same properties with N550B Series except concrete
strength. H550B Series used 70 MPa high design compressive strength
concrete.
Fig. 4.1 shows the comparison of N420A Series and N550B Series shear
stress – shear strain relationships. The N550B Series specimens shows almost
same shear behavior with N420A Series except specimens with biaxial
compression stresses as can be seen in Fig. 4.1. Once the peak load was
reached, N420A-SBC and N550B-SBC specimens failed explosively. N550B-
SBC specimen failed with no yielding of reinforcement and N420A-SBC
specimen failed as soon as the longitudinal rebar yielded.
-
75
Fig. 4.1 Shear stress – shear strain of N420A and N550B Series
N550B Series showed somewhat low shear stiffness than N420A Series
because the steel stiffness was decreased with decreased reinforcement ratio.
The reinforcement ratio of N550B Series was decreased by 420 over 550 to
make the almost same ρfy values with N420A Series. But the decreased
reinforcement ratio ρ made decreased steel stiffness ρEs, and the decreased
steel stiffness made the decreased shear stiffness of N550B Series. Especially,
N420A-PS and N550B-PS specimens used same concrete. Even the ρfy
value of N550B-PS are larger than N420A-PS as you can see in Table 4.1,
N550B-PS shows low shear stiffness and shear strength than N420A-PS.
-
76
Table 4.1 Comparison of N420A-PS and N550B-PS
N420A-PS N550B-PS
fc' (MPa) 35.2
vu (MPa) 7.70 7.68
fyx (MPa) 448 631
fyy (MPa) 477 631
ρx (%) 2.09 1.56
ρy (%) 1.35 1.04
ρxfyx (MPa) 9.36 9.84
ρyfyy (MPa) 6.44 6.56
ρxEs (MPa) 4180 3120
ρyEs (MPa) 2700 2080
Because of decreased ρEs values, N550B Series showed larger shear
strain than N420A Series as can be seen in Fig. 4.1. And also N550B Series
showed larger maximum crack width and average crack width as can be seen
in Fig. 4.2 and Fig. 4.3. These large shear strains and crack widths are
softening the concrete. The shear strength is decreased by large shear strains
and crack widths. This is called by strain effect. The effect is small in service
load level, but the additional research will be required.
-
77
Fig. 4.2 Shear stress – maximum crack width of N420A and N550B Series
Fig. 4.3 Shear stress – average crack width of N420A and N550B Series
-
78
Fig. 4.4 Shear stress – shear strain of N420A-PS, N550B-PS and H550B-PS
H550B-PS specimen used 70 MPa high design compressive strength
concrete. H550B-PS behaved in a ductile manner with the shear strain
exceeding 0.048 before the load carrying capacity was significantly reduced
as can be seen in Fig. 4.4. H550B-PS specimen failed after yielding of both
rebars sufficiently as can be seen in Table 4.2.
Table 4.2 Comparison of N420A-PS, N550B-PS and H550B-PS
Specimens fc' (MPa) vu (MPa) γxy (10-3) εx / εsyx (%) εy / εsyy (%)
N420A-PS 35.2 7.70 10.95 115.2 227.7
N550B-PS 35.2 7.68 9.64 83.7 136.3
H550B-PS 55.8 8.08 17.94 122.0 344.2
-
79
4.2 Applicability of Modified Compression Field Theory
The Modified Compression Field Theory (MCFT) uses equilibrium,
compatibility and constitutive relations to predict the stress – strain response
of reinforced concrete members subjected to shear as discussed in chapter 1.2.
For the analysis of shear behavior of the reinforced concrete elements by
MCFT in this study, CAN CSA A23.3 M84 compression softening equation
and Bentz 1999 tension stiffening equation were used. And for the concrete
stress – strain curve, the Popovich (HSC) formulation was used to analyze the
shear behavior of reinforced concrete elements.
1
11
0.8 170
p c
p c
c
f fb
e e
be
¢=
¢=
= £-
(4.1)
1
11 3.6t
c
c
b
ff
M
AM
d
e
p
=+
=å
(4.2)
Eq. (4.1) is CAN CSA A23.3 M84 compression softening model. This
model is strength only softened version. Eq. (4.2) is Bentz 1999 tension
stiffening model. M is bond parameter to indicate the bond characteristics of
different arrays of reinforcement is to divide the area of concrete in tension by
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80
the perimeter of all the reinforcing bars bonded to the area. Ac is are of
concrete reinforced by the bar and db is the diameter of reinforcing bar. In a
case that the different reinforcement is used by directions, the selected value
of the M parameter will be the lowest value for each of the orthogonal
reinforcement directions.
Fig. 4.5 shows the observed shear stress – shear strain response for each
test series along with the corresponding MCFT predictions. The mean MCFT
predicted to test ratio for the peak shear stress was 1.03 with a coefficient of
variation of only 6.4 %. The strains at peak stress were also well predicted
with a mean predicted to test ratio of 1.04 and a coefficient of variation of
13.5 %. The concrete principal compressive stresses at peak stress were also
well predicted with a mean predicted to test ratio of 0.98 and a coefficient of
variation of 5.5 %. Table 4.3 provides a summary of the observed and
predicted values of twelve reinforced concrete elements.
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81
(a) N420A Series
(b) N550B Series
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82
(c) N550A Series
(d) H550B Series
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83
(e) H550A Series
Fig. 4.5 Comparison of predicted and observed shear stress – shear strain
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84
Table 4.3 Comparison of observed and MCFT predicted values
Specimens fn / v
Observed MCFT Prediction Predicted / Observed
vu
(MPa)
Values at vu vu
(MPa)
Values at vu
vu
Values at vu
fc1
(MPa)
fc2
(MPa)
γxy
(10-3)
fc1
(MPa)
fc2
(MPa)
γxy
(10-3) fc2 γxy
N420A-PS 0 7.70 -0.06 15.74 10.95 7.80 0 15.80 11.66 1.01 1.00 1.02
N420A-SBT +0.4 5.87 0.37 11.61 17.34 5.55 0 11.40 17.03 0.95 0.98 0.94
N420A-SBC -0.4 9.56 -0.58 21.01 7.09 10.52 0.68 20.39 7.13 1.10 0.97 1.01
N550B-PS 0 7.68 0.32 15.87 9.64 7.95 0.51 15.49 10.05 1.04 0.98 1.04
N550B-SBT +0.4 5.97 0.25 12.00 21.65 5.71 0 11.85 18.80 0.96 0.99 0.81
N550B-SBC -0.4 10.47 -0.44 22.75 8.26 10.08 0.49 19.71 8.97 0.96 0.87 1.09
N550A-PS 0 9.64 -0.15 20.33 9.98 9.37 0.54 18.26 9.88 0.97 0.90 0.99
N550A-SBT +0.4 6.93 -0.10 14.22 8.29 7.63 0.52 15.02 11.94 1.10 1.06 1.44
H550B-PS 0 8.08 0.04 16.44 17.94 8.05 0 16.41 18.40 1.00 1.00 0.96
H550B-SBC -0.3 10.48 -0.74 21.95 12.56 11.43 0.28 22.71 11.80 1.09 1.03 0.94
H550A-PS 0 9.84 -0.13 20.93 11.43 10.80 0.53 21.47 11.01 1.10 1.03 0.96
H550A-SBC -0.2 11.27 -0.58 24.73 10.16 12.60 0.42 24.84 10.66 1.12 1.00 1.05
Average 1.03 0.98 1.04
Coefficient of variation, % 6.4 5.5 13.5
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85
As can be seen in Table 4.3, most specimens’ shear behavior is quite well
predicted by MCFT. Especially, the shear strength and the concrete principal
compressive stresses at peak stress of N420A-PS, N420A-SBT, N550B-PS,
N550B-SBT, and H550B-PS were predicted by only less than 5 % error. The
MCFT is also able to predict the full load deformation response with good
accuracy. In particular, the cracked elastic stiffness was well predicted for all
elements. But the shear strength and the concrete principal compressive
stresses at peak stress of N420A-SBC, N550B-SBC, N550A-PS, N550A-SBT,
H550B-SBC, H550A-PS and H550A-SBC were predicted by over then 5 %
error. The concrete principal tensile stresses at peak stress of these specimens
show somewhat big difference over than 0.62 MPa. Fig. 4.6 shows the
comparison of concrete principal compressive stresses of all tests.
(a) N420A Series
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86
(b) N550B Series
(c) N550A Series
-
87
(d) H550B Series
(e) H550A Series
Fig. 4.6 Comparison of predicted and observed principal compressive stress –
principal compressive strain
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88
4.3 Modification of Tension Stiffening Equation
According to Bentz (2005) paper, the coefficient of factor for ε1 strain in
denominator in tension stiffening equations was determined from Fig. 4.7.
Fig. 4.7 Tension stiffening denominator versus bond parameter
By the way, the solid square marker was obtained from only three
specimens of Toronto Large Elements SE1, SE6, and SE12 as can be seen by
Fig. 4.8. And Fig. 4.9 shows comparisons between the test data and Bentz
tension stiffening equation as shown in Eq. (4.2).
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89
Fig. 4.8 Tension stiffening denominator of individual Toronto Large Elements
experiments versus bond parameter
(a) SE1
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90
(b) SE6
(c) SE12
Fig. 4.9 Comparison of predicted and observed principal tensile stress –
principal tensile strain with Bentz tension stiffening equation
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91
From Fig. 4.9, the difference between the test and the MCFT prediction
by the Bentz tension stiffening equation can be regarded as acceptable. In the
same manner in the Bentz (2005) paper, the coefficients for large reinforced
concrete elements that have been reported so far including the twelve
specimens in this study were obtained.
As seen in Fig. 4.10, overall comparison between the test results and the
prediction by Bentz tension stiffening equation shows that Bentz equation
gives consistently overestimates the tension stiffening effect after cracking. As
the first trial, therefore, A = 8.0 which is almost twice greater than Bentz
tension stiffening equation’s coefficient 3.6 is applied to Eq. (4.3)
1
11t
c
ff
A M e=
+ × × (4.3)
Fig. 4.10 also includes the estimations by applying 8.0 to A in the Eq.
(4.3). From the comparison of MCFT prediction by Bentz tension stiffening
equation and an example prediction with A = 8.0 in Eq. (4.3), the modification
of A is required.
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92
(a) N420A-PS
(b) N420A-SBT
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93
(c) N420A-SBC
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-PS
Test
Bentz
A = 8.0
(d) N550B-PS
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94
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-SBT
Test
Bentz
A = 8.0
(e) N550B-SBT
(f) N550B-SBC
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95
(g) N550A-PS
(h) N550A-SBT
-
96
(i) H550B-PS
(j) H550B-SBC
-
97
(k) H550A-PS
(l) H550A-SBC
-
98
(m) SE1
(n) SE5
-
99
(o) SE6
(p) SE11
-
100
(q) SE12
(r) SE13
-
101
(s) SE13
(t) SE13
Fig. 4.10 Comparison of test, Bentz, and modified Bentz with A = 8.0 in
principal tensile behavior
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102
By the way, only the modification of A could not be satisfactory. Right
after cracking the Bentz tension stiffening equation underestimates and after
some point, the Bentz equation overestimates the test results. The difference
between the test and estimation is not a matter of coefficient value. In other
words, it is matter of form of equation.
Through several trials, removing of square root in the denominator like
Eq. (4.4) gives better correlation with the large elements test results.
1
11t
c
ff
A M e=
+ × × (4.4)
Fig. 4.11 shows comparison of Bentz tension stiffening equation and Eq.
(4.4) with the best coefficient A which were found for each specimen. As
shown in Fig. 4.11, removing of square root could simulates better the
descending branch immediately after cracking as well as overall response.
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103
(a) N420A-PS
(b) N420A-SBT
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104
(c) N420A-SBC
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-PS
Test
Bentz
A = 3.6
(d) N550B-PS
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105
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-SBT
Test
Bentz
A = 3.7
(e) N550B-SBT
(f) N550B-SBC
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106
(g) N550A-PS
(h) N550A-SBT
-
107
(i) H550B-PS
(j) H550B-SBC
-
108
(k) H550A-PS
(l) H550A-SBC
-
109
(m) SE1
(n) SE5
-
110
(o) SE6
(p) SE11
-
111
(q) SE12
(r) SE13
-
112
(s) SE14
(t) EZ9
Fig. 4.11 Comparison of test, Bentz, and Eq. (4.4) with best coefficient A for
each specimen
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113
In the same manner with Bentz (2005), all best coefficient of A for each
specimen was averaged and A = 4.5 was obtained as shown in Fig. 4.12.
Fig. 4.12 Tension stiffening denominator versus bond parameter by new
equation
Consequently, a new equation for tension stiffening equation after
cracking is proposed like Eq. (4.5).
1
11 4.5t
c
ff
Me=
+ (4.5)
Following Fig. 4.13 are comparison of the test results, Bentz equation,
and the Eq. (4.5).
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114
(a) N420A-PS
(b) N420A-SBT
-
115
(c) N420A-SBC
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-PS
Test
Bentz
This study
(d) N550B-PS
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116
0 4 8 12 16
Principal Tensile Strain, ×10-3
-1
0
1
2
3N550B-SBT
Test
Bentz
This study
(e) N550B-SBT
(f) N550B-SBC
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117
(g) N550A-PS
(h) N550A-SBT
-
118
(i) H550B-PS
(j) H550B-SBC
-
119
(k) H550A-PS
(l) H550A-SBC
-
120
(m) SE1
(n) SE5
-
121
(o) SE6
(p) SE11
-
122
(q) SE12
(r) SE13
-
123
(s) SE14
(t) EZ9
Fig. 4.13 Comparison of test, Bentz, and proposed equation in this study
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124
Chapter 5 Conclusion
In-plane shear tests of twelve large reinforced concrete elements representing
nuclear power plant low level wall element were performed. Shear behavior
of reinforced concrete elements with high-strength materials was compared
with reinforced concrete elements of APR 1400 nuclear power plant wall’s
shear critical region. N420A Series representing APR 1400 nuclear power
plant wall and N550B Series reinforced with high-strength reinforcing bars
showed almost same shear behavior. H550B Series that applied with high-
strength reinforcing bars and high-strength concrete showed quite ductile
shear response. These test results showed the applicability of high-strength
materials to the shear design of nuclear power plant structures.
Modified Compression Field Theory accurately predicted the ultimate
shear strength by the average of prediction to test ratio 1.03 and coefficient of
variation 6.4 %. Also MCFT accurately predicted the shear strain and
principal compressive concrete stress at ultimate shear strength by the average
of prediction to test ratio 1.04, coefficient of variation 13.5 % and the average
of prediction to test ratio 0.98, coefficient of variation 5.5 % respectively. But
the Bentz tension stiffening equation overestimates the test results of large
reinforced concrete elements. The proposed tension stiffening equation for
large reinforced concrete elements in this thesis made predictions better the
principal tensile concrete stress after cracking of large reinforced concrete
elements.
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125
References
Bae, G-M, Proestos, G. T., Lee, S-C, Bentz, E. C., Collins, M. P., and Cho, J-Y
(2013), “In-Plane Shear Behavior of Nuclear Power Plant Wall Elements with
High-Strength Reinforcing Bars,” SMiRT-22 Transactions.
Bentz, E. C. (2005), “Explaining the Riddle of Tension Stiffening Models for
Shear Panel Experiments,” Journal of Structural Engineering, V. 131, No. 9,
pp. 1422-1425.
Bentz, E. C., Vecchio, F. J., and Collins, M. P. (2006), “The Simplified MCFT
for Calculating the Shear Strength of Reinforced Concrete Elements,” ACI
Structural Journal, V. 103, No. 4, pp. 614-624.
Biedermann, J. D. (1987), “The Design of Reinforced Concrete Shell
Elements an Analytical and Experimental Study,” M.A.Sc thesis, Department
of Civil Engineering, University of Toronto, Canada.
Collins, M. P., and Mitchell, D. (1991), Prestressed Concrete Structures,
Prentice Hall, 766 pp.
Hsu, T. T. C., and Mau, S. T. (1992), Concrete Shear in Earthquake, Elsevier
Applied Science, 518 pp.
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126
Khalifa, J. (1986), “Limit Analysis and Design of Reinforced Concrete Shell
Elements,” PhD thesis, Department of Civil Engineering, University of
Toronto, Canada.
Kirschner, U. H. K. (1986), “Investigating the Behavior of Reinforced
Concrete Shell Elements,” PhD thesis, Department of Civil Engineering,
University of Toronto, Canada.
Kuchma, D. A. (1996), “The Influence of T-headed Bars on the Strength and
Ductility of Reinforced Concrete Wall Elements,” PhD thesis, Department of
Civil Engineering, University of Toronto, Canada.
Liping, X., Bentz, E. C., and Collins, M. P. (2011), “Influence of Axial Stress
on Shear Response of Reinforced Concrete Elements,” ACI Structural Journal,
V. 108, No. 6, pp. 745-754.
Porasz, A. (1989), “An Investigation of the Stress-Strain Characteristics of
High Strength Concrete in Shear,” M.A.Sc thesis, Department of Civil
Engineering, University of Toronto, Canada.
Stevens, N. J., Uzumeri, S. M., and Collins, M. P. (1991), “Constitutive Model
for Reinforced Concrete Finite Element Analysis,” ACI Structural Journal, V.
88, No. 1, pp. 49-59.
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127
Vecchio, F. J., and Collins, M. P. (1986), “The Modified Compression-Field
Theory for Reinforced Concrete Elements Subjected to Shear,” ACI Journal,
V. 83, No. 2, pp. 219-231.
Vecchio, F. J., and Selby, R. G. (1991), “Toward Compression-Field Analysis
of Reinforced Concrete Solids,” Journal of Structural Engineering, V. 117,
No. 6, pp. 1740-1758.
Vecchio, F. J., and Collins, M. P. (1993), “Compression Response of Cracked
Reinforced Concrete,” Journal of Structural Engineering, V. 119, No. 12, pp.
3590-3610.
Vecchio, F. J., Collins, M. P., and Aspiotis, J. (1994), “High-Strength Concrete
Elements Subjected to Shear,” ACI Structural Journal, V. 91, No. 4, pp. 423-
433.
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128
초 록
본 논문에서는 전단 및 이축 응력을 받는 12개 철근콘크리트
요소의 실험결과가 제시된다. 요소들은 실제 원전구조물 벽체
요소의 1/3 스케일로 제작되었고, 지진하중, 원전 사고시 내압의
증가를 고려하여 하중조건이 결정되었으며, 토론토대학교의 Shell
Element Tester를 이용하여 철근콘크리트 요소가 파괴될 때까지
가력되었다. 기준실험체에는 현 APR 1400 원전구조물에서
사용되는 콘크리트 압축강도, 철근 항복강도 및 철근비가
사용되었고, 고강도 콘크리트, 고강도 철근 및 감소된 철근비가
사용된 철근콘크리트 요소와 기준실험체의 전단 거동이 비교되었다.
한편, 최근 철근콘크리트 구조물의 전단 설계에는 압축장이론이
도입되고 있다. 특히 수정압축장이론은 CSA Standards, AASHTO
LRFD, fib Model code, Eurocode 2 전단 설계에 도입되었다. 향후
ASME, ACI 318, ACI 349와 같은 원전구조물 설계 관련
설계기준에도 수정압축장이론이 도입될 것으로 예측된다.
수정압축장이론은 예측값 대비 실험값을 평균 1.03, 변동계수
6.4 %로 매우 정확히 예측하였다. 최대 전단 응력에서의 전단
변형률 또한 평균 1.04, 변동계수 13.5 %로 정확히 예측되었다.
수정압축장이론은 균열 이후 요소의 전단 강성도 잘 예측하여
원전구조물의 전단 설계에 적용가능성을 보여주었다. 그리고 대형
철근콘크리트 요소에 대한 새로운 인장 경화 모델이 실험결과를
바탕으로 제안되었다.
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129
주요어: 콘크리트 전단, 고강도 재료, 원전구조물, 수정압축장이론,
인장 경화
학 번: 2011-20982
Chapter 1 Introduction 1.1 General 1.2 Modified Compression Field Theory 1.3 Objective and Scope
Chapter 2 Experimental Program 2.1 Test Variables 2.2 Specimen Descriptions 2.3 Shell Element Tester 2.4 Instrumentation
Chapter 3 Experimental Results 3.1 N420A Series 3.2 N550B Series 3.3 N550A Series 3.4 H550B Series 3.5 H550A Series
Chapter 4 Observations and Analysis 4.1 Applicability of High-Strength Materials 4.2 Applicability of Modified Compression Field Theory 4.3 Modification of Tension Stiffening Equation
Chapter 5 Conclusion References Abstract
11Chapter 1 Introduction 1 1.1 General 1 1.2 Modified Compression Field Theory 4 1.3 Objective and Scope 9Chapter 2 Experimental Program 10 2.1 Test Variables 10 2.2 Specimen Descriptions 16 2.3 Shell Element Tester 21 2.4 Instrumentation 24Chapter 3 Experimental Results 30 3.1 N420A Series 32 3.2 N550B Series 41 3.3 N550A Series 50 3.4 H550B Series 58 3.5 H550A Series 66Chapter 4 Observations and Analysis 74 4.1 Applicability of High-Strength Materials 74 4.2 Applicability of Modified Compression Field Theory 79 4.3 Modification of Tension Stiffening Equation 88Chapter 5 Conclusion 124References 125Abstract 128