Investigation of Axial Strengthened Reinforced Concrete...
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Research ArticleInvestigation of Axial Strengthened Reinforced ConcreteColumns under Lateral Blast Loading
Mohammad Esmaeilnia Omran and SomayehMollaei
Department of Civil Engineering, University of Kurdistan, Sanandaj, Iran
Correspondence should be addressed to Somayeh Mollaei; [email protected]
Received 26 May 2017; Revised 25 August 2017; Accepted 6 September 2017; Published 16 October 2017
Academic Editor: Abdul Qadir Bhatti
Copyright © 2017 Mohammad Esmaeilnia Omran and Somayeh Mollaei. This is an open access article distributed under theCreative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, providedthe original work is properly cited.
Different factors can affect blast response of structural components. Hence, experimental tests could be the best method forevaluating structures under blast loading. Therefore, an experimental explosion loading has been done on RC members by theauthors. Four RC components, with identical geometry and material, with and without axial load were imposed to air blast.Observed data of the members’ response under blast loading was used for validation of finite element modeling process usingABAQUS software. With respect to complexity, limitations, and high costs of experimental tests, analytical studies and softwaremodeling can be good alternatives. Accordingly, in this paper, the behavior of 6 different models of normal and strengthenedRC columns under blast loading was evaluated using ABAQUS. Strengthening configurations considered here were designed forenhancing axial capacity of RC columns.Therefore, we can investigate the effectiveness of axial strengthening of column on its blastresistance capacity and residual axial strength. The considered strengthening methods were different steel jacket configurationsincluding steel angle, channel, and plate sections. The results showed that retrofitting significantly improves blast performance ofthe columns. Moreover, residual strength capacity of the columns strengthened with steel channel is higher than the other models.
1. Introduction
A wide range of engineering structures such as high-risebuildings, bridges, tunnels, dams, platforms, and militaryand security shelters are constructed by reinforced concretematerials. There has been much attention to reinforced con-crete (RC) structures performance under static and seismicloads but evaluation of RC structures’ behavior under blastloading and identification of their dynamic characteristicsare important for valid design of concrete structures giventhat many structures may face extreme dynamic loading suchas explosion in their lifetime. Columns are the key loadbearing elements in building structures and in case of anexplosion event near the building, columns are mostly thefirst structural elements which are affected by lateral loadingcaused by explosion. Studying the explosion of explosiveshas been considered by scientists and researchers and theefforts of scientists and researchers in the field of shock wavephysics became important since the 20th century [1]. One ofthe pioneers in this field is Hopkinson (1915) who conducted
extensive research and tests and formed the Hopkinson-Cranz scaling law [1, 2].
Recently, many different studies have been conductedon different types of concrete structures such as columnsunder explosion loads [3–7]. With respect to complexity,limitations, and high cost of laboratory researches in thisfield, analytical studies and software modeling can be agood alternative to laboratory and experimental methods.Finite element analysis method is a powerful and usefultool for researchers and structural designers to have anaccurate estimation of behavior of structures under blastloading without requiring high costs and great difficulty. Shiet al. (2008) defined a failure criterion based on residualaxial capacity for reinforced concrete columns and drew 𝑃-𝐼 (pressure-impulse) diagrams for columns based on thisfailure criterion using numerical modeling by LS-DYNAsoftware [8]. Bao and Li (2010) conducted parametric studieson RC columns using numerical modeling in LS-DYNA [3].In line with the most important results, reinforced concretecolumns must be designed in such a way that their moment
HindawiShock and VibrationVolume 2017, Article ID 3252543, 18 pageshttps://doi.org/10.1155/2017/3252543
2 Shock and Vibration
capacity should be less than shear capacity. On the otherhand, lateral deformation of column must be controlled inorder to prevent instability caused by secondary moments.In this study, standoff distance has been considered to beconstant and explosion has been considered to occur at aclose distance. A similar study has been carried out by Wuet al. (2011) using arbitrary Euler–Lagrange analysis in LS-DYNA software for analysis of columns’ response undercontact explosion [9].The results obtained have been used forevaluation of residual axial capacity of columns and the effectof different parameters on this capacity has been evaluated.ABAQUS/Explicit software has been used in finite elementmodeling by Arlery et al. (2013) on effects of close explosionon reinforced concrete columns [10]. In line with the results,depth of column section and distance to the center of theexplosion had the greatest effects in reducing the amount ofdamage in the column and height and width of section andconcrete compressive strength are less effective [10]. Centerof the explosion is extremely close to the structure in thisstudy and the response of structure in this case is usuallylocal and in form of erosion of section. A numerical studywas carried out by Kyei and Braimah (2017) to investigatethe effects of transverse reinforcement spacing on the blastresistance of RC columns using LS-DYNA code. The studyrevealed that the effect of transverse reinforcement spacingand axial loading significantly affects RC column behav-ior under blast loading at low scaled distances. At higherscaled distances, however, the effects were insignificant[11].
Some researchers have studied the retrofitting andstrengthening of RC columns under the blast loading. Craw-ford (2013) reported some of the methods of using FRPfor strengthening RC columns in order to increase thestrength of RC columns under the simultaneous effect of blastloading and axial force [6]. According to the main results,FRP coating increases the ductility and shear strength ofthe column. The focus in these studies was based on FRPmaterial and other methods for retrofitting RC columns werenot considered. Carriere et al. (2009) have introduced SRPcovers as a perfect replacement for CFRP for retrofittingRC elements against explosion [12]. The effect of retrofittingreinforced concrete beams and columns using SRP coatinghas been evaluated using explosion tests and numericalmodeling by AUTODYN. Based on the obtained results, SRPcoatings have lower cost and easier installation process incomparison to CFRP covers. Also, SRP increases ductilityof RC columns under blast loading and prevents brittlecollapse of RC columns. Nevertheless, there has been noreference to displacements or strains in the consideredsamples and also the scales of studied samples are small.Xu et al. (2016) discussed the blast resistance of UHPC(ultra-high performance concrete) columns by conductinga series of field tests. It was reported that UHPC materialsprovide sufficient strength, ductility, and energy absorptionand crack controlling capacities compared to conventionalnormal strength concrete [13]. Zhang et al. (2016) reportedan experimental investigation on Concrete-filled double-skin tubes (CFDST) columns subjected to blast loading.Based on the results, it was obvious that CFDST column
Pres
sure
Time
Atmospheric pressure
O A B
C
D−
+
20
Figure 1: Pressure-time diagram of blast wave.
has excellent blast resistance and it can prevent concretecrushing and steel buckling and thus has an overall globalflexural response as opposed to localized structural failure[14].
By reviewing literature, it can be observed that retrofittingeffects have been considered in minor studies. Moreover,most studies about blast retrofitting of RC columns have beenconsidered using polymer sheets. On the other hand, the needfor further studies in this field still remains due to uncer-tainties in the phenomenon of explosion and complexity ofthe behavior of RC sections under lateral blast loading.Thus,in this paper, 6 models of retrofitted RC columns have beenevaluated under blast loading. The effects of different config-uration of steel jackets have been investigated usingABAQUS6.13 software [15]. All of the strengthening configurationsconsidered herewere designedwith the purpose of enhancingthe axial load bearing capacity of the RC columns.Therefore,we can investigate the effectiveness of axial strengtheningof the RC columns by steel jackets on their blast resistancecapacity.
2. Blast Loading
Explosion is an instantaneous phenomenon which createslarge amounts of light, heat, sound, and pressure resultingfrom blast wave due to sudden release of large amounts ofenergy. The real source of this energy can be gunpowder,steam compressed in the boiler, or uncontrolled nucleardevelopments. However, release of energy should be suddenand a high-energy environment should be formed aroundit. A part of this energy is released through heat radiationsand a part of it enters into the air (air blast) and ground(ground shock) through radial waves [18]. An approximatepressure-time diagram at a certain distance from the centerof the explosion is drawn in Figure 1. As can be seen in thefigure, Section𝐴 corresponds to time before the arrival of thewave front and 𝐵 is after incident shock impact and showsthe sudden increase of pressure. Positive pressure has endedat𝐶 and negative phase of pressure (suction) can be felt in theenvironment. This is alongside the blast wind in the oppositedirection to the direction of incident shock impact and 𝐷corresponds to the disappearance of blast wave effects andreturn of pressure to atmospheric pressure [19].
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200
200
1200
440
440
155
155
190
190
190
0F;N?
2.40
6 ∗ 4 0F;tes150 × 50 × 5
4, 50 × 53 ∗ 4 0F;tes150 × 100 × 5
Col-5Col-4Col-3Col-2Col-1Col-0
206 × 50
3.1 × 3.1
2C
Figure 2: Details of dimensions and retrofitting configuration of columns [16].
Methods for estimation of pressure diagram for anexplosion and its distribution on structural face have beenpresented in many different references [18–21].
3. Details of the Studied Models
Here, RC columns with the specifications provided in [16] byBelal et al. (2015) have been used. Six models of RC columnswere considered; one of them is simple (not retrofitted)while others are retrofitted using different configurationof steel jackets. Characteristics of the section and detailsof retrofitting methods for all samples are summarized inFigure 2 and Table 1. Columns have rectangular symmetricsection with dimensions of 200mm and height of 1200mmwhich retrofitting offered in order to increase their axialbearing capacity. Steel elements used in strengthening ofsamples have been used in such a way that they all have equalhorizontal cross-sectional area [16].
Concrete compressive strength used in samples is 34MPawhich is the same for all samples. Specifications of steelmaterials have been mentioned in Table 2 and failure strainhere is the strain which corresponds to ultimate tensile stressof steel material.
4. Finite Element Modeling
Here, finite element models of columns and steel jackets havebeen initially developed and then these models have beenanalyzed under lateral blast loading. Proper modeling andmeshing of reinforced concrete and steel as well as the inter-action between them are important factors in development ofaccuratemodels. Details ofmodeling process are explained inthis section.
4.1. Modeling of Concrete Material. Concrete damage plastic-ity (CDP) model has been used in this study for modelingof concrete’s behavior which was presented by Lubliner etal. (1989) [22] and was later completed by other researchers[23, 24]. Two main failure mechanisms including tensilecracking and compressive crushing are assumed for concretein this model. Nonlinear behavior of concrete is describedusing isotropic damage elasticity and tensile and compressiveplastic concepts. Figure 3 shows stress-strain curves forconcrete material in uniaxial tension and compression.
In Figure 3, 𝐸0 is the modulus of elasticity, 𝜎𝑡 is tensilestress, 𝜎𝑐 is compressive stress, 𝜀𝑡
∼ck is cracking strain, 𝜀𝑡∼in
is inelastic strain associated with existing stress, and 𝑑𝑡
4 Shock and Vibration
t
t
t0
E0
(1 − dc)E0
tJF t
?F
(a)
c
c
cu
c0
E0
(1 − dc)E0
cJF c
?F
(b)
Figure 3: Uniaxial behavior of concrete; (a) tension; (b) compression [15].
Table 1: Specifications of models (dimensions: mm).
Model Strengthening configuration Longitudinal and transverse reinforcement DimensionsCol-0 Without strengthening 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Col-1 Steel angles4 L 50 × 50 × 5 + 3 × 4 plates 150 × 100 × 2 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Col-2 Steel angles4 L 50 × 50 × 5 + 3 × 4 plates 150 × 50 × 2 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Col-3 Steel channels2C (206 × 50)/(3.1 × 3.1) + 3 × 4 plates 150 × 100 × 2 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Col-4 Steel channels2C (206 × 50)/(3.1 × 3.1) + 3 × 4 plates 150 × 50 × 2 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Col-5 Complete steel jacket (steel plates)4 × 4 plates 200 × 2.4 4 𝜙 12 - 𝜙 8 @ 100 200 × 200 × 1200
Table 2: Specifications of steel material.
Material Nominal diameter (mm) Modulus of elasticity (MPa) Yield strength (MPa) Ultimate stress (MPa) Failure strainLongitudinal bars 12 210000 360 463 11Stirrups 8 210000 240 340 14
and 𝑑𝑐 are damage parameters in tension and compression,respectively. Completion of failure surface is controlled usinghardening variables of 𝜀𝑐
pl and 𝜀𝑡pl which are, respectively,
related to failure mechanisms under compressive and tensileloading [15]. In fact, 𝜀𝑐
pl and 𝜀𝑡pl are equivalent plastic strains.
Stress-strain curve changes linearly until the failure stresspoint 𝜎𝑡0 due to uniaxial tensile of stress-strain curve andthese stresses are along with onset and extension of smallcracks in concrete. Damage will be visible in form of cracksafter passing the mentioned point which is shown in form ofsoftening regime in stress-strain space. Response in uniaxialcompressive will be elastic until reaching 𝜎co yielding pointand behavior in plastic zone is generally expressed in form ofhardening regime and curves will change to softening curvesin the end by reaching the point of ultimate tension 𝜎cu[15].
4.1.1. Failure Criterion. William-Warnke failure criterion andHillborg failure energy model (1976) are used to describe thefailure and crack propagation in CDP model. The general
form of William-Warnke failure criterion is in the formof
𝐹 (𝐼1, 𝐼2, 𝐼3) = 0, (1)
where 𝐼1, 𝐼2, and 𝐼3 are the first, second, and third stresstensor invariables, respectively. This failure surface is a cone-like shape in the stress space. Each form of stress correspondsto one point in stress space. If this point is out of space definedin the above equation, it shows the failure ofmaterial [15].Thebrittle behavior of concrete in Hillborg failure energy modelis more determined by stress-displacement response than bystress-strain response under the tension. Crack failure energymodel can be achieved using the expression of tensions afterfailure as a function of crack’s width [15].
In the CDP model used here, values for dilation angle,eccentricity, 𝑓𝑏0/𝑓𝑐0 ratio (compression biaxial yield stress touniaxial yield stress), 𝑘 yield level parameter, and viscosityparameter (𝜇) have been considered to be equal to 40, 0.1,1.16, 0.6667, and 0.001, respectively.
Shock and Vibration 5
Col-5Col-4Col-3Col-2Col-1Col-0
Figure 4: Finite element models of studied RC columns.
4.2. Modeling of Steel Material. In this study, steel reinforcingbars have been modeled separately and with dimensionssimilar to those used in real samples. Steel material behaviorhas been assumed to be linear elastic-perfectly plastic. Itshould be noted that the behavior of steel has been consideredto be isotropic. In all stages, Von-Mises surface model is usedhere for steel. In this model, yielding has been considered tobe isotropic and it has been assumed to be a function of mainstresses and when deviatoric stress reaches a critical value inthemain stresses space, yielding occurs.Thismodel is definedin the form of the following equation:
Φ = 12[(𝜎1 − 𝜎3)
2 + (𝜎1 − 𝜎2)2 + (𝜎2 − 𝜎3)
2] − 𝐹𝑦2. (2)
In this equation, 𝜎1, 𝜎2, and 𝜎3 describe the main stresses and𝐹𝑦 is the yield stress of material. In fact, the above equationdescribes a three-dimensional space in which each mode ofstress corresponds to one point in the stress space. If this pointis out of three-dimensional cylinder defined by the aboveequation, it shows the yielding of material. At this model,effect of hardening is not considered [15].
4.3. Concrete and Reinforcement Interaction. The interac-tion between concrete and steel reinforcing bars is a veryimportant parameter in modeling of RC structures. Thisinteraction as a factor causes continuity between steel andconcrete materials and thus makes it possible to use thewhole capacity of materials including concrete compressivestrength and tensile strength of steel bars. Embedded elementmodel has been used in this study formodeling of interactionbetween concrete and steel elements. In this technique, if anode of steel elements is placed in concrete elements, degreesof freedom for that node are removed and node becomesa buried node. Thus, the degrees of freedom for buriednode are calculated using the degrees of freedom of concreteelements adjacent to this node.Therefore, degrees of freedom
of each buried node depend on degree of freedom of concreteelement node adjacent to it [15].
4.4. Meshing and Elements. C3D8R solid element has beenused for three-dimensional modeling of concrete. This ele-ment is a three-dimensional cube with 8 nodes which usesreduced integration method. T3D2 truss element has beenused for modeling of steel bars which is a three-dimensionaltruss element with 2 nodes. This element has been selectedbecause axial force plays a key role in the analysis of barsand there is no need for elements with several nodes.Thus, volume and time of computation will be significantlyreduced. S4R shell element has also been used for modelingof steel jacket which is three-dimensional shell element with4 nodes and 6 degrees of freedom [15].
Figure 4 shows finite element models of RC columns withdifferent types of steel jacket retrofitting configuration. In thenext section, these columns will be evaluated under the effectof blast loading.
4.5. Loading and Boundary Conditions. Blast loading appliedon columns has been done based on the methodologyproposed in UFC 3-340-02 [19]. Determined pressure hasbeen applied to lateral surface of the column. Figure 5 showspressure-time curve and applied pressure for blast loading ofthe retrofitted columns model.
5. Experimental Program
In the present study, a field test was conducted to inves-tigate the behavior of conventional columns subjected toblast loading. In total, four 0.35m × 0.35m RC memberswith the same reinforcement and span length of 3m weretested under an explosion loading at a standoff distance of3m. Blast test was performed on two reinforced concretecolumns with initial axial force and two columns without
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(a)
−0.5
00.5
11.5
22.5
33.5
4
Pres
sure
(N/m
G2)
10 20 30 400Time (msec)
(b)
Figure 5: Blast pressure-time history (b) and applied blast load (a).
3000 mm
150mm 150mm200 mm
Mid plate: 100 × 100 × 8mmEnd plates:350 × 300 × 8mm
350mm
Longitudinal bars:4Φ25
Closed stirrups:Φ10@200 mm
Cover: 50 mm
350mm
RC specimen
Supportstructure
Vertical steel section (lead indicators holder)
300 mm 500
mm
Steel plate: 300 × 1700 × 8mm
Steel bar: Φ24
Steel section: IPE200
Steel plate:300 × 2000 × 10 mm
Longitudinal bars:Φ22@170mm
Transverse bars:Φ22@170mm
700 mm
300 mm
Concrete cover:mm60
Figure 6: Cross section and reinforcement details of the specimen and support condition.
axial force to evaluate their behavior under the same load-ing conditions. RC components not forming part of theseismic force resisting system were detailed according toACI 318-14 [25]. The data collected from each specimenincluded maximum transverse displacement (deflections atcenter), axial strain of longitudinal bars, and postblast crackpatterns. Recorded data from this test were used in orderto validate FEM modeling and analysis process. Chargeweight including 20 kg of cartridge emulsion explosive with
density of 1.165 g/cm3 and velocity of detonation of 5800m/s(27mm diameter) is used such that TNT equivalent factoris about 0.90 (𝑊 = 18 kg-TNT). Dimensions and reinforce-ment details of the samples are shown in Figure 6. Allthe samples were placed horizontally simply on the supportstructure so that there were pinned support conditions atboth ends of the samples. Characteristic compressive strengthof the concrete, used for construction of the samples, wasdetermined by laboratory tests and its average value was
Shock and Vibration 7
(a)
Before After
(b)
Figure 7: Test setup for blast loading of the specimen (a) and aerial photos of the explosion event (b).
30MPa. AIII steel bars with yield strength of 400MPaand ultimate strength of 600MPa were used as longitudi-nal and transverse reinforcement as well as posttensioningsystem.
In order to impose constant axial compressive load on thesamples, 6 posttensioned steel bars were used and each barhad been initially tensioned using click-type torque wrench(Britool Expert HVT7200 (200–810N⋅m)). In each case, thebars were anchored to a 50mm thick steel plate at two ends ofthe columns. Constant axial stress in each steel barwas 100 kNand there were six posttensioning bars in every column.Hence, there is an axial force of 600 kN in two posttensionedcolumns (equal to 16% of the static axial load capacity of thecolumn). In Figure 7, the test setup and aerial photos of theexplosion event are shown.
Axial strain gauges (FLA-3-350-11, 350Ω (Tokyo SokkiKenkyujo Co. Ltd.)) were installed on the longitudinal barsat half-length of the samples.The data transferred from straingauges during the blast loading are recorded using digital dataacquisition card DAQ- NI USB-6009 (National InstrumentsCorporation). Lead rods were installed under the samples asmaximum displacement indicators at mid length.There weretwo lead rods under each sample and comparing their lengthbefore and after blast loading could show the maximumdisplacement of the column at mid length. Figure 8 showsthe shape of the indicator rods before and after blast loading.Based on the results, average amount of lateral displacement
of the columns with and without axial load under blastloading is 3.5 and 8mm, respectively.
FEmodeling and analysis of the columnswere done usingthe process described in Section 4. For imposing axial load, arigid part was modeled at one end of the column. Deformedshape and main crack pattern of the column models underblast loading are shown in Figure 9. Maximum transversedisplacement of a nod at mid length of the models with andwithout axial loading is calculated to be 3.04 and 7.23mm,respectively. These estimations are in a good agreement withexperimental test results.
Axial strain curves of the steel bars at mid length ofthe column resulting from strain gauges in the laboratoryspecimen are drawn in Figure 10 in comparison with FEMresults. The strain curves are for front face (up-side) andback face (beneath) of the columns. It was observed that FEanalysis can have an appropriate prediction of strain changesduring the blast loading. Some discrepancy of the resultscould occur probably because of unintended noises duringthe blast event that can affect recorded data.
In the next step of validation of the FE analysis,maximumblast response of the equivalent single-degree-of-freedom(SDOF) system of the considered RC beam (without axialforce) was calculated using UFC-3-340-02 [19] methodology(Chapters 3 and 4). For the charge weight of 18 kg-TNT withstandoff distance of 3m, the scaled distance of the blastloading is 𝑍 = 1.14m/kg1/3. At such scaled distance, one can
8 Shock and Vibration
Before After
Figure 8: Lead rods installed under the specimen.
P = 0
P = 600 kN
Figure 9: FE modeling and analysis of the columns.
assume uniformly pressure distribution on the structural face[19, 21]. Based on empirical equations proposed by UFC 3-340-02 [19], over-peak pressure (𝑃𝑠0 = 0.72MPa) and positivephase duration (𝑡0 = 5.1msec) of the blast wave could beestimated. Dynamic Increase Factor (DIF) for RC membersin bending for concrete and reinforcement is 1.05 and 1.17,respectively. Using the methodology introduced in UFC-3-340-02, estimated maximum response of elastoplastic SDOFsystem under ideal bilinear-triangular pulse is𝑋𝑚 = 9.18mm.Experimental result of maximum transverse displacement ofthe specimen without axial load was about 8mm. It shouldbe noted that generally this method produces a conservativeestimate of the blast response of the structure for designpurpose [19].
Selected sample for validation axial loading process in FEsoftware is a real columnwhich has been considered as 0C0 in
[17] by Hadi and Widiarsa (2012). Geometric characteristicsand reinforcing details in this sample are very similar toour own sample. Specifications of this model and its axialtest process are shown in Figure 11. Compressive strength ofconcrete in this sample is equal to 79.5MPa and yield strengthof longitudinal and transverse reinforcement is 564 and 516,respectively [17].
Sample 0C0 is tested under static axial loading andaxial load-displacement diagram is drawn for it. Axial load-displacement curves obtained from the experiments areshown in Figure 12(a) [17] in which dashed curve (– – –)is related to 0C0 sample column. Diagrams obtained fromFE modeling and experimental testing have been drawntogether for better comparison in Figure 12(b). It is evidentfrom Figure 12 that the result of FEM here matches withthe experimental results with a good accuracy. Thus, finiteelement method in this research can be used to continueanalysis.
6. Results of Analysis under Blast Loading
Curves in Figure 13 show the results of shear strength-lateraldisplacement (at the middle height) of the columns. It isevident from Figure 13 that the Col-0 which has not beenretrofitted has the lowest shear strength compared to othercolumns. In this model, the shear strength initially reachesthe maximum amount of 300 kN and then slightly increaseswith slight ups and downs. The initial resistance is greaterin other columns compared to Col-0 column. Moreover, thegreatest displacement of column’s mid height corresponds tounretrofitted column.
Curves in Figure 14 show horizontal displacement historyat the columns mid height. For better understanding of thedetails, results are shown once without Col-0 curve. It is clearthat Col-0 has the highest lateral deformation. In addition,the lowest horizontal displacement in themiddle height of thecolumns is observed for Col-3 and Col-4 (maximum amountof about 4mm). These columns have been strengthened bytwo steel channels and have shown a high resistance againstlateral blast loading. Moreover, Col-5 which is completelycovered with steel plates has shown a low deformation(maximum 10mm). Afterwards, there is Col-2 and Col-1 that
Shock and Vibration 9
Exp-(1)Exp-(7)FEM
Back face (P = 600 kN)
0.01 0.02 0.03 0.04 0.05 0.060Time (sec)
−0.0003
−0.0002
−0.0001
00.00010.00020.00030.00040.0005
Axi
al st
rain
Front face (P = 600 kN)
Exp-(2)Exp-(8)FEM
0.01 0.02 0.03 0.04 0.05 0.060Time (sec)
−0.0004−0.0003−0.0002−0.0001
00.00010.00020.00030.0004
Axi
al st
rain
Exp-(3)Exp-(5)FEM
Back face (P = 0)
0.02 0.04 0.06 0.08 0.10Time (sec)−0.0005
0
0.0005
0.001
0.0015
0.002
0.0025
Axi
al st
rain
Exp-(4)Exp-(6)FEM
Front face (P = 0)
0.02 0.04 0.06 0.08 0.10Time (sec)−0.0004
−0.0002
00.00020.00040.00060.0008
0.0010.00120.00140.0016
Axi
al st
rain
Figure 10: Axial strain-time curves for the longitudinal reinforcement resulting from experimental test and FEM.
10 Shock and Vibration
200 mm
200 mm
4N12
4N12
R8@100 mm
R8@100 mm
200 mm
50mm
800 mm
100 mm
Figure 11: Column sample selected for validation [17].
0
500
1000
1500
2000
2500
3000
3500
4000
Load
(kN
)
5 10 15 200
Axial displacement (mm)
0C01HC01V2HC0
3HC0
(a)
FEEXP.
0 −2 −3 −4 −5 −6 −7−1
Axial displacement (mm)
0
500000
1000000
1500000
2000000
2500000
3000000
3500000
4000000Fo
rce (
N)
(b)
Figure 12: Result of finite element analysis (b) and experimental results [17] (a).
have four steel angles and their maximum displacement isabout 16 and 23mm, respectively.
Based on Figure 14(a), failure mode of RC column with-out retrofitting (Col-0) is brittle and the column’s lateral dis-placement increases dramatically. However, all strengthenedRC columns with steel jackets have more ductile behavior.Belal et al. (2015) demonstrated that specimen strengthenedwith angles or channel sections (Col-1, 2, 3, and 4) recorded ahigher axial strength than that strengthened with plates (Col-5). Moreover, strengthening strategy of Col-4 and Col-1 ismore effective than the other methods [16]. Here, we showedthat Col-3 and Col-4 have the highest blast capacity than theother columns.
Deformations of reinforcing bars for three column mod-els are shown in Figure 15 for better understanding of thecondition of these columns under the effect of blast loading.Figures 15(a) shows the ultimate moments for Col-0 (withoutretrofitting) under blast loading. Also, Figures 15(b) and
15(c) show the condition of steel bars in Col-3 and Col-5,respectively. It is clear that steel reinforcement in Col-3 doesnot have considerable deformations and this leads to highresistance of column under the blast loading. On the otherhand, there are some plastic deformations in bar grids in Col-5.
Figures 16–21 show the graphical stress contours for6 columns. Figure 16 shows bending stress in the col-umn without retrofitting (Col-0). Failure conditions can beclearly observed in this figure. In Figures 17–21, bendingstress contours (left) and Von-Mises stress in steel jackets(middle) and in the column itself (right) have been shownfor 5 retrofitted columns. It is clear that Col-1 (with 3connecting plates) has a lower resistance and has deformedgreater than Col-2 (with 6 connecting plates). Given thefact that columns are fixed at both ends, upper and lowerparts of the columns have more critical conditions. Othercritical conditions have occurred in connecting plates in
Shock and Vibration 11
Col-1
0100000200000300000400000500000600000700000800000900000
Shea
r for
ce (N
)
−5 −10 −15 −20 −250
Mid height displacement (mm)
Col-3
0
100000
200000
300000
400000
500000
600000
700000
800000
900000
Shea
r for
ce (N
)
−1 −2 −3 −40
Mid height displacement (mm)
Col-5
0100000200000300000400000500000600000700000800000900000
Shea
r for
ce (N
)
−3.5−1 −1.5 −2 −2.5 −3−0.50
Mid height displacement (mm)
Col-4
0100000200000300000400000500000600000700000800000900000
Shea
r for
ce (N
)
−5 −10 −15 −20 −25 −300
Mid height displacement (mm)
Col-2
−5 −10 −150
Mid height displacement (mm)
0
100000
200000
300000
400000
500000
600000
700000
800000
900000
Shea
r for
ce (N
) Col-0
−50 −100 −150 −200 −250 −3000
Mid height displacement (mm)
0
100000
200000
300000
400000
500000
600000Sh
ear f
orce
(N)
Figure 13: Results of shear strength of columns.
columns with perforated retrofitting. For instance, the mid-dle plate in Col-2 and Col-3 has experienced less von-Mises stress, while other two plates have critical state ofstress.
7. Residual Axial Strength
Axial capacity of columns before and after blast loading candefine residual axial strength of the column. Residual axialstrength is a very important parameter for estimating theoverall behavior and progressive collapse of the buildingsunder the blast loads. Given that residual axial strength isindependent of the mode of behavior of the structure, itcould be the best criterion for defining damage level of
the columns after blast loading [3, 10, 26]. In this paper,after analysis of FE models under lateral blat loading, acompressive uniform axial pressure was applied on one endof the column and failure of the column, ultimate axial load,and its deformation were investigated. In Table 3, 𝑃𝑢0 axialstrength of undamaged RC column (before blast loading) and𝑃𝑢1 axial strength of damaged column are summarized. Here,axial strength is assumed to be an axial load level in whichby 1% increase in load, displacement increases more than10%.
According to Table 3, Col-4 and Col-1 undamaged col-umn models have the highest axial capacity. Then, there areCol-2 and Col-3 and the lowest undamaged axial capacity isobserved in Col-5 model. After applying blast load, Col-0,
12 Shock and Vibration
−10
0
10
20
30
40
50
60La
tera
l disp
lace
men
t (m
m)
0.05 0.1 0.15 0.20Time (sec)
Col-1Col-2Col-3
Col-4Col-5Col-0
(a)
−5
0
5
10
15
20
25
Late
ral d
ispla
cem
ent (
mm
)
0.05 0.1 0.150Time (sec)
Col-1Col-2Col-3
Col-4Col-5
(b)
Figure 14: Lateral displacement of column’s middle height.
S, max. principal(Avg: 75%)
0.00044.02488.049132.073176.097220.122264.146308.170352.195396.219440.244484.268528.292
(a)
S, max. principal(Avg: 75%)
0.00030.08060.16090.240120.321150.401180.481210.561240.641270.721300.801330.882360.962
(b)
0.00030.13760.27590.412120.550150.687180.825210.962241.100271.237301.375331.513361.650
S, max. principal(Avg: 75%)
(c)
Figure 15: Deformations of steel bars in (a) Col-0, (b) Col-3, and (c) Col-5.
Table 3: Failure loads of the columns.
Model 𝑃𝑢0 (kN) 𝑃𝑢1 (kN) 𝑃𝑢1/𝑃𝑢0Col-0 1231 — —Col-1 1897 380 0.2Col-2 1684 791 0.47Col-3 1627 1506 0.92Col-4 1873 1762 0.94Col-5 1524 990 0.65
which is unstrengthened, has lost its whole capacity.The leastdecrease in axial capacitywas observed forCol-4 andCol-3 (6
and 8%, resp.). Axial strength of Col-1 andCol-2 has intenselydecreased (80 and 53%, resp.). Buckling of the steel anglescould be the reason for this phenomenon.
In Figure 22, deformation shapes of the blast damagedcolumns under axial load, near the failure state, are shown.According to Figure 22, failure mode in Col-1, 2, 3, 4, and5 is close to the column’s head. However, in Col-0 (withoutretrofitting), failure occurs through the whole height of thecolumn.
In Figure 23, axial load-displacement curves, after andbefore blast loading, are drawn. According to Figure 23,residual axial strengths for Col-1 and Col-2 are 𝑃𝑢1 =380 and 791 kN and corresponding axial displacements are
Shock and Vibration 13
S, S33(Avg: 75%)
−19.222−17.623−16.024−14.426−12.827−11.228−9.629−8.031−6.432−4.833−3.234−1.635−0.037
Figure 16: Bending stress in Col-0.
S, S33(Avg: 75%)
−15.445
−14.090
−12.734
−11.379
−10.023
−8.668
−7.312
−5.957
−4.601
−3.246
−1.890
−0.535
0.821
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
46.430
73.442
100.455
127.468
154.480
181.493
208.506
235.518
262.531
289.544
316.556
343.569
370.582
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
0.189
31.055
61.921
92.787
123.653
154.519
185.385
216.251
247.117
277.983
308.849
339.715
370.582
Figure 17: Stress contours in Col-1.
𝛿𝑢1 = 3.2 and 4.79mm, respectively. It should be notedthat deformation of Col-1 is increasing rapidly. In contrast,these values for the undamaged models are 𝑃𝑢0 = 1897 kN,𝛿𝑢0 = 1.18mm and𝑃𝑢0 = 1684 kN, 𝛿𝑢0 = 2.04mm, respectively.Hence, dramatic decrease in axial capacity and increase indeformation in Col-1 and Col-2 are obvious. In Col-3 andCol-4, which are strengthened by steel channels, maximumaxial loads and corresponding deformations, after blast load-ing, are 𝑃𝑢1 = 1506 kN, 𝛿𝑢1 = 2.01mm and 𝑃𝑢1 = 1762 kN,𝛿𝑢1 = 1.27mm, respectively. For undamaged column modelsCol-3 and Col-4, maximum axial loads and correspondingdeformations are 𝑃𝑢0 = 1627 kN, 𝛿𝑢0 = 1.84mm and 𝑃𝑢0 =1873 kN, 𝛿𝑢0 = 1.37mm, respectively. For Col-5, the differencebetween the axial capacity and corresponding displacement,
before and after blast loading, is more than Col-3 and Col-4models (𝑃𝑢1 = 990 kN, 𝛿𝑢1 = 3.65mm and 𝑃𝑢0 = 1524 kN, 𝛿𝑢0= 2.11mm).
8. Conclusion
In this study, the performance of simple and steel jacketstrengthened reinforced concrete columns has been evalu-ated under the effect of blast transverse loading. It should benoted that all of the strengthening configurations originallyare used for enhancing the axial capacity of RC columnsunder pure axial loading. Here, the effectiveness of thosestrengthening methods on explosion capacity of the RCcolumns was investigated. Finite element method (FEM) was
14 Shock and Vibration
S, S33(Avg: 75%)
−17.019
−15.509
−13.998
−12.487
−10.977
−9.466
−7.955
−6.445
−4.934
−3.423
−1.913
−0.402
1.109
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
10.514
40.939
71.364
101.788
132.213
162.637
193.062
223.487
253.911
284.336
314.760
345.185
375.609
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
0.482
31.743
63.003
94.264
125.525
156.785
188.046
219.306
250.567
281.828
313.088
344.349
375.609
Figure 18: Stress contours in Col-2.
S, S33(Avg: 75%)
−11.063
−9.963
−8.863
−7.763
−6.663
−5.563
−4.463
−3.363
−2.263
−1.163
−0.064
1.036
2.136
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
10.479
39.912
69.345
98.779
128.212
157.645
187.078
216.511
245.945
275.378
304.811
334.244
363.677
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
0.774
31.016
61.258
91.500
121.742
151.984
182.226
212.468
242.710
272.952
303.193
333.435
363.677
Figure 19: Stress contours in Col-3.
presented for analysis of models using ABAQUS softwarepackage. A real scale blast loading test was done by theauthors and its results are used for validating FE modelingand analysis process. The test included four RC memberswith the same geometry and reinforcement details wheretwo samples have initial axial force and two other sampleshave no axial force. FE modeling of the samples underblast loading showed a good agreement with experimentalobservations. Afterward, FE modeling process was used foranalysis of steel jacket retrofitted columns under lateral blast
loading and postblast condition. According to the obtainedresults, simple columnwithout retrofitting hasmuch less blastresistance compared to retrofitted columns.Thus, retrofittingcolumns with steel jacket can greatly improve the resis-tance of columns against explosion loads and extremelyenhance residual axial capacity of the RC columns after blastloading.
Retrofitting method with steel channels and connectingplates (Col-4) can be used as an effective way to simulta-neously enhance axial and lateral blast resistance of the RC
Shock and Vibration 15
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
46.153
80.675
115.197
149.719
184.240
218.762
253.284
287.806
322.328
356.850
391.371
425.893
460.415
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0) S, S33
(Avg: 75%)
−21.349
−19.441
−17.533
−15.625
−13.717
−11.808
−9.900
−7.992
−6.084
−4.176
−2.268
−0.360
1.548
0.586
38.905
77.224
115.543
153.863
192.182
230.501
268.820
307.139
345.458
383.777
422.096
460.415
Figure 20: Stress contours in Col-4.
S, S33(Avg: 75%)
−20.749−18.954−17.159−15.364−13.570−11.775−9.980−8.185−6.390−4.595−2.800−1.0050.790
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
44.74071.16197.583124.005150.426176.848203.269229.691256.113282.534308.956335.377361.799
S, Mises
(Avg: 75%)SNEG, (@ L;=NCIH = −1.0)
0.21330.34560.47890.610120.742150.874181.006211.138241.270271.403301.535331.667361.799
Figure 21: Stress contours in Col-5.
columns. Although strengthening with steel angles (Col-1and Col-2) has enhancing effects on axial capacity, theyare the least effective ways for enhancing blast resistanceof the columns. Hence, we can say that deformations ofthe RC columns under blast loading have the lowest level
in retrofitting with steel channel sections compared to steelangles. This fact leads to higher residual strength capacityof the columns strengthened with steel channel sections.However, buckling of the angles under axial load decreasesthe axial strength of the column. Given the fact that both
16 Shock and Vibration
Col-4 Col-5
Col-2 Col-3
Col-0 Col-1
U,U2
−5.929e + 00−5.412e + 00−4.894e + 00−4.377e + 00−3.859e + 00−3.342e + 00−2.825e + 00−2.307e + 00−1.790e + 00−1.272e + 00−7.547e − 01−2.372e − 01+2.802e − 01
U,U2
−2.008e + 00−1.838e + 00−1.667e + 00−1.497e + 00−1.326e + 00−1.156e + 00−9.855e − 01−8.150e − 01−6.446e − 01−4.741e − 01−3.037e − 01−1.332e − 01+3.724e − 02
U,U2
−3.547e + 00−3.249e + 00−2.951e + 00−2.654e + 00−2.356e + 00−2.058e + 00−1.761e + 00−1.463e + 00−1.165e + 00−8.677e − 01−5.700e − 01−2.723e − 01+2.534e − 02
U,U2
−1.324e + 00−1.204e + 00−1.084e + 00−9.647e − 01−8.450e − 01−7.252e − 01−6.055e − 01−4.858e − 01−3.660e − 01−2.463e − 01−1.266e − 01−6.833e − 03+1.129e − 01
U,U2
−4.785e + 00−4.371e + 00−3.957e + 00−3.543e + 00−3.128e + 00−2.714e + 00−2.300e + 00−1.886e + 00−1.472e + 00−1.057e + 00−6.432e − 01−2.290e − 01+1.852e − 01
U,U2
−1.047e + 02−9.584e + 01−8.696e + 01−7.807e + 01−6.918e + 01−6.030e + 01−5.141e + 01−4.252e + 01−3.364e + 01−2.475e + 01−1.586e + 01−6.978e + 00+1.908e + 00
Figure 22: Deformation of damaged columns at failure load.
ends of columns have been assumed to be clamped, the mostcritical points are located in those areas under blast loading.This critical condition was observed in Col-1 (strengtheningwith steel angles) and Col-3 (strengthening with steel chan-nels) which have 3 connecting plates in two upper and lowerplates.
Generally, it can be said that the results obtainedfrom FEM have been very useful and can have acceptable
precision in comparison with experimental test data. Pos-sible differences between finite element analysis results andexperimental observations are due to laboratory errors andequipment failure under blast pressure, assumptions ofhomogeneity of materials, lack of accurate estimation ofexplosion loads on the structures, and the difference betweenthe actualmechanismof interaction between steel reinforcingbars and concrete. In general, retrofittingwith the steel jackets
Shock and Vibration 17
Col-1-undamagedCol-1-damaged
0.5 1 1.5 2 2.5 3 3.50Displacement (mm)
0200400600800
100012001400160018002000
Load
(kN
)
Col-2-undamagedCol-2-damaged
1 2 3 4 5 60Displacement (mm)
0200400600800
10001200140016001800
Load
(kN
)
Col-4-undamagedCol-4-damaged
0.5 1 1.5 20Displacement (mm)
0200400600800
100012001400160018002000
Load
(kN
)
Col-3-undamagedCol-3-damaged
0.5 1 1.5 2 2.50Displacement (mm)
0
200
400
600
800
1000
1200
1400
1600
1800
Load
(kN
)
Col-5-undamagedCol-5-damaged
1 2 3 4 50Displacement (mm)
0200400600800
10001200140016001800
Load
(kN
)
Figure 23: Axial load-displacement curves for the columns before and after blast loading.
would cause a large improvement in the performance ofRC columns under the blast loading and their residual axialcapacity after blast event.
Conflicts of Interest
The authors declare that there are no conflicts of interestregarding the publication of this paper.
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