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A‘ of:1:1r1:'<?:;E1:=:l>';§;':':1:I£:2=5:§:i:I:F:l:EI:7 --=:=E=E=2=EIi=:sE=:=5I:1;-:€¢:i=:=:=E=}=:=:=:=====-215:. ;=>.e=:;;:;> -=v.-:"<1:=-=:1.=--:.= I.>¢1:12er -'<‘-:=:=:=:=:=;=$:z?£=:€%=:=:$§Fii:1-'.':=-=:=-=:=-=:I Susumu INOUE Toyoaki MIYAGAWA Manabu FUJII We investigate the effects of mechanical degree of prestress, volumetric ratio of lateral confinement, concrete compressive strength, steel index, and shear span effective depth ratio on the energy dissipation properties of partially prestressed concrete beams under different loading histories. The relationships between these test variables and non—dimensional dissipated energy are derived based on the test results. Results indicate that seismic damage to partially prestressed concrete beams can be evaluated quantitatively using a proposed damage index based on hysteretic dissipated energy. Keywords: partially prestressed concrete, non —dimensi0nal dissipated energy, loading history, mechanical degree of prestress, volumetric ratio of lateral confinement, damage evaluation Susumu Inoue is Associate Professor of Civil Engineering at Osaka Institute of Technology, Osaka, Japan. He received hisDoctor of Engineering Degree from Kyoto University in 1994. His research interests include the ductility improvement of reinforced and prestressed concrete members and seismic damage evaluation of concrete structures. He is a member of the JSCE, JCl, and JSMS. Toyoaki Miyagawa is Associate Professor of Civil Engineering at Kyoto University, Kyoto, Japan. He received his Doctor of Engineering Degree from Kyoto University in 1985. He is the author of a number of papers dealing With the durability of reinforced concrete structures. He is a member of the JSCE, ACI, JSMS, and a number of technical committees. Manabu Pujii is Professor of Civil Engineering at Kyoto University, Kyoto, Japan. He received his Doctor of Engineering Degree from Kyoto University in 1972. His current research activities are focused on the optimal design of prestressed concrete cable—stayed bridges, structural safety evaluations, and the durability of concrete structures. He has written some 50 papers on these subjects. He is a member of the JSCE, ACI, JCI, JSMS, and a number of technical committees. "~l51— 1. INTRODUCTION It is very importantto be able evaluate seismic damageto concretestructuresquantitativelyand preciselyin order to judge the serviceabilityof suchstructuresafter an earthquake,and theneed for repair and/orstrengthening. In general,seismicdamageisjudgedmainlyby a site inspectionof the damagedstructures.Basedontheresultsof suchinspections,theresidualdeformabilityof the damaged structuresis evaluated along with the maximumresponsedeformation[1]. The safety of concrete structuresunderseismicloadingisusually estimatedfromthe deformationductility,so it is important to relatethe degreeof damageto the residualdeformability. It is alsowell known that the ductility of concretemembersunder reversedcyclic loadingsuch as experiencedduhg anearthquakeissigniBcantlylowerthanthatundermonotonousloadhg. Thisimplies thatseismicdamageto concretestructuresandmembersshouldbeevaluatedby takingintoconsideration damageaccumulationdue to cyclic loadreversalsandrepetitions. This situationhasledto certaindamageindexesthattakeintoaccountthedamageaccumulationduring earthquakesbeingproposedbased on hystereticenergydissipationor low-cycle fatiguelaw [2, 3, 4]. However,these damageindexesarebased on test results forreinforcedconcrete(RC)membersand they do not cover the case of partially prestressedconcrete(PPC) or prestressedconcrete (PC) members. PPC structureshave attractedattentionrecentlyfor the high degreeof freedomtheygive designersand they are often used for memberssubjectedto earthquakeloading as structuralbeams. However,theenergydissipationpropertiesof PPCmembersare affectedby many factorsas compared with RCmembers.Consequently,it is necessaryto quantitativelyclarifythe effectsof thesevarious factorson energydissipationin orderto makepreciseevaluationof damageduring earthquakes. In thispaper,the effectsof variousfactorson the accumulationof dissipatedenergyin PPC beamswhichulthately failin flexureunderreversedcyclicloading- arediscussedbased on resultsobtained inexperimentsdoneby theauthors[5-10]. h addition,a newdamageindexbasedon the total energy dissipatedup to theultimatestate is proposed. 2. EXPERIMENTAL PROCEDURE 2 .1 Test Variables A largenumberof factorshave an inhence on the energydissipationproperties of PPC beams. In this paper, however, the following five test variables, which are expected to have a relatively large influence, are selected: a) Volumetricratio of lateral confinement( p s) The volumetricratio of lateral confinementp sis definedby the equation P s= volumeofone transeverse hop X loo (%) volume ofcoreconcreteconfinedby onehop (1) b) Mechanicaldegreeof prestress ( A) Themechanicaldegreeof prestress A is definedas a =__A A, tv'AB fsy (2) Where, gyp:: yalfeelad OsftrpernegsttEeSsflpnrge sSttreeesls lngSteel A s:area of non-tensioned deformed bar fsy:yield strength of non-tensioned deformed bar -152- c) Concrete compressivestrength(fTc) Table 1 Details of Test Variables d) Steel index (q) The steel index q is defined as Equation (3). S e ri e s - A S e r ie s - B S e ri e s - C S e ri e s - D p s (% ) 0 , 0 .6 , 1 .2 , 2 .4 0 .6 , 1 .2 , 2 .4 0 .6 , 1 .2 , 2 .4 0 , 0 .6 , 1 .2 , 2 .4 A 0 .4 , 0 .7 , i .0 0 ,4 , 0 .7 , 1 .0 0 .4 , 0 .7 , 1 .0 0 .4 , 0 .7 , 1 .0 4 0, 80 40 4O 4 0, 80 5 ,8 ,10, 12,2 3 5, 8, 12 5 ,8 , 12 5, 8 ,1 0, 12 ,2 3 flc (M P a ) O I c, q-qp.%=#.# (M P a ) ∼ q 0 .2 , 0 .2 5 , 0 .3 , 0 .2 5 , 0 .3 0 .2 5 , 0 .3 0 .2 , 0 .2 5 , 0 .3 a /d 2 .3 , 2 .9 , 3 .5 2 .3 , 2 .9 , 3 .5 3 .5 3 .5 nu m b er o f 63 l9 9 24 (3, Where, b: widthof cross section s p e c im e n s a cTcp:introduced prestress dp.'s;effe?ctive depth of prestressing ds:effectivedepthof non-tensioned deformedbar flc:compressivestrength of concrete e) Shear span- effectivedepth ratio (a/d) Detailsofthe adoptedvaluesof thesetestvariablesarelistedin Table 1 for each series of loadingtests. In all test specimens,the tensile stress in the prestressingbars immediatelyafter prestressingwas laSdjaustperdof3Beat7e?y%50iFae,h8t&n;=,e aSnkdenlgFhAccfO.rrd %g='.y :.t?a.1ftar:ddulC.e.? reefsf;cetcitvi: ePlry: SEetsEelncaCsOen C.rfe;ec =40MPa. On the other hand, the introduced prestressin specimens with fc=80MPa is 10MPa and 23MPa for A =0.4 and 1.0, respectively. 2i23p9dfBSBS b Specimens used for the loading tests were simplebeamsof partially prestressedconcrete, includingalso fullyprestressedconcretebeams, with a rectangularcross section ofb x h = 10 x 20cm (b:width,h:full depth of section) and a totallengthof 160cm.As shown in Fig.1, they were symmetrically reinforced with prestressingbarsandnon-prestressingdefomed bars. The effective depth of the lower a a no n -te n sio n ed ba ( 2 v / EL Jl ..J ] 33 1 Jtl pre i stre ssing ba r a I v tl tT b=400mm, c=200mm for a/d=2.3 b=400mm, c=100mm for a/d=2.9 a=600mm, b=200mm, c=100mm for a/d=3.5 46 80 O1 n 3 I O OtL) a) O O CU r 1DD 100 46 L E Ll un it:m m =400mm, 80 I K a=500mm, 100 T1 2 Ei a a LL> 0 1 46 80 0 Q V) I p;iBecs:tu9;sefi3ftShfBlin'eg=dff'i1;ndlea5a:3nSi10,n lt were used to fabriaa) - case, the real value rcoa7end.hbearsst e(fesf-c4a9g5eT[TE?s with the JSCE.s Standard Specification for Design and Constructionof ReinforcedConcrete Structuresin orderto prevent premature shear failure. As prestressing steel, round prestressingbars (SBPR A-1, B-1 and C-1) wereused in all specimens.Theseprestressing -153- Ago. BO a a) a 7 Q JL> 0 O 0 a ∼ 0 a 1 +13 1l 1050N/rnm2 I fpy=1 1 20l l 70N/mm2 loo Q LO a r- P1 0 a •` 0 a 80 4I6 O 7 $13 I 0 Q i LE> rQ C) CU A3 % DID 1=8:i? J3 Q OJ 1 A:B: 3S +6 O 1 f" - r--r 4I9. 2 PIS fpy= 1270N/mm2 71 00 80 +6 ., 1 0 LI e % 0 a - 0 m2 100 (fRV=495N/mm2) were used. The spacing of the Q Q CU DID i 93 i t .fp3y3=.1; /0; ioir.Chemeln3,5o"mm hooks rectangular at the closedcorners hoops - r- ill ll 0 A:S.: g?9 of A isslightlyshaller !;0.f7:seisdee%6gih= longitudinalreinforcingt2fafne bars. As lateral confinementand shear rein- reinforcementwas chosenin accordance Sfhs;=af C) CO fpy= 920 N/mm2 Fig.1 Dimensions of Specimens 1 :poy9- 0 N /m m2 ,agsuteTer;ithPOScte-ieennstionpeaSte an.df los,-(x8y, g W/C=45 %. OSItlvo(xby) J ¥2 I A + -1 cyc(a i 2 i3W 3l In this paper, the following four loading histories are adopted in order to investigatethe effectsof loadinghistoryon energydissipation properties. negatlve pos(uve(xby) P 5 4 > i 9 2 I J) 3 2 i 8 + 3 cycle negative (a) Series-A cycle 3 TB -l <J 3i] r)cgatfvo (b) Series-B posJtJvoxby) ( (c) Series-C 10cycles a) Series-A cycle Series-A consists of gradually increasingreversedcyclicloading with one load reversal at each denectionamplitude.h this series, negauve (d) Series-D Fig.2 Applied I,oading Histories fsh egraapdS ill?yd idnec?eeacst1?d? e.agTf lgTd(e( eaarsr;f;ge.cg;piac6ify( if it dyiecledddte.n8e.CZ?.ni ,th2e6&,a3x i6myL A.lu.PaLo( t6h :).diflh : C;1i:1nd ad=RleiE;idoei wherethe load E &omthe measuredload-deflectioncurve and is somewhatlarger thanthe calculated v6afuies ,oBt?i_?,ed? using thebaaC,tsu actual yieldssttrreesnseihg strength obfa,tsh of theeh::1ffa?,recamdgy reinforcing byTerlSdaenddafrei bars-andpre_stressingbars. tdhearti;zqhb,ye iunSf1.nrgcltnhge :Ldyiside iahliuseiiglXICea;) U b)Series-B Series-Bconsistsofgraduallydecreasingreversedcyclicloadingwithone loadreversalat eachdeflection amphtude,inwhichthe apphed deflectionamplitudeis gradually decreasedfrom 6 uto 6 y.The sum of the applieddeflectionamplitudesis adjusted to equal that of Series-A. c) Series-C Series-Cconsistsof mixedSeries-A andSeries-Bloading'in which the applied deflectionamplitude isbst graduallyincreasedup to 6 uandthen graduallydecreased.The sum of the applied deflection amplitudesin Series-C is also equalto that of Series-A. d)Series-D Series-D is graduallyincreasingreversed cyclicloadingwith ten load reversalsat each deflection amplitude. Theseloadinghistoriesare shownschematicallyin Fig.2.Specimenswere tested under symmetrical two-pointloadingwith various shearspan lengthsandflexural spanlengthscorrespondingto the a/d ratio.Aner the prescribedloadingsequences,all specimensweresubjectedto additional loadingcycles untiltheir load carrying capacity fell to approximately509To of the maximum. 3iBBSiiW 3-iBBBAhiQABiBs* It isnecessaryto dehe theultimatestateof membersif seismicdamageto concretestructuresis to be evaluated.In this paper,the ultimatestateis definedas thepointat whichthe load carryingcapacity has fallento 80% of the maximumload.All testedspecimensreachedtheir ultimatestate as a result of crushhgandspaningof concretewithinthenexuralspanas morecycleswere appliedafteryielding of the tensilereinforcement. -154- a;30 B20 i 0 A H15 D V J=0% p._-0.67% p '=1.93% p._-2.68% •`Q Ql 0:.LEO.94 0 J= I) gpo Jb 0: ^=0.50 ^=o.70 ^=0.89 %25 I SSb5 Q Z= B 15 2 3 4 5 6 7 8 9 defleetlon, 101112 i A I-0.94 : f''--8QNP&, s:y5 EsR5 5 yO A_-o.43 A _-o.60 ^=o.89 : 1''=80NP&, S510 a) q S 1''=40NF'&, A : (''=40NF'&, + •`i520 •`E I b i1 10 a 1 525 A: 0: V: l•` L q3 J= J=Ql20 S5 vO 5 30 0 : ^=o.43 p 1 2 3 4 6/6yo'l 5 6 7 8 deflectlon, 9 1011 12 -0 1 2 3 4 6/6yo'I 5 6 7 dof/ect]on, 8 9 101112 6/6yc'( Fig3 Effects of ps on EdTValue Fig.4 Effects of A onEdTValue Fig.5 Effects of fTcon EdTValue (Series-A, A =0.70) (Series-A, p s%2.50%) (Series-A, p s%1.25%) On the other hand, the dissipated energy at each deflection amplitude Pd) is equal to the area surroundedby each loop in the load-deflection hysteresis.Dissipatedenergy itself,however,varies greatlyunderdifferentloadingconditionsforthe samesection.Therefore,non-dimensional dissipated energyat each deflectionamplitude(Ed')is definedin this paper as follows, Ei- B:a (4) P ycd 6 ,cd are the calculatedyieldloadand yield deflectionof each beam, respectively.This tahnedef6flgt zh&rien,aEgg of differencesin maximum load carrying capacityamongthe beams. 3 i2BfkGtS_Qf3ksi* a) Effectsof volumetricratio of lateral confinement( p s) Figure 3 showsthe effectsof volumetricratio of transversehoops ( p s)on the energydissipationof Series-A beams; the horizontal axis represents non-dimensional applied deflection amplitude and the vertical axis is the non-dimensional dissipatedenergy PdT)at each deflection Esp/ lfticda2. As Fig3, the Eatvalueincreasesalmostlinearlywith increasingdeflectionamplitudewithin the range ofrelativelysmall applieddeformationandthe rate of increaseis almostconstantirrespectiveof p s vha.1xeevgelrV,esnt ihpast lTcer:2siLgeStr vb=3:Sets.wdee S?eeassaema?.sTmha?lE,d IdVeai::t19.fnaab=;HtuwdiiE. aTShTsailsl ebre cPasu;ealtuhee, beamswith a smaller p svalueexhibitsigniBcantstrengthdegradationat smallerdeflectionamplitudes, resultingin reduced energy dissipationlater.In other words,the point afterwhich the qTvalue does not increase linearlycan be correlatedwith a point of significantstrengthreduction - that is, the ultimatestateof the beam. b) Effectsof mechanicaldegreeof prestress( A) Figure4 showsthe effectsof mechanicaldegreeof prestress( A) on Ed'Valuesfor beamswith p sof approximately 2.59To. As seen in this figure, for the particular deflectionamplitude, the Ed' Value EEcaol=fswslThanhe:r:its?n%cr^e?smg "hs isbecause theareaenclosed byeachhysteresisloopbecomes c) Effects of concretecompressivestrength (fc) Figure5 showsthe EdTvaluesof the beamsmadewith concreteof different compressivestrengths.The Ed Value of the flc=40MPabeam is somewhatlarger than that of the flc=80MPabeam at the same -155- a;30 B30 525 : q=o.257 + : q--0,434 0 %25 ko •`igpo gy5 a/a_-2.33 a/d=2.91 / / ,U a/d=3.49 -I.-A gy5 S510 S._q10 gas vO 0 A 0 EB5 1 2 3 4 5 6 7 deflectlon, 8 9 101112 ,0 1 2 6/6yc'I 3 4 5 6 7 deflect(on, 8 9 1011 6/ 12 6yc.'l Fig.7 Effects of a/d on Ed' Value Fig.6 Effects of q on Ed' Value (Series-A, A %0.45, ps%2.50%) (Series-A, A =0.46, p s=2.43%) d enectionamplitude.However,the A value of the former is 0.43 (0.89) and somewhatsmallerthan thatof the latter,whichis 0.50(0.94).Therefore,consideringthe differencein A value betweenthese two beams, the effect of concrete compressive strength can be seen to be smaller than that of volumetricratio of lateralconfinementand mechanicaldegree of prestress. d) Effects of steelindex (q) Figure 6 showsan exampleof Ed'Valuesof beams with differentsteel indexes; that is, q=0.257and 0.434. The Bgureindicatesthat the Eatvaluesof these two beams at the same deflectionamplitudeare almost equal.Therefore,the effects of steel index on the non-dimensional dissipatedenergy can be consideredto be negligibleif the othertest variables are the same. e) Effects of shear span-effective depth ratio(a/d) In Fig.7,Eatvaluesof beams loaded under differenta/d ratios are shown. The Eu'value at a particular non-dimensionaldeflection amplitudeis almost the same irrespectiveof the a/d ratio. With different a/d ratios,the acting shear force differseven if the applied deflectionamplitudeis the same. In these tests, however, each specimen was reinforced accordingto the maximum shear force, so energy dissipationpropertieswere almost identicalsince flexure is more predominantthan shear. This result impliesthat the effectsof a/d ratioon non-dimensionaldissipatedenergyare smallif a beamis designed to fail in flexureeven when loaded under a smallera/d ratiowithin the range of 2.33-3.77 adopted in thesetests. 3i3W Fromtheresultsof the Series-A tests,it is clear that the effectsof concretecompressivestrength,steel index,andshearspan-effectivedepthratioon the accumulationof non-dimensional dissipatedenergy are relativelysmall as comparedwith volumetricratioof lateralconfinementand mechanicaldegree of prestress. Here, then, the process of non-dimensional dissipatedenergy accumulationup to the ultimate state under different loading histories is discussedmainly in the light of the effects of mechanicaldegreeof prestress andvolumetricratioof lateralconfhement. a) Series-A b etweennon-dimensionaldissipated energy(Eat)and normalized LeHdtBo(ns7p6S TppFiea8daeraeScht?.wnnEep ycal)for the Series-A beams. The Ed'Value of each Series-A beam i ncreases almost linearlywith incJr-6-asing applied deflectionamplitudeup to the ultimate state.As previously shown in Fig3, the volumetric ratio of lateral confinementaffects only the deflection amplitudeat the point where the EdTvalue stopsincreasinglinearly,that is, at ultimatedeflection.On the other hand, the gradient of the initial linear section is affected by the mechanical prestress,made clearby Fig.4. Consideringthese results,the relationshipbetweenEdTand 6 /dBgyrc?1 eCaOnf be expressedin linear form as follows. -156- 1 LLl I i;3 LLJ t Jt --- : t71eaSured : c&fculated + 5 ig: f 0 g!1 / 5 / 7Q i.,_EL 5B 5 C b + : measured A •`/+- H 75 .'' I .+ 5B ,+I I:i ¥f 7 (a) A =0.46 2 + -.-- : m8&Sured : c&Icu[&1ed 6 4 /,..'' ,i.,J'' T 8 9101112 deffectlon, 6/ 6yc'I e %gg 5 J= 't} ,f 1 23456 ,+. / Z=S S5i 10 H :i ---- : eelctlla(ed gb 1Q qb •` .8' A C 3 4 5 6 deflectlon, b (.-,t'- ' 2 7 8 9 6/ 61C'I 3 ' 4 deflect/on, (b) A =0.71 5 6 6/ 61C-I (c) A =0.87 Fig.8 Examples of Relationships between EdTand 6 / 6 ,cat(Series-A, p s-2.43%) t3 A A - - C Q •` i o 5i a2 •` Q Q 0 1 •` •`t> S-1 .•`.......I.@..g. 8 Q t> -2 1 .;i-..,.......8s....--.-a.i' OOO -3 0 e) -4 0.3 0.4 0.5 0.6 0.T 0.8 0.9 1.0 meobanfcatdegree of prestress, 1 (a) coefficient a 0 .3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 mechanlc&( degree of prestress, 1 (b) coefficient B Fig.9 Relationships betweenCoefficients a , B , and A Ei-a73=.B (5) (626ycd, Where, a and B are functions of the mechamicaldegreeofprestress A. and (b), respectively. ;Bee rceiaeff7:fehiss baeTnedenF;ncgeq%c;ean,tS aas ;uBm,eTtdo ^b ealrien S2roTn1:;i :igss;9f-ia,) although some scatter is observed.ney can be expressed as in Eq.(6) and Eq.(7) from a regression analysisTofthe test data. oc--2.43 A.3.25 a-4.17^-4.15 (0.43 S^So.94) (0.43 S^S (6) o.94) (7) Figure 8 also shows calculatedE; values derived&omthe regressionanalysis mentionedabove.As indicatedin Fig.8,the calculatedvaluesderived from Eq.(5)-Eq.(7) coincidewell with the measured values.In somebeamswith larger A values,however,the differencebetweenmeasured and calculated EdT valuestendsto be greaterinthe largerdeflectionamplituderangenear the ultimatestate dueto the instabilityof the dissipatedenergy. b)Series-B Figure10showssomeexamplesof the relationshipsbetweenEd'and 6 / 6 ycdfor the Series-B beams. -157- a2 L= 30 + : me&9ured h J{ -M_ : C&lculafed •`ii22: : me&9ured _", : c&lcul&(ed 5 gg!7 ¥i !g':i !g 'A : measured !f:8 ^' A / !f2 5 7 2 6/ 6yQ'I 9 4 5 6 de(Iect/on, (a) A =o.46 I:I C b ,.4.,'' 89701112 deflectlon, + _-.. : ealeulaled / 0 J= I 34567 A + tiE7 A g!15 iE 70 A T 8 9 2 6/61O'E A 9 4 dQ(Ieetlon, 5 6 6/61C'I (c) A =0.87 (b) A =0.71 Fig.10 Examples of Relationships between Ed. and 6/ 6 ycal(Series-B, p s-2.43%) In Series-B, the Eat Value is found to decrease tt 0.6 S,0.5 aaLm,ohSLdqeu ;sd;taidCua!lnyy%e,neEe: dafrpolie d6due.nTehCit!Oi: •` becauseno new cracks occurfor deflectionamplia o.4 fudessmaller than 6 uwhen deflection amplitude 0 : ^=o.46 q th lS gradually decreased, so there is less dissipated energy than in corresponding Series-A beams at the same deflection amplitude. Therefore, the relationship between EdTand 6/6ycal can be written as Eq.(8). q) 8 0.3 a 0.2 (626ycal, •` %1& 3 4 5 6 T 8 9 107112 6 H&X/ Fig.ll J ^=o.87 A 'S' The value of the coefficient 7, is affected by the A value and the maximumdenection amplitude ^=0.71 D: 0.1 1 2 Ei-y(i)2 A: 6 yc.I RelationshipbetweenCoefficient r and 6max/6ycal A edTceatfirdS LcZlsef1(g6urmg: 't.hFei g7ur: all:eShd:Trsei!eesraellslfsTsihnifnbveeTee;;ocpo.edfftci etn.t arm:7d? ,?alTaxiE faaf tees beamstested,the equationsbelow are obtainedfromregressionanalysisof the experimentaldata. v =1.494 y =1.488 v =0.879 (i=) (i=) +0.088 (^=0.46) (9) +0.088 (^=0.71) (10) (^=0.87) (ll) (k) +0.036 Figure10 alsoshowscalculafedEd'Valuesat each deflection amplitude derived from Eq.(8)-Eq.(ll). Lh.e;slrcEtaatAds Ewditvhal^u e-s.?80TiCsi dne.twaesl lg:Atdh :5eth=teafS:re^m=e.T.s; aalihdO.u.g,h1. tThhei:qsreL?ienT; bbeeTaeues: fE: relativereductioninEatvalue&omthe hst cycleto the secondtends to becomelarger withincreasing A value,while a quadraticreductionrate is assumedin the calculationirrespectiveof A values. -158- a20 i= 30 4L ...__ : caleul&(ed I h! 5522o5 A + i ;U: 1I/ + : 1*e&Sured .-_. : calculated + : :measured ____ c&Ieul&ted !E16 /+I g!15 iE 10 L + : me&sqred ige :8 gin .I.'>/ 7;g5 A, / C b 4 S% .i.:.i}' SB2 a b ¥L../ 2 1 234567 89701112 deflect/ot7, 6/ 6yQ'l 3 4 5 6 7 I78 de(Iect]oT7, (a) A =0.46 1 9 2 3 4 dQflectlon, 6/6ycJl (c) A =0.87 (b) A =0.71 Fig.12 Examples of Relationships between Ed' and 6 / 6 ycal(series-C, 1 72 112 a 8 a 8 L4 A.4 5 6 5/5yc'I p s-2.43%) J= C Q Q •` 4L b Tb ;o ;a •` •` -4 -4 -8 -8 0 _40 _30 _20 _1Q 0 10 20 30 40 50 0 _40 _30 -20_70 0 10 20 90 40 50 DeFlectlon, 6 (mm) Deflectlon, 6 (mm) (a) A=o.70 (b) A =0.89 Fig.13 Examples of Load-Deflection Hysteresis Loops (Sereis-D, P s%2.50%) c) Series-C Esiq?hraet ls:esnhoinws e?idi6A/ eeyaahrse 'aast itohneShd1&Sefcot;otnh3 sslenrireesa-sSd? e8T;LeT5?hbe:hhaaVnidO,r tlhSeatThOaS: it.h,eassatEee dedection is reduced resembles that of Series-B beams. Therefore, the Eatvalue of Series-C beams ;:mad?aetiecXfPurneg;ie.dn aosf a6lin6e;cral fuWTtchtiinoThOefde6fl/eStylCGln31:chrienasfnegd,eeflg;.cii.on hcreasingregionand by a d) Series-D In Fig.13areshownsomeexamplesof load-deflectionhysteresisloopsfor the Series-D beams.Figure 14 gives an exampleof the ratio of non-dimensional dissipatedenergyat the n-th cycle(EdT(D(n))) for each deflectionamplitude to that at the first cycle pat(D(1))). Figure 15 shows the ratio of non-dimensionaldissipatedenergyat the flrStCyclefor each deflectionamplitudeof Series-D beams (Edy(D(1))) to that of the correspondingSeries-A beams at the same deflectionamplitude(Ea(A)). Figure14showsthat the Ed'Valueat a particulardeflectionamplitudedecreaseswith increasingcycles z5ea8d.;Pep.eft ittioaT.atAtthtehfeirds? flc;cctlie? nAaRmef lti;und ;.oafd 1,e6pyg t;Fie.nEsd,I tVhaeluEe; a:atlhuee siesC.0.nic6y.C3oe.hfa;hfaatl laetntLoe first cycle. Almost the same t-endencyis observed aAf the deflecfionuampliludeof 2 6 eltPso;g6h cvIJi ;lnV.aLfTeli^ 7euLT=adu urAg^pVe ;TfAiAounV;A7; sAB&ve&L ;t"s&Lal7A{r. W&LvevJfvLAe ujAeAaAeA;Iiw.vn vaAm•`p fityldue";sv T 3uD8Ath.er •`A6yr ;lelduL more,on the otherhand,the reductioninEdTvalue is somewhatdifferent;the fall in the Eatvalue fryom the bst cycletothe secondis very small,and the total reductionratio afterten cycles is at most 10%. At a deflection amplitude near the ultimate state, such as 6 6y, the Eat value begins to decrease remarkablywith repeated cycles. -159- •` lT •` i ab •` LLJ 1 •` tt 7 .1 I_ •` 0.9 uJb 1.1 tth C a 0.6 •` b 0.5 i L LLJ 0 : ^=o.43, A U V 0 l1 0.8 0.7 L i 1.2 1.Ol 0.4 0 .3 0 : ^=0.43, A : A_-0.70, 1'c=40NP& f'c=40NP& U : A_-0,89, V: ^=0.50, f'c=40NP& f'c=80NP& 0: ('c=80NP& ^=o.94, 1.0 .b 0.9 Lq S 0.8 0 .7 58y 48y 38y 28y 8y 68y (I.=40AIF'& l'c=40NP& Ire_-40NP& f'e=80NF'& f'c=80NF'& A_-0.70, ^=o.89, ^=0.50, ^=o.94, tb 0.2 0.7 a : : : : GA9o Ag Ao Vv 5 0 0.6 10 1 1 10 10 7 1 10 10 1 2 10 n (cycle) 5 6 deFlect]oT1, 7 8 6/6ye'I Fig.14 Changes of EdT(D(n))md'(D(1))with Fig.15 Relationship between EdT(D(1))md'(A) Repeated Cycles (Series-D, p s% 2.509To) and 6 / 6 ,cal fgedreonneectciyocnl eaTfP lbteundeest?.fnqso rreeihuac: d2t6o y,u.p-ts.tp7oe oufl ttihmatat.ef Set.ate;stphznEdLvgalsuee,iOefs _SAribeeSa-mDsbaetatTes same deflection amplitude, as seen in Fig.15. This implies that the energy dissipated at a certain deflection amplitude is influencedby the preceding number of load cycles at smaller deflection amplitudes. Theseresultsallowthe Eatvaluesof beamssubjectedtoreversedcyclicloadingwith 10 loadrepetitions at each deflectionamplitudeto be estimated,as describedbelow. Asmentionedpreviously,Ed'Valuesat a particulardeflectionamplitudedecreasewith increasingload cycles, and the amount of the its reduction is affectedby the applied deflection amplitudeand the numberof cycles.It can be assumedthatthe reductionfromthe first cycleto the secondis the greatest, thenbecominga smaller constantvalue fromthe secondcycleto the tenth. It is also assumedthat the Edlvalues of Series-D beams at the first cycle at each deflection amplitude is lower than that of correspondingSeries-Abeamswith only one loadrepetitionat that amplitude.These reductionratios are taken fromthe experimentaldatafor Series-D beams. OInthecaseof 6=6 (12) Ei p(1))-Ei (A) Eip(n))-o.7Ed'P(I))-%(n-2) @Inthecaseof (22; n2;10) (13) 6-26, (14) Ei p(I))-0.88Ei (A) Ed/P(A))-0.8Eip(I))-%(n-2) (22; n2;10) -160- (15) @Inthecaseof 6 2;36 Ei p(I))-0.88Ei (A) Ed'P(n))-0.95Eio'(1))-9f(n-2) Where, (16) (17) (22; nao) non-dimensionaldissipatedenergyat the first cycleat each deflectionamplitude Ed[(D(n)) : non-dimensionaldissipatedenergyat the n-th cycleat each deflectionamplitude Eat(A) : nonJimensional dissipated energy of corresponding Series-A beam calculatedfrom Eq.(5)at the same deflectionamplitude n: number of cycles E at(D(1)): Figure 16 shows a comparison of calculated EdT values and measurements. As this shows, the a 8.0 C a 7.0 0 ¥.-... coo o CO : measured : celcuI8tOd ;cS?yunlttaaetl:rSe;u:'ltVusan;:'trShe1'sn:iin1hCaeitd:ea:7gee:lea::5ht?t.h6neya tudes of more than > b This is mainly because the EdTvalues at the 4fiesyt. cycle at each deflection amplitudecalculatedhm Eq.(14) or Eq.(16) tend to be underestimated at larger deflection amplitudes.However,the differencebetween measured and calculatedEdT valuesis relativelysmall and EdT values of Series-D beams can be well estimated by this method. 6.0 J..--I.-- 0 LJJ 5.0 .=.?I?54 4 .0 O .=.'qxmqi 3.0 0 2.0 .:.'bn333 1.0 6y 10 7 3Q Say =: 26y 1 70 46y 70 7 56y 7 70 70 n (cycle) untiltheUltimateState Fig.16 Example of Changes in Measured and Even if the total energy dissipatedover a given Calculated Ed'Value loadinghistory can be calculatedas described,it (A =o.70, ps=2.66%) isdifficultto evaluatethe degreeof damageunless the totalenergywhich a membercan dissipateup to the ultimate state is known. Therefore, the effects of volumetric ratio of lateral confinement, =etchheE%Lda?egr(ef Bfd.:;Sahreess,isacnudslsoeaddFegreTstory onthenon-dimensional totaldissipatedenergyup Figure 17 shows the effect of loading history on the accumulationof non-dimensional dissipated eEneErd!u:. Tsniii,trh.exuA1;Te;:elS5tZ7st5Fedr' uLt2a eTrhg:addeuPa;.nyddSeOcrne:eag^ c-yVcAlcu.ei aYihneg:eas^s=e?i.e4s6l Lhteesvtas!utehaOnf thatundergraduallyincreasingloadingas in Series-A. In Series-B tests, a relativelylarge deflection cTcplehidne iseaaEpsliewdi tag?E2lSet,1oparde5fecs:,clsei cChOnaSseq^u e=n61.y.,61.wTghe edsieagcor;catscrraecEsalanrgS e.,deunri:5 etnheufF.si unloading, hysteresis loop and reduced energy dissipation. On the otherhand,rasublebissinw;thp lLnighh1?rg^O fvtahleu eps-( 6^=0.71 and 0.87), no significant difference according to loading history can be observed. In these cases, diagonal cracking is insignificant even at large deflectionamplitudesandthe crackrestorationperformanceis gooddue to the effectivenessof higher Enter?gdyu?zd,parr?1?i;;3s;rFersot=stsheesecroenscu,list,eteee aemffse cits Osfhl.o3dnT.g bheisct.o=ye osnmta7?e; c3TtTZiactrieoans10nfgdi^s slfaaltueed. -161- -I L4J N 40 i----. H 100 L-.-.--.1-..-.-l. -J-_- I- Lb 70 I tt) 50 120 LN Lu H i l--.lL--- I-I -.__- e A---i-1:-i. .tL ,,> •`tJL 8D i i 30 A : Serle9.8 I :/ Serlee-0 60 i •` ,t<ittI 40 Ji + : Ser/oe-A A : Ser/e9-a I : 9erIQe-C 6 + : Serlec-A A : SerlqQ-a J : Serlee-a /J 20 ,I 1 /tt t1 4 tl I J( 10 20 1 2 3 4 5 6 7 e defJectlot7, 9 7017 12 A 1 2 9 4 5 8 7 deflect[on, 6/6yc'I (a) A =0.46 e 9 0 70 7 2 3 deflectlot7, 6/6yc'I 4 5 6/6ycal (c) A =0.87 (b) A =0.71 Fig.17 Effects of Loading Histories on EEdT(p s=2.43%) 120 110 Lq 100 BJ 90 80 70 60 50 40 30 2 a 10 •` l- L a b 120 110 LJJ 100 H 90 80 70 60 50 40 30 20 10 - •` a A 0 : ^=o.43, @: ^=0.50, i: A_-0.71, I : ^=o.89 0 th + : ^=o.46 A: 0: V: •` ^=0.70 ^=o.87 ^=0.94 /-/ .,-.-----.A.,I/-i A -----1/ 1 2 3 yotume(rtc ratlo of hoops, p. (%) Fig.18 0 : p.=o% A : p-=0.67% 0 : p.=1.22% V: pJ=2.43% .3 0.4 0.5 0.6 0J 0.8 0.9 1.0 meohanlcat degree of pros(ress, A Fig.19 Effects of A on EEdlult. Value (S Cries-A) Effects of ps on EEdTult.Value (Series-A) fT;rdPFgfsa7e8e=sd-S]h;:e3rageo;Las?i.;:he;bdee:be hand, the value of EEd'ult.decreases with increasing A value within the range 0.43S A 5;0.94 and can be assumedto be almost inverselyproportionalto A when ps is constant. Further,the effectiveness oflateralconhement onimprovementto theenergydissipationpropertiesis dependent of A. From these results, the =EdTult.Value can be expressed as in Eq.(18). (18) EELt.=a ps2.b(i).c(#).d The values of the coefficients, a, b, c, and d should be estimatedseparately for Series-A beams and Series-D beams, since =EdTult. Values of Series-D beams are substantially higher than those of Series-Abeamsas a resultoften load repetitions at each denection amplitude.On the other hand, the values of these coefficientsestimated for Series-A beams should be applicable to Series-B and tsheerite&-e? sbeerTs: saTZe.uthgehttO1:1 dEis#u:tevdaleuneesrg.yf SSrTenstilihbeeuakiLartee ssiaieeShna?tsVmearYledri.fferent among -162- •` I 4 12J 0 i I: b h 0 : ^=o.43 a +.. ^=0.44 A: ^=0.46 i.. ^=0.50 D: I: ^=o.51 A_-o.70 b 10. 0 LIJ H e.0 E L_ Lb •` A n A + 0 A A: ^=0.50 I D: V: A_-o.70 ^=0.89 C): ^=o.94 HLu240 200 A . 4Jd v 160 120 A %v,I 40 I D + 2'0 -t a A E] 20 40 0 : ^=0.43 t> 280 J1 60 320 V: A_-o.77 Y: ^=0.86 O: +.. ^=o.87 ^=o.89 a 60 80 80 40 : ^=0.94 100 120 40 80 120 160 200240280320 E Ed'u(1<c&l) I Ed'ut(.(c'L) (a) Series-A Fig.20 (b) Series-D Comparison between E EdTulI.(mea) Values and E EdTulI.(cd) Values The coefficients a, b, c, and a obtained for Series-A beams by regression analysis of the test results are as follows: a=-5.52, b=32.48, c=7.44, d=-35.20 (standard deviation of =Ed'ul.. is 13.52) On the otherhand, the values of these coefficientsfor Series-D beamsare the following: a=-2939, b=45.69, c=30.28, d=-46.44 (standard deviation of i:EdTul..is 24.01) Eachcalculatedvalueofthe non-dimensionaltotaldissipatedenergyuntilthe ultimatestate obtained from Eq.(18) (=Ed andP) forSeries-A khcaldei?eSn-djcbaeta!? geest,hee:tTvi!f;hTehTseeasfZgr:rae; aslhu.ei fhEtd 'yEeda)u)lt.inva7igess. 2c2n(bae) 33@ re:tll;Ti:teeldy tlOa,ag eCeLtai:rfeesg-rae ,baelatEos? gasfhned idclistcerdePbayntChye bs;a%ezTdmdeeavSi:trieodna.nfd lC3a.l5C2u.I aiE?sfsE&'adi.nl1; becauseonlytheeffectsof volumetricratio of lateralconfinementandmechanicaldegreeof prestress areconsideredin the calculationprocess If the degreeof seismicdamageto concretestructuresor membersunder earthquakeloadingcouldbe expressednumerically, it would be a criterion by which to carry out repairs or strengthening to damagedstructures.Herewe discussthe possibilityof evaluatingseismicdamage based on hysteretic dissipatedenergy. A damageindex (DI) as Eq.(19) in this study is defhed. EEd' DI-ii= '19' Where, i: Ed'ul..: the non-dimensional total energywhich can be dissipated by a member until EEd.: fE::tttiu=lataecStuaieufoafeadgni.v:n_iiAdelins5ohni:foernyergy dissipated duringl.ading -163- •` Q •` •` I)------_-_ Q 1.0 •` o,6 qb A : SIrfI&.a D : SrTIIJIC v : Strl*a-D )ii:tt I g' o.4 5 Q ..-.- Att I . E3 o.6 5 o.6 •` :tit q> a o.4 6Tim o : SrrtJJI-A A : SrrlIJ-a D : S*TIJaJ v : SJrlt&-D :::iB --.I.ll a.. Ji--4_. A : SJTl*8-a J=tqo.2 b Eq".2 b 1.0 a 0.e tL B' o.4 •` •` YL a Q.e o : S*rltJ-A •` S •` a 0.8 5 •` -t 7a7.=iL, 1.0 E:•`o.2 b D : SIr'l*JJ v : SITl*J-D 7 1 2 3 4 5 6 7 8 9 101112 2 3 4 5 6 7 B 9 10 .--- 1 2 3 4 5 6 deflect[on, 6/6ycat deflectlon, 6/6yc'I deflectlon, 6/6ycBI (a) A %o.46 (b) (c) A %o.87 Fig.21 A i;0.71 Examples of Changes in DI (p s%2.50%) DI=Orepresents the no damage situa tion and DI=1.0 means that a member has reachedits ultimatestate; that is, in this study,when the load carrying capacity at a given deflection amplitude falls to 80% of the maximumultimate load. As mentionedpreviously, the value of differswith the number of rep=e aEg'at. cyclesat a particulardeflection amplitude.This impliesthat the effect of dissipatedenergy after the second cycle on the degreeof damage is different from that of the first loading at thesamedeflectionamplitude.In consideration of practical application, therefore, it is desirableto modify the I Eatvalue where several loadrepetitions take place at the same deflection a 20 3l, Q 18 C Q JL ql tL Q 76 5 14 4 Z= a 12 10 lJ O.L e} B.1 P.50J B7 I.& 1} 1J IJ 1} 1} 1J 1.5 1.f 17 1.8 1J 2JI ZJ I.1L,, I.I Z.S1,f damage )I 2.8&3 9A ft7dex, DI Fig.22 Statisticsof DI inthe Ultimate State ST,pelEtluddaembaygue? iEhgea draeAuacgt!ocnaEa;Loernwbe i:5acl::tSidde;Ssitnhge tehfefeAtoodfif%SdS i%ated? Veanleureg yaOnnd tthhee a=mg?.nd:. value for a basic loading history which is already known, for example, Series-A. In this paper, however,DI valuesof Series-D beamsare calculated from the = Eatvalues without modificationand coefficientsfor Series-D beams. As for the the I Ed'ult.Values are calculated from Eq.(18) us Series-B and Series-C beams, on the other hand, in#i5:lt. valuesare calculated using the coefficients for Series-A beams. Figure21 showssome examplesof the changesin DI during loadingtests. In Series-A, the degree of damageis smallat an earlystageof loadingandthe ratio of accumulateddamage riseswith increasing applieddeflectionamplitude.In Series-B, on the otherhand, the DI value afterthe first cycle reaches 0.3•`0.4. This implies that the beams are significantly damagedif subjectedto a deflectionclose to the ultimate value at the first cycle of loading. Subsequently,however,the increasein accumulated damagebecomessmaller.h Series-D beams,damageis accumulatedas ten load repetitionstake place at each deflectionamplitude, and the ultimatestate is reached at a smaller deflection amplitudeas comparedwith the correspondingSeries-A beam. In case of the beams with A=0.87, the DI value ecause the relative difference between doesnot reach 1.0 even at the end of loading. This is mai ngEbd 'u1.. Value itself is smaller than that of a gaelac=lai;tdh aEl:tug.raxdvtah.euea?tual valueislargesincethe h Fig.22,a histogramof DI correspondingto the ultimate state calculated for each beam is shown.A high degree of scatter (C.0.V.=0.454) in the DI value at the ultimate state is observed, although the averagevalue of DI is almost 1.0. The relative difference tends to be particularly large in the case of -164- b eamswith higher A value andlower p svalue. Thisis mainly dueto thegreater uncertaintyin the defhition of theultimatestate underreversedcyclicloadingand in the effectsof test variables. As previouslymentioned,non-dimensionaltotaldissipatedenergyup untiltheultimatestate is affected by notonlythetestvariablesadoptedin this studybut alsoby certainother factors.Therefore,further investigationsof energydissipationpropertiesarenecessaryin orderto establishanevaluationmethod for seismicdamageto concretestructuresbasedon hystereticdissipatedenergy. 4ii2QW In this paper, the effects of varioustest variableson the energydissipationpropertiesof partially prestressedconcretebeamsareinvestigated.h addition,a damageindexbasedon hystereticdissipated energyis proposedbasedon the experimentalresults. The mainconclusionsreachedin thisworkare as follows. (1) The energydissipationpropertiesof partiallyprestressedconcretebeams are affectedmainlyby volumetricratio of lateral confinementand mechanicaldegreeof prestress.The effects of concrete ?ompressivestrength,longitudinalsteelindex,andshearspan-effectivedepthratio are relativelysmall ln comparison. (2)Thenon-dimensionaldissipatedenergy,which is the dissipatedenergynormalizedby the product of calculatedyieldloadandyielddeflection,of partiallyprestressedconcretebeams is also influenced by the loadinghistory.The value of non-dimensionaldissipatedenergyat eachdeflectionamplitude can be expressedas a linear functionof the applieddeflectionamplitudeas the deflectionincreases, andas a quadraticas the denectiondecreases.Thevalues of the coefficientsin these functions depend mainlyon the level of mechanicaldegreeof prestress. (3) The non-dimensional dissipated energy at a particular deflection amplitude decreases with increashgcycles.Therate of decreaseis affectedby the applieddeflectionamplitudeand the number of cycles.Thenon-dimensionaldissipatedenergyat the first of ten loadrepetitionsis less thanwhere onlyone repetitiontakes place at eachdeflectionamplitude. (4)Thenon-dimensional total dissipatedenergyup untilthe ultimatestateincreaseswith increasing volumetric ratio of lateral confinement,while it decreaseswith increasing mechanical degree of prestress. It can be estimatedto a certain extent by a functionof these two variables.The value of non-dimensional total dissipatedenergy until the ultimate state is almost constant if the sum of applied deflection amplitudes is the same, although it tends to be somewhat smaller with less mechanicaldegreeof prestresswhere the deflectionis graduallydecreased, as in Series-B. (5)The degreeof damageto partiallyprestressedconcretebeams under reversedcyclicloadingcan be expressedquaJltitatively by a damageindexbasedonthe hystereticdissipatedenergy. However,further investigations on the process of dissipatedenergy accumulationare necessaryfor a more accurate evaluationof seismicdamageto concretestructures. References 1 2 3 P ublic Works Research Center: Manual for Restorationof CivilEngineering Structures Damaged during Earthquakes, Ministry of Construction, 1986 Park, Y. J. and Ang, A. H-S.: Mechanistic Seismic Damage Model for Reinforced Concrete, Joumal of Structural Engineering, ASCE, Vol.111, No.4, pp.722-739, 1985 Uomoto, T., Yajima, T., and Hongo, K.: Damage Evaluation of Reinforced Concrete Beams Subjected to Cyclic Bending Moment Using Dissipated Energy, Proc. of JSCE, No.460N-18, pp.85-92, [4] 1993 Stephens, J. E. and Yao, J. T. P.: Damage Assessment Using Response Measurements, Journal of Structural Engineering, ASCE, Vol.113, No.4, pp.787-801, 1987 -165- [5] Kobayashi, K., houe, S., and Matsumoto, T.: helastic Behavior of Partially Prestressed Concrete underReversedCyclicLoading,Proc.of the 5thCanadianConferenceon EarthquakeEngineering, Ottawa, pp.841-848, 1987 [6] houe, S., Kobayashi,K., and Katsuno,Y.: helastic Defomation Propertiesof PartiallyPrestressed Concrete Beams under Reversed Cyclic Loading, Proc. of the 42nd Amual Conference of the JSCE, Vol.5, pp.232-233, 7 8 9 1987 Igo, Y. et a1.: Load Carrying Capacityof PartiallyPrestressedConcreteMembers under Reversed Cyclic Loading, Proc. of the 43rd Amual Conference of the JSCE, Vol.5, pp.610-611, 1988 Inoue, S. et al.: Application of Rectangular Hoop as Lateral Confhement for Concrete Beam Members, CAJ Proceedings of Cement & Concrete, No.43, pp.340-345, 1989 Inoue, S. et al.: Effect of Loading Histories on the Energy Dissipation of Partially Prestressed Concrete Beams and Their Damage Evaluation, Proc. of the JCI, Vol.15, No.2, pp.401-406, 1993 [10] Fukushima,Y. et al.: Effectsof Various Factorson the DissipatedEnergy of Partially Prestressed ConcreteBeams,Proc. ofAmual Meetingof the JSCE Kansai Branch, pp.V-5-1-V-5-2, 1993 -166-