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Dissipative CLT-Based Seismic Upgrading System for RC-Framed Structures: Experimental Characterization, Numerical Modelling, and Design Guidelines

Barbagallo, Francesca; Marino, Edoardo Michele; Pozza, Luca; Mazzotti, Claudio

Abstract

This paper investigates a seismic retrofit technique named e-CLT, which is part of the solution for integrated seismic and energy rehabilitation of buildings developed in the framework of the research project e-SAFE funded by the European Union’s Horizon 2020 research and innovation program. According to this technique, the RC structure is cladded bymeans of CLT panels equipped with friction dampers, to increase lateral stiffness, strength, and energy dissipation capacity. The effectiveness of the e-CLT system has been proved by a full-scale experimental test. A finite element numerical model of the RC frame with e-CLT system has been developed and calibrated based on the experimental results. Hence, guidelines for the design of seismic strengthening of multistorey RC framed building structures by e-CLT system have been drawn based on the results of a parametric analysis conducted on a set of RC case study frames representative of a variety of existing buildings not designed for seismic resistance.

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Ea hquake Enginee ing & S uc u al Dynamics RESEARCH ARTICLE Dissipa i e CLT-Based Seismic Upg ading Sys em o RC-F amed S uc u es: Expe imen al Cha ac e iza ion, Nume ical Modelling, and Design Guidelines F ancesca Ba bagallo1E ika Liccia dello1Edoa do Michele Ma ino1Claudio Mazzo i2Luca Pozza2 1Depa men o Ci il Enginee ing and A chi ec u e, Uni e si y o Ca ania, Ca ania, I aly 2DICAM Depa men , Uni e si y o Bologna, Bologna, I aly Co espondence: F ancesca Ba bagallo ( [email p o ec ed]) Recei ed: 14 June 2024 Re ised: 11 Feb ua y 2025 Accep ed: 17 Feb ua y 2025 Funding: This pape was ca ied ou in he amewo k o he “Ene gy and seismic a o dable eno a ion solu ions” (e-SAFE) p ojec , which has ecei ed unding om he Eu opean Union’s Ho izon 2020 esea ch and inno a ion p og am unde g an ag eemen No. 893135. Keywo ds: exis ing buildings | ic ion dampe s | seismic ene gy ehabili a ion | seismic s eng hening | imbe ABSTRACT This pape in es iga es a seismic e o i echnique named e-CLT, which is pa o he solu ion o in eg a ed seismic and ene gy ehabili a ion o buildings de eloped in he amewo k o he esea ch p ojec e-SAFE unded by he Eu opean Union’s Ho izon 2020 esea ch and inno a ion p og am. Acco ding o his echnique, he RC s uc u e is cladded by means o CLT panels equipped wi h ic ion dampe s, o inc ease la e al s i ness, s eng h, and ene gy dissipa ion capaci y. The e ec i eness o he e-CLT sys em has been p o ed by a ull-scale expe imen al es . A ini e elemen nume ical model o he RC ame wi h e-CLT sys em has been de eloped and calib a ed based on he expe imen al esul s. Hence, guidelines o he design o seismic s eng hening o mul i- s o ey RC amed building s uc u es by e-CLT sys em ha e been d awn based on he esul s o a pa ame ic analysis conduc ed on a se o RC case s udy ames ep esen a i e o a a ie y o exis ing buildings no designed o seismic esis ance. 1 In oduc ion In he second hal o 20 h cen u y, ein o ced conc e e (RC) s uc u es sp ead wo ldwide. Howe e , mos o hese buildings p eda e mode n code p o isions, bo h in e ms o s uc u al and ene gy equi emen s. In Eu ope, mo e han 75% o he land is occupied by esiden ial buildings and mo e han 40% o hese a e mul i-s o ey RC amed s uc u es cons uc ed be o e he 1960s o he 20 h cen u y [1]. These s uc u es a e expec ed o exhibi poo seismic esponse, and hei ene gy pe o mance is so inadequa e ha hey a e liable o 36% o he o al ene gy consump ion and CO2emissions in Eu ope [2]. An explica i e example o his issue is o e ed by he I alian e i o y. Acco ding o he la es census o I alian esiden ial buildings [3], mo e han 70% o he cu en esiden ial buildings we e ealized be o e 1981, when seismic zona ion included only 25% o he I alian e i o y. These buildings su e om high seismic ulne abili y, as d ama ically demons a ed by ecen seismic e en s [4, 5]. In addi ion, almos 90% o he I alian building s ock was cons uc ed be o e 1991, ha is, be o e he en o cemen o he i s egula ion on he mal pe o mance c i e ia [6]. To boos a compelling ansi ion owa d a esilien and sus ainable socie y, Eu opean egula ions on cons uc ion wo k [7] ha e been adding equi emen s o keep he cons uc ion pe o mances in ac and ex end i s se ice li e as long as possible [8]. The e o e, he ehabili a ion o hese build- ings is a eal need and, as a ma e o ac , du ing he las 30 yea s he a e o e o i in e en ions inc eased om 20% o 40% and i is expec ed ha his end will s eadily inc ease in he nea u u e. This is an open access a icle unde he e ms o he C ea i e Commons A ibu ion License, which pe mi s use, dis ibu ion and ep oduc ion in any medium, p o ided he o iginal wo k is p ope ly ci ed. © 2025 The Au ho (s). Ea hquake Enginee ing & S uc u al Dynamics published by John Wiley & Sons L d. Ea hquake Enginee ing & S uc u al Dynamics, 2025; 54:1775–1796 h ps://doi.o g/10.1002/eqe.4334 1775 o 1796 Con en ional uncoupled ehabili a ion echniques aim o enhance he seismic pe o mance o he he mal one [9]. Fu he mo e, he majo i y o he con en ional echniques equi e he addi ion o de ices ha occupy space o ins alla ion, need in asi e ins alling wo k ha o ce eloca ion o occupan s and cause ac i i ies dis up ion. Hence, new app oaches a e equi ed o p omo e en i onmen al economic–social sus ainable ene gy and seismic e o i in e en ions. Among he in eg a ed app oaches cu en ly unde de elopmen , he “double skin” app oach is one o he mos p omising. I consis s o he supe imposi ion o a second ex e nal s uc u e designed o enhance seismic and he mal pe o mance o he building. The main ad an age o his solu ion is ha i s ins alla ion akes place om he ou side o he building, hus educing o he minimum he dis up ion o he dis u bance o occupan s. Di e en cons uc ion echniques and ma e ials ha e been p oposed o he second skin. Fo example, Takeuchi e al. [10] de eloped a s eel dissipa i e açade, Ma ini e al. [11] p oposed a second skin wi h s eel shea walls and he possibili y o in oducing dissipa i e membe s, Fe an e e al. [12]in es iga ed an in eg a ed solu ion based on s eel exoskele on. RC second skin has been de eloped as well, such as he new RC in illed ame connec ed o he exis ing s uc u e p oposed by Man edi and Masi [9] o he cas -in-si e RC ame sys em endowed wi h EPS modules de eloped by Pozza e al. [13]. An al e na i e app oach is ollowed by Bou nas [14], who p oposes he use o Tex ile Rein o ced Mo a jacke s o inc ease he ou -o -plane load capaci y and he ene gy abso p ion capaci y o in ill walls in RC ames. In he ide owa d he eco iendly ma e ials, he use o wood as a s uc u al ma e ial has ecen ly gained p ominence. In pa icula , c oss-lamina ed imbe (CLT) is a sus ainable solid wood-based cons uc ion ma e ial wi h low mass and excellen s uc u al pe o mance. CLT panels consis o an odd numbe o s acked c osswise laye s o so wood boa ds, bonded by s uc u al adhesi e [15], ha can sus ain loads in all di ec ions [16]. CLT panels a e p oduced o a high deg ee o p e ab ica ion, allowing e icien on-si e ins alla ion. No wi hs anding he ligh weigh na u e o CLT, i is cha ac e ized by a high in-plane la e al s i ness and s eng h. Fu he mo e, he possibili y o combining CLT panels wi h duc ile join s makes he use o CLT appealing in ea hquake-p one a eas [17, 18]. Thanks o hese ea u es, he use o CLT panels has been ecen ly ex ended o seismic e o i o RC exis ing s uc u es, basically ollowing he second skin app oach al eady men ioned. S azi e al. [19] p oposed he encasemen o CLT panels wi hin he RC ame bays, as a eplacemen o mason y in ills. Diagonal es s we e conduc ed on con ined and no con ined CLT panels, while he e ec o he CLT panels on RC s uc u es was nume ically in es iga ed on a single-s o ey one- bay RC ame. Also, Smi oldo e al. [20] p oposed o eplace he exis ing mason y in ill o RC ames wi h a CLT panel, which was inse ed in o he ame and ixed o RC membe s by a imbe sub- ame. The imbe sub- ame and he RC ame a e connec ed by conc e e sc ews, which a e designed o emain elas ic. The duc ile componen o he sys em is he connec ion be ween he imbe panel and imbe sub- ame. The p oposed echnique was in es iga ed by pusho e analysis on single-bay single-s o ey ames and he nume ical esul s showed an inc ease in e ms o la e al esis ance and maximum displacemen s. Al hough bo h s udies demons a ed he good pe o mances p o ided by he CLT in ills, in eal exis ing s uc u es he inse ion o he CLT panels in place o in ill walls would equi e qui e la ge demolishing wo k and a no negligible dis u bance o occupan s. In his ega d, Smi oldo e al. [21] conduc ed an expe imen al s udy on an RC ame o in oduce a less in asi e op ion, i.e., CLT panels a e applied o he building açade, wi hou emo ing he mason y in ills, and as ened o he ou e ace o RC beams by dowel- ype connec o s. Howe e , he expe imen al es s e idenced ha also his ex e nal con igu a ion equi es qui e in asi e wo ks on he mason y in ill panels, which mus be cu o a oid in e ac ion be ween RC columns and he walls. Fu he mo e, he dowel- ype connec o s ans e ed he shea o ce om he CLT panel o he columns, which mainly sus ained he damage mechanism. Sus e sic and Dujic p oposed he combina ion o CLT panels wi h a “nano” insula ion laye o c ea e an ou e shell ha is connec ed o he exis ing s uc u e by s eel ancho b acke s [22]. The echnique was expe imen ally es ed on a wo-s o ey one-bay RC ame wi h mason y in ills and nume ically in es iga ed on a h ee-s o ey wo-bay RC ame [23–25]. The dissipa i e capaci y is delega ed o he s eel angula b acke s. Howe e , i is s a ed ha such a connec ion would equi e modi ica ions o be applicable in eal s uc u es. Indeed, i equi es access om he inside o he building [22]. Badini e al. [26] p oposed he use o CLT walls pe pendicula ly o he açade. The wall is connec ed o he RC ame by s eel b acke s, while pos - ensioned s eel endons a e in oduced be ween CLT panels o inc ease he dissipa i e capaci y. Howe e , he impac o he o ces ansmi ed by he ex e nal s uc u e o he exis ing RC membe s may imply he educ ion o he capaci y o RC membe s and he need o addi ional in e nal local in e en ions. In his amewo k, his pape p oposes an inno a i e in eg a ed seismic and ene gy sys em, named e-CLT. The concep o his sys em was d a ed in [27] and i s de elopmen as a seismic upg ading ool is pa o he mul idisciplina y Ho izon 2020 inno a ion esea ch p ojec e-SAFE (ene gy and seismic AF o d- able Eno a ion solu ions) [28]. This pape p esen s he esea ch ac i i y o his p ojec in he ield o seismic upg ading and he ela ed ou comes. The e-CLT sys em is based on he idea o endowing exis ing RC- amed buildings wi h a second pe o m- ing skin made o p e-assembled and cus omizable componen s. The e-CLT sys em is composed o p e ab ica ed CLT panels supe imposed o he ex e nal wall and connec ed o he RC beams by ic ion dampe s. Each dampe connec s he CLT panels o wo consecu i e loo s o he in e media e RC beams and consis s o wo s eel p o iles: he ancho p o ile is connec ed o he RC beam by ancho bol s and o he o he p o ile, named ee p o ile, by slo ed holes and p e ensioned high-s eng h bol s. The ee p o ile ecei es he shea o ce om he CLT panel placed abo e and ansmi s i o he ancho p o ile by means o he ic ion exe ed on he con ac su ace. The componen s o he dampe a e shaped so as o decouple he CLT panel’s e ical mo emen s om hose o he dampe s. In case o a seismic e en , wo possible scena ios may occu : I he seismic ac ion is mode a e, he dampe s igidly connec he CLT panels o he RC s uc u e, hus making a ailable addi ional la e al s i ness and s eng h. This is help ul o a oid damage in non-s uc u al componen s. On he o he hand, i s ong seismic ac ions occu , he dampe s ac i a e and dissipa e pa o he inpu seismic ene gy by sliding. This educes he damage o 1776 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License s uc u al componen s and p e en s he building om collapsing. I is no ewo hy ha he ac i a ion o he dampe s de ines an uppe bound o he o ce sus ained by he CLT panels, hus p e en ing hei ailu e e en in case o unexpec edly s ong g ound mo ions. The e-CLT sys em p esen s se e al ad an ages wi h espec o o he sys ems. The e-CLT panels can be combined wi h non-s uc u al p e-assembled panels made o ligh weigh wooden ames and p o ided wi h high-pe o ming windows. The e-CLT sys em is designed o allow a quick and easy ex e nal ins alla ion, which can be pe o med by mobile li ing equipmen , hus a oiding cos s and ime needed o he sca olding se - up. Di e en pa s o he sys em, such as ancho p o iles, a e sui able o p e-assembly p ocess o si e. Fu he mo e, since he ins alla ion p ocess akes place om he ou side, he dis u bance o occupan s is minimized and ope a i i y dis up ion is a oided. The dampe , conside ing i s size, is sui able o ins alla ion on mos common RC amed buildings. Fu he mo e, i is ins alled ou side he building and he dampe inspec ion and main enance a e also eased by s ing cou ses, which can be easily emo ed. Compa ed o s udies a ailable in he li e a u e, he pape has a wo old inno a i e goal: on one hand, o demons a e and quan i y he bene i s p o ided by he e-CLT sys em o he s uc u al esponse o an RC ame, based on expe imen al es s; on he o he hand, o assess he impac o he e-CLT sys em on he s uc u al pe o mance o a se o ealis ic RC buildings, by means o ini e elemen nume ical models and inc emen al nonlinea dynamic analysis (IDA). To his end, he esea ch ollowed h ee main s eps: (1) he e ec o he e-CLT sys em on he seismic esponse o RC ames was expe imen ally ep oduced, (2) a eliable nume ical model o he RC ame wi h e-CLT sys em was de eloped, and (3) he seismic pe o mance o mul i-s o ey RC ames wi h di e en e-CLT con igu a ions was in es iga ed, so as o p o ide guidelines o he design o seismic upg ading by e-CLT. Fi s , he esul s o wo quasi-s a ic cyclic es s ca ied ou on wo in illed RC ames (wi hou and wi h e- CLT), a e p esen ed. The es s cha ac e ized he cyclic esponse o he s uc u al sys em and p o ided da a o he calib a ion o nume ical model. In pa icula , he a ailabili y o wo es s allowed he calib a ion o he nume ical models o he RC ame and he e-CLT sys em in wo s eps. To ex end he s udy o ac ual buildings wi h RC amed s uc u es designed acco ding o old (non-seismic) egula ions, a se o mul i-s o ey RC ame models is de ined. Inc emen al dynamic analyses and pusho e analyses a e ca ied ou on hese ame models o in es iga e he seismic de iciencies o exis ing RC- amed buildings and he capabili y o pusho e analysis in de ec ing such de iciencies. Hence, IDAs a e ca ied ou on he RC ame models equipped wi h e-CLT. Th ee di e en con igu a ions o e-CLT a e conside ed: he local na ow con igu a ion, he local ex ended con igu a ion, and he sp ead con igu a ion. The esul s o IDA led o iden i ying he mos e ec i e con igu a ion, ela ing i o he ou come o pusho e analysis (design analysis), and quan i ying he bene i s ha can be gained by e-CLT. In he nume ical in es iga ion, bo h duc ile and agile ailu e modes o s uc u al membe s a e checked. The seismic pe o mance o he models is analyzed in e ms o he dis ibu ion o seismic demand and demand- o-capaci y a io along he heigh , agili y cu es, and mean annual equency o exceedance o Nea Collapse and Signi ican Damage limi s a es. The inal sec ion d aws he design p o isions o he seismic upg ading o RC s uc u es by e-CLT. 2Expe imen al Tes ing o he e-CLT Sys em The expe imen al campaign is ca ied ou a he CIRI-EC labo a o y o he Uni e si y o Bologna and is de o ed o (1) cha ac e izing he cyclic esponse o a mason y in illed RC ame s eng hened by he e-CLT echnology and (2) p o iding physical e idence ha he componen s o he seismic upg ading sys em pe o m as in ended, e en a e epea ed and se e e cycles o loading. To his end, wo RC ame specimens we e es ed in eal scale, in bo h uns eng hened and s eng hened con igu a ions, unde quasi-s a ic cyclic loading. 2.1 Specimen Desc ip ion Two iden ical one-s o ey–one-bay RC ames a e es ed in he wo in es iga ed con igu a ions. The RC ames eplica e he ypical cons uc i e ea u es o I alian buildings o he ‘70s and a e designed in compliance wi h he building code en o ced in 1974 [29] conside ing g a i y loads only. De ails on he design o he RC ames may be ound in [30].Thespanleng his equal o 4.0 m and he in e -s o ey heigh is 3.2 m. Columns ha e 300 ×300 mm c oss sec ion, while a 300 ×400 mm c oss sec ion is adop ed o beam. The RC ames a e in illed wi h a single laye 120-mm- hick mason y wall ealized wi h ex uded hollow blocks and aligned wi h an ex e nal su ace o he ame (Figu e 1a). Comp ession es s we e pe o med on cube and cylinde samples collec ed du ing he cas phase o he wo ames. The a e age alues o he cylinde comp essi e s eng h o s eng hened and uns eng hened ames a e 21.9 and 21.4 MPa, espec i ely. Tensile es s we e un on h ee s eel eba specimens collec ed om he s eel lo and he a e age yielding s eng h was equal o 534.6 MPa. The e-CLT sys em was cons i u ed by a 100 mm hick CLT panel (5 laye s o 20 mm hickness) connec ed o he RC ame by means o a s eel appa a us (Figu e 1b). The wo uppe componen s o he s eel appa a us a e ancho ed o he uppe RC beam and suppo he CLT panel, while he wo bo om componen s a e mechanical ic ion dampe s ac i a ed by he ela i e displacemen be ween CLT panel and bo om RC beam. 2.2 Expe imen al Se up and Tes P o ocol A speci ically designed se up is de eloped o ca y ou quasi- s a ic es s o he wo specimens (Figu es 1and 2). The RC ame is ancho ed o he s ong loo while a ho izon al displacemen is imposed o he op RC beam by means o a 500 kN MTS se o-hyd aulic jack ancho ed o he conc e e eac ion wall. The ancho ing sys em o he bo om RC beam is ealized by igid s eel b acke s and pos - ensioned dywidag ba s and i ually a oids also he ho izon al sliding o he RC ame o e he s ong loo . Fu he mo e, he s eel b acke s aligned on he RC columns se e as a as ening sys em o he e ical ba s used o apply he axial o ce o he columns. The axial o ce, equal o 250 kN, is applied o each column by means o hyd aulic jacks placed o e hem and cons ained by ans e se s eel beams as ened o he bo om b acke s desc ibed be o e. The e ical load applica ion sys em is designed wi h od end pins and conical nu s, which allow cyclic la ge displacemen s in he ho izon al di ec ion. The applied e ical o ces ep oduce he axial o ce caused by he 1777 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License FIGURE 1 Geome y and pho os o specimens: (a,c) uns eng hened and (b,e) in illed s eng hened RC ame, (d) membe s c oss sec ions. FIGURE 2 Tes se up: (a) global scheme and (b) pho o o labo a o y es ing sys em (s eng hened con igu a ion). g a i y load o he seismic design si ua ion in he i s s o ey columns o a h ee-s o ey esiden ial building. The ho izon al displacemen applica ion sys em is composed o a s eel ie made up o s i ened ans e se s eel pla es placed a he wo ends o he uppe RC beam and connec ed h ough pos - ensioned dywidag ba s. The se o-hyd aulic ac ua o is connec ed o one end o he ie and is cons ained o he eac ion wall. The en i e es sys em is ans e sally s abilized by means o a la ice s eel sys em allowing o he ho izon al and e ical displacemen s only o he op RC beam h ough sphe ical olle s. This ans e se s abiliza ion sys em a oids possible ou -o -plane displacemen o he RC ame, in pa icula in he case o he s eng hened con igu a ion, wi h he e-CLT panel eccen ically ixed wi h espec o he ho izon al o ce alignmen . The measu emen sys em depic ed in Figu e 2is composed o : (1) wo ho izon al ansduce s eco ding he base displacemen (LVDT 1) and he op displacemen (LVDT 2) espec i ely; (2) a ho izon al ansduce eco ding he ela i e displacemen be ween he ic ion dampe and he base RC beam (LVDT 3) and (3) a LOAD CELL eco ding he o ce in he ac ua o . The RC ame d i is calcula ed as he di e ence be ween he ho izon al displacemen s o he op and base RC beams eco ded du ing he es using LVDT 2 and LVDT 1, espec i ely. Mo eo e , 1778 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License TABLE 1 Ho izon al loading p o ocol. S ep o loading 1 2 3 4 5 6 7 8 9 10 11 D i ampli ude (mm) ±1±2±4±8±16 ±24 ±32 ±48 ±64 ±80 ±96 D i a io (%) ±0.03 ±0.06 ±0.13 ±0.25 ±0.50 ±0.75 ±1.00 ±1.50 ±2.00 ±2.50 ±3.00 Loading a e (mm/s) 0.02 0.05 0.10 0.20 0.20 0.30 0.40 0.50 0.70 1.00 1.20 No. o cycles 33333333333 (a) (b) (c) -300 -200 -100 0 100 200 300 -125 -75 -25 25 75 125 ]Nk[F D i [mm] S engh ened Uns engh ened -150 -100 -50 0 50 100 150 -125-100 -75 -50 -25 0 25 50 75 100 125 ]mm [ i D Sliding [mm] 0 50 100 150 200 250 300 1 2 4 8 16 24 32 48 64 80 96 ]Jk[y g e nede a p is s iD D i [mm] S engh ened Uns engh ened FIGURE 3 Cyclic esponse o he uns eng hen and s eng hen ames: (a) load-d i hys e esis loops, (b) RC d i e sus e-dampe sliding, (c) dissipa ed ene gy. he ic ion dampe sliding is eco ded o he s eng hened con igu a ion using LVDT 3. Figu e 2shows a comp ehen- si e scheme o he se up and a pho o o he expe imen al equipmen . The specimens a e loaded in wo phases: i s , he e ical o ces a e applied and g adually inc eased up o he a ge alue o 250 kN in o ce con ol, hen he ho izon al displacemen is cyclically applied. In he second phase, he e ical o ces a e kep cons an , by con olling he hyd aulic p essu e o he jacks, while d i cycles o inc easing ampli ude a e applied by con olling he di e ence in he ho izon al displacemen s o he uppe and lowe beams. Du ing he en i e cyclic loading phase, he o ce in he ac ua o is measu ed using he LOAD CELL. The ho izon al loading p o ocol is designed aking in o accoun he displacemen capaci y o he e-CLT sys em. I is summa ized in Table 1, which lis s d i ampli ude, d i a io, loading a e, and a numbe o cycles o each s ep o he cyclic loading. 2.3 Tes Resul s All he componen s o he e-CLT sys em beha ed as in ended, up o he end o he es . Indeed, he CLT panel emained elas ic and did no expe ience ins abili y o any kind o local damage e en unde he la ges imposed d i , ha is, 3% o he s o ey heigh . Hence, i e icien ly ans e ed he ho izon al o ce om he op beam o he wo ic ion dampe s a he bo om o he panel. The dampe s ac i a ed as planned unde he push exe ed by he CLT panel and slid al e na i ely back and o wa d dissipa ing ene gy. A he end o he es , he s eel appa a us was dismoun ed and he single componen s (pla es, sc ews, bol s, and aluminum shim laye s) we e accu a ely examined. No sign o yielding o o he ype o damage was de ec ed, hus p o ing ha he s eel appa a us and as ening sys em beha ed elas ically o he whole du a ion o he es . Figu e 3a compa es he load-d i hys e esis loops ob ained o he uns eng hened ( ed line) and s eng hened (black line) con igu a ion. I is e iden ha he RC ame wi h he e- CLT sys em exhibi s ini ial la e al s i ness and peak s eng h signi ican ly la ge han hose o i s uns eng hened coun e pa . Mo eo e , he s eng h deg ada ion (i.e., di e ence be ween he o ce achie ed a he 1s and he 3 d epea ed cycles) esul s gene ally lowe o he s eng hened con igu a ion, especially o la ge d i le els. Figu e 3b shows he slippage be ween he wo pa s o he ic ion dampe e sus he d i o he RC ame eco ded du ing he es . A a ia ion o he RC ame d i while he dampe slippage emains cons an ( e ical b anches in he g aph) iden i ies a e e sal o loading. This occu s when he o ce ansmi ed by he CLT panel o he dampe empo a ily becomes lowe han he dampe ic ion o ce and he a ia ion o he slippage s ops. A e he e e sal, when he o ce in he dampe a ains again he alue o he ic ion o ce, bo h d i and slippage s a a ying simul aneously again. Hence, he heigh o he e ical b anches o he g aph ep esen s he po ion o he d i ha canno be ans o med in o slippage because o he de o mabili y o he panel and o he ic ion dampe as ening sys em. The small heigh o he e ical b anches o he g aph obse ed in Figu e 3b demons a es ha a 100-mm- hick CLT panel is s i enough o ans o m almos he whole d i in o slippage (abou 80%, since o d i sligh ly lowe han 100 mm he slippage is abou 80 mm), hus o cing he dampe s o dissipa e ene gy e icien ly. This esul s in a big posi i e impac o he e-CLT sys em on he ene gy dissipa ion capaci y (compu ed acco ding o [31]). Indeed, he a ea enclosed by he hys e esis loops (dissipa ed ene gy) o he s eng hened ame is much la ge han ha o he uns eng hened ame (Figu e 3a). The 1779 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License RC in illed ame + e-CLT RC membe s In ill panel CLT panel F ic ion dampe s In illed RC ame e-CLT sys em FIGURE 4 Desc ip ion o elemen s o he nume ical model. compa ison be ween he ene gy dissipa ed a he end o each loading s ep by he s eng hened and uns eng hened ames (Figu e 3c) quan i ies he imp o emen o dissipa ion capaci y p o ided by e-CLT, which can be e en 200% o ha o he uns eng hened ame. 3 Nume ical Model o he Tes Specimen A plane nume ical model o he es specimen is implemen ed in OpenSees [32] and de eloped in o wo “mac o-sys ems”: he in illed RC ame and he e-CLT sys em (Figu e 4). Each pa o he nume ical model is i s desc ibed, and hen he alues o mechanical pa ame e s a e calib a ed so ha he cyclic esponse o he nume ical model ma ches he expe imen al one. 3.1 Desc ip ion o he Nume ical Model The nume ical model o he in illed RC ame includes columns, beams, and in ill panels, and i is assumed ixed o he g ound. Fo RC columns and beams, nonlinea beha io is supposed o be limi ed o plas ic hinge egions a membe ends, while he emaining pa o he elemen emains elas ic. They a e modeled as beamWi hHinges elemen wi h he modi ied Gauss Radau in eg a ion ule [33]. The leng h o plas ic hinge Lpl is se equal o he dep h o he c oss sec ion and he c oss-sec ion o e Lpl is disc e ized in o ibe s. Speci ically, he conc e e pa o he c oss-sec ion is subdi ided in o ibe s ha ing 5 mm dep h and wid h equal o he wid h o he c oss-sec ion, while single ibe s a e used o model eba s. The Ken –Sco –Pa k cons i u i e law (Conc e e01 uniaxialMa e ial)[34] and he elas ic–plas ic cons i u i e law wi h kinema ic ha dening (S eel02 uniaxialMa- e ial)[32] a e assigned o he conc e e and he s eel ibe s, espec i ely. A pai o diagonal usses is used o model he in ill panel. Unde he e ec o ho izon al o ces, only he comp essi e b anch is ac i e, while he ensile one p o ides a minimal non- ze o s i ness necessa y o nume ical s abili y. Al hough his modeling app oach o in ill panels is a he simple, i is ecog- nized o ep oduce sa is ac o ily he global esponse o ames unde ho izon al o ces and is deemed an accep able comp omise be ween compu a ional bu den and accu acy o esul s [35]. As p oposed by Panagio akos and Fa dis [36] and Cela ec e al. [37], he o ce-displacemen ela ionship o he diagonal usses is de e mined o eplica e he shea o ce-d i ela ionship o he in ill panel. This ela ionship consis s o ou b anches: he i s b anch co esponds o he linea elas ic beha io up o he i s c acking o he in ill, he second b anch uns om he i s c acking up o he maximum s eng h, he hi d b anch is he pos -capping deg ading b anch, and uns om he maximum s eng h o he esidual s eng h, inally, he ou h b anch is ho izon al and co esponds o he esidual s eng h. Fo each b anch, he alues o s i ness and maximum o ce a e de e mined acco ding o he equa ions p oposed in [37]. The abo emen ioned mul ilinea o ce-displacemen ela ionship is con e ed in o an equi alen s ess–s ain ela ionship. The alues o s ess–s ain couples o he h ee co ne s o he en elope, bo h in he posi i e and nega i e loading di ec ion, a e assigned o he usses by he Pinching4 uniaxialMa e ial implemen ed in OpenSees. The e-CLT sys em is composed o he CLT panel and ic ion dampe s (Figu e 4). The CLT panel is modeled by means o six equi alen usses: wo e ical usses, wo ho izon al usses, and wo diagonal usses (Figu e 5). All usses a e elas ic and ha e c oss-sec ion wi h he uni a y a ea. The axial s i ness o he usses is calib a ed o p o ide he same in-plane s i ness o he CLT panel. To his end, he elas ic modulus o he e ical and diagonal usses Ecand Eda e calib a ed so ha he ho izon al and he e ical displacemen s o he uss model a e equal o hose o he ac ual CLT panel subjec ed o wo ho izon al o ces applied on he op co ne s o he panel (Figu e 5). Consis en ly, he elas ic modulus o he ho izon al usses Ebis calib a ed so ha he ho izon al displacemen o he CLT panel simula ed by usses is equal o ha o he ac ual CLT panel subjec ed o wo opposi e ho izon al o ces applied on op o he panel (Figu e 5). The displacemen demands o he ac ual CLT panel a e de e mined by a second “suppo ” nume ical model, which simula es only he CLT panel by a single shell elemen wi h elas ic o ho opic ma e ial. The Young and shea moduli in he h ee mu ually pe pendicula di ec ions o he shell elemen s depend on he mechanical cha ac e is ics o he conside ed CLT panel. F ic ion dampe s a e simula ed by ze o-leng h elemen s loca ed a he beam- o-column in e sec ion (Figu e 4). The beha io o ic ion dampe s in he ho izon al di ec ion is desc ibed by an elas ic-plas ic beha io (S eel01 uniaxialMa e ial in OpenSees), whose yielding s eng h ep esen s he ic ion o ce ha ac i a es he dampe s. In he e ical di ec ion, he dampe can mo e eely. The concen a ed g a i y loads on columns a e hose applied du ing he expe imen al es and a e equal o 250 kN. The ho izon al loading applica ion sys em o he expe imen al es is simula ed by a uss elemen wi h s eel elas ic modulus and c oss- sec ion a ea equal o ha o he s eel ie used in he es . The uss connec s wo addi ional ex e nal nodes ha a e o mally coinciden wi h he RC beam ends. Each addi ional node is connec ed o he co esponding node o he beam end by a ze o- leng h elemen ha eac s only in comp ession wi h e y la ge axial s i ness. Two opposi e ho izon al o ces equal o 320 kN a e applied a each end o he beam o eplica e he p es ess o ce applied in he es . 1780 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License H L h h Shell elemen h Ho izon al displacemen equilib ium Ve ical displacemen equilib ium H L h h Shell elemen h 1) Fo ces wi h same di ec ion Ho izon al displacemen equilib ium 2) Fo ces wi h opposi e di ec ion FIGURE 5 E alua ion o he axial s i ness o equi alen usses simula ing he CLT panel. (b)(a) (c) D i [mm] D i [mm] D i [mm] FIGURE 6 Expe imen al e sus nume ical cyclic esponse o he uns eng hened ame in e ms o o al base shea - op displacemen : (a) sub- componen app oach, (b) nume ical model o RC ame (la ge ampli ude displacemen s); (c) nume ical model o RC in illed ame (low ampli ude displacemen s). 3.2 Calib a ion o he Pa ame e s o he Nume ical Model To calib a e he mechanical ea u es o he desc ibed nume ical model, he esul s p o ided by he expe imen al es , in e ms o base shea and op displacemen , a e assumed as a ge s. Two cal- ib a ion p ocesses a e ollowed in se ies: Fi s , he cha ac e is ics o he RC ame and he in ill panel a e de e mined based on he esul s o he cyclic es on he in illed RC ame (wi hou e-CLT sys em). A e wa d, he ea u es o he e-CLT componen s a e calib a ed o ma ch he expe imen al esul s o he s eng hened specimen (wi h e-CLT). In he i s calib a ion p ocess, he mechanical cha ac e is ics o bo h RC membe s (columns and beams) and in ill panels a e deduced om he same expe imen al es , ollowing a “sub- componen ” app oach (Figu e 6a). This app oach is based on he expe imen al obse a ion ha , o la ge displacemen demand, he s i ness and s eng h o he in ill panel d as ically dec ease in almos all RC amed s uc u es subjec ed o ho izon al o ces. This allowed he de e mina ion o he mechanical pa ame e s o he RC membe s assuming as a ge he cyclic esponse unde he la ges displacemen ampli udes, when he s i ness and s eng h o he in ill panel has become negligible. In his s ep, he nume ical model includes only he RC membe s and he maximum comp ession s eng h o conc e e Fcm is se equal o 21.65 MPa, i.e., he mean comp essi e s eng h ob ained om he conc e e comp essi e coupon es s. The co esponding Young’s modulus Ecm is calcula ed as 2 Fcm/εc2 and i is equal o 21950 MPa. Howe e , o ake in o accoun he e ec o conc e e c acking, he momen o ine ia o he sec ion is educed o 50% and 80% o Ig o beams and columns, espec i ely [38]. The con inemen e ec on he co e o he membe c oss sec ions is neglec ed because he specimen is ep esen a i e o RC s uc u es designed wi hou seismic p o isions, ha gene ally ha e ew s i ups. The s ains a maximum comp ession s eng h εc0 and a c ushing s eng h εcu a e assumed equal o he con en ional alues 2 ×10−3and 3.5 × 10−3, espec i ely. The esidual conc e e comp essi e s eng h is calib a ed based on he esul s o he ull-scale expe imen al es ca iedou on heRC ameandse equal o6MPa,abou 30% o he peak alue. The ension s eng h o conc e e is i ually ze o. As o s eel, Young’s modulus Esis assumed equal o 1781 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License TABLE 2 Lis o pa ame e s o nume ical model. Conc e e 01 S eel 02 Maximum conc e e comp ession s eng h Fcm =21.59 MPa Yielding s eng h Fym =400 MPa Young modulus Ecm =21950 MPa Young modulus Es=210,000 MPa s ain a maximum comp ession s eng h εc2 =0.002 Kinema ic ha dening a io b=0.001 s ain a c ushing s eng h εcu =0.0035 Residual conc e e comp essi e s eng h =6MPa In ill panel (Pinching 04) Thickness w=120 mm Floa ing poin s de ining he eloading o he cyclic esponse: DispP =0.5, Fo ceP =0.5, uFo ceP =0, DispN =0, Fo ceN =0, uFo ceN =0 Young modulus Ew=1979.7 MPa Shea modulus Gw=791.9 MPa C acking s eng h 0.23 MPa Floa ing poin s con olling he cyclic deg ada ion: gK1,gK2,gK3, gK4,gKLim =1; gD1 gD2 gD3 gD4 gDLim =0, gF1 gF2 gF3 gF4 gFLim =0.5 Pos -capping deg ading s i ness pa ame e α=0.035 Residual s eng h pa ame e β=0.02 Equi alen usses o CLT F ic ion dampe s (S eel 02) Elas ic modulus o diagonal uss Ed=13840.3 MPa Yield s eng h (ac i a ion o ce) 25.7 MPa Elas ic modulus o e ical uss Ec=172423.5 MPa Ho izon al s i ness =299.6 kN/m Elas ic modulus o ho izon al uss Eb=329436.1 MPa Ve ical and o a ional s i nesses =0.0 210,000 MPa while he yielding s eng h ym is equal o 400 MPa. The kinema ic ha dening a io bis se equal o 0.001, while no iso opic ha dening is p esen . Based on he ma ch wi h he expe imen al esul s o he RC ame, he alue o he yielding s eng h is assumed lowe han ha p o ided by he coupon es . This s a egy allowed he nume ical model o ake in o accoun he s eng h deg ada ion caused by he ins abili y o longi udinal eba s ha occu ed du ing he expe imen al es a la ge displacemen demand. These pa ame e s led o he cyclic esponse plo ed in Figu e 6b by he ed line, which is in qui e good ag eemen wi h he expe imen al esponse (black line) a e he comple e c ushing o in ills. Once he mechanical pa ame e s o he RC membe s ha e been de e mined, he nume ical model is in eg a ed wi h he equi alen diagonal usses simula ing he in ill panel. In his second s ep, he ea u es o he in ill panel a e de e mined so ha he nume ical model ma ches he expe imen al esponse when low-medium displacemen ampli udes a e applied, and he in ill panel has no been signi ican ly damaged ye . The mechanical p ope ies a e assigned acco ding o he da a p o- ided by he expe imen al es s. Hence, he hickness is equal o 120 mm, Young’s modulus and shea modulus a e equal o 1979.7 and 791.9 MPa, espec i ely, while c acking s eng h is equal o 0.23 MPa. The pa ame e s αand β, which ule he pos -capping deg ading s i ness and he esidual s eng h, a e calib a ed o ma ch he cyclic esponse o he in illed ame p o ided by he es , and alues α=0.035 and β=0.02 a e ound. Since he expe imen al esul s o he in illed ame showed cyclic deg ada ion o s eng h and s i ness unde cyclic loading, he alues o he loa ing poin s de ining he load- ing/ eloading o he Pinching4 uniaxialMa e ial a e epo ed in Table 2. The second calib a ion p ocess is de o ed o he de e mina ion o he mechanical pa ame e s o he usses, simula ing he CLT panel, and he ic ion dampe s, so ha he s uc u al esponse p o ided by he nume ical model is in acco dance wi h he expe imen al esul s o he s eng hened RC ame. Wi h ega ds o he CLT panel, he elas ic moduli Ed,Ec,Ebo he diagonal, e ical, and ho izon al usses a e se equal o 13840.3, 172423.5, and 329436.1 MPa, espec i ely. These alues we e de e mined by scaling by 0.50 imes he elas ic modulus o he usses ha we e equi alen o he es ed CLT panel modeled by a shell elemen (C24 class). The la e was cha ac e ized by an elas ic o ho opic beha io wi h elas ic moduli equal o 6748, 4622, and 370 MPa in he X,Y,andZdi ec ions, espec i ely. Figu e 7a shows he ela ion be ween d i o he ame and sliding o he dampe loca ed a i s base. I can be obse ed ha he d i inc eases linea ly wi h he displacemen o he dampe . The ed and black lines show ha he esul s p o ided by he nume ical model and expe imen al es a e in good ag eemen . As o he dampe , he pa ame e s ha need o be de ined a e he yield s eng h o he elas oplas ic ma e ial and i s elas ic modulus. The expe imen al es shows a qui e asymme ic esponse o he dampe subjec ed o he cyclic ho izon al o ce, wi h a peak posi i e and nega i e s eng h equal o 29.44 and −22.04 kN, espec i ely. The yield s eng h assigned o he dampe in he nume ical model is se equal o 25.7 MPa, which is he a e age alue be ween he posi i e and nega i e s eng hs p o ided by he es . The elas ic modulus was calib a ed so ha he esponse o he nume ical analysis i ha o he expe imen al es , and i is se equal o 299.6 kN/m. The esponses o he dampe p o ided by he expe imen al es and he nume ical model a e epo ed in Figu e 7b,whe e he sliding o he dampe has been plo ed as a unc ion o he o al applied o ce. The wo plo s show ha he nume ical model is able o p edic accu a ely he esponse o he expe imen al es . 1782 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License (b)(a) (d)(c) -150 -100 -50 0 50 100 150 1257525-25-75-125 D i [mm] Sliding [mm] Expe imen al Nume ical -300 -200 -100 0 100 200 300 1257525-25-75-125 F [kN] Sliding [mm] Expe imen al Nume ical -300 -200 -100 0 100 200 300 1257525-25-75-125 F [kN] D i [mm] Expe imen al Nume ical 0 50 100 150 200 250 300 968064483224168421 Dissipa ed ene gy [kJ] D i [mm] Expe imen al Nume ical FIGURE 7 Compa ison o expe imen al e sus nume ical cyclic esponse o he s eng hened ame in e ms o (a) op displacemen e sus sliding o he dampe , (b) o al o ce e sus dampe displacemen , (c) o al base shea e sus op displacemen demand, (d) dissipa ed ene gy. Once he calib a ion o he pa ame e s is concluded by checking he local esponse o CLT membe s and dampe s, he en i e nume ical model is ully de ined. A lis o all he calib a ed pa ame e s is epo ed in Table 2. Hence, he global esponse in e ms o base shea and op displacemen o he ame is obse ed (Figu e 7c). The seismic esponse o he s eng hened ame is cha ac e ized by a peak o esis ance, a ound 200 kN, and a e y high elas ic s i ness due o he in ill. A e he c acking o he in ill panel, he s i ness and he la e al s eng h dec ease and end o hose o he RC ame wi h CLT and dampe s. The nume ical model ( ed line) is able o es ima e he peak s eng h and he elas ic s i ness p o ided by he expe imen al es (black line) accu a ely as well as he cyclic esponse o he ame a e c acking o he in ills. Indeed, he calib a ed nume icalmodel can accu a ely p edic he ene gy dissipa ed by he specimen du ing each cycle o imposed displacemen , wi h a maximum e o a he ending cycle lowe han 13% (Figu e 7d). 4Case S udy Buildings A se o case s udies is de ined o encompass RC- amed buildings cha ac e ized by s uc u al ea u es and seismic sho comings common in he Medi e anean building s ock. Fi s , he p oce- du e ollowed o design he RC membe s is p esen ed and all he con igu a ions o he case s udy buildings a e de ailed. Hence, he nume ical model de eloped o analyze he case s udy is desc ibed. 4.1 Design o Case S udy Buildings Since mos o he exis ing RC buildings we e cons uc ed be ween he middle and he end o he 20 h cen u y, when seismic codes we e no in o ce ye o seismic zona ion was s ill unde e olu ion, hey a e a ec ed by di e en le els o seismic de iciencies. Following his obse a ion, i s , a e e ence case s udy ame is designed o g a i y loads only. This is ep esen a i e o hose buildings ha we e no o iginally concei ed o ace seismic o ces bu we e a e wa d included in seismic-p one a eas. This building is i e-s o ey high and has a ec angula plan layou (Figu e 8) wi h dimensions equal o 28.8 and 15.5 m in he X-andY-di ec ion, espec i ely. The loo decks a e ealized by RC jois s a anged along Y-di ec ion connec ed by a 40 mm hick slab, and a e suppo ed by he ou se en-bay ames o ien a ed along he X-di ec ion. Only wo ames a e disposed along he Y-di ec ion, o close he pe ime e o he plan layou . Since he majo i y o beams a e disposed along he X-di ec ion and columns oppose hei s ong ine ia axis mainly along he X-di ec ion, he la e al s i ness and s eng h along he X-di ec ion a e signi ican ly la ge han hose along he Y-di ec ion. Such a di e ence in he wo di ec ions o he building is a ea u e ha o en cha ac e izes s uc u es designed wi hou seismic p esc ip ions. The dis ibu ion o la e al s i ness and s eng h is symme ic wi h espec o bo h axes passing h ough he geome ic cen e o he plan layou , meaning ha he s uc u al esponse o ho izon al seismic o ces is pu ely ansla ional. Dead and li e loads on s uc u al elemen s a e de e mined acco ding o he nominal alues p o ided in [39]. The allowable s ess me hod is ollowed o size he c oss sec ions and s eel ein o cemen o membe s, as p esc ibed by he I alian code en o ced in 1974 [29]. Columns a e designed conside ing axial o ce only, while beams a e designed o bending momen and shea o ce. The in e nal axial o ce No columns and he dis ibu ed loads es ing on beams a e e alua ed acco ding o he ibu a y a ea concep . The cha ac e is ic comp essi e cubic s eng h Rck o conc e e is equal o 25 MPa (co esponding o cylinde s eng h ck equal o 20 MPa o s eng h class C20/25). S eel g ade Feb38K wi h a cha ac e is ic yield s ess yk =375 MPa 1783 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License X- ame models Y- ame models (a) (b) (c) Uns eng hened ame Sp ead e-CLT Local ex ended e-CLT Local na ow e-CLT 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N Δ 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N θ / θ NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N θ / θ NC Beams 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N VEd/V Rd Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N V Ed /V Rd Beams 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N Δ 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N θ / θ NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 N θ / θNC Beams 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N V Ed /V Rd Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 N V Ed /V Rd Beams FIGURE 13 Dis ibu ion along he heigh a he a ainmen o NC limi s a e in he uns eng hened in illed ame o (a) d i demand; (b) cho d o a ion D/C a io o columns and beams; (c) shea o ce D/C a io o columns and beams. building, while in he Y- ame model, wi h espec o he o he wo e-CLT con igu a ions, i p o ides a simila o a lowe e ec on he seismic esponse. The dis ibu ions along he heigh o he uns eng hened ba e and pilo is building o maximum d i demand, cho d o a ion D/C a io in columns, and cho d o a ion D/C a io in beams a e plo ed o he ela ed PGA capaci ies in Figu e 15a–c, espec i ely. The analysis o he d i demand and he cho d o a ion D/C a io in columns shows ha X- ame models o bo h ba e and pilo is buildings in he uns eng hened con igu a ion expe ienced concen a ion o damage a one o wo s o eys, while a seismic demand a he dis ibu ed along he heigh is obse ed in he Y- ame models. When applied in he sp ead o local ex ended con igu a ion, he e-CLT sys em in he X-di ec ion success ully educed (by abou 40%) bo h he d i demand and he cho d o a ion demand o columns o he s o eys wi h he la ges displacemen demands. I e-CLT sys em is loca ed acco ding o he local na ow con igu a ion, d i demand and cho d o a ion demand in columns o he X- ame model concen a e a a single s o ey ( he hi d in he ba e building and he ou h in he pilo is building) and become e en la ge han hose o he buildings in he uns eng hened con igu a ion. This beha io s ems om he ac ha he e-CLT sys em was loca ed only a he ou h s o ey in he ba e building and he hi d s o ey in he pilo is building. Thus, he maximum seismic demand shi om hese s o eys o he adjacen ones, making he local na ow con igu a ion no e ec i e om a global poin o iew. In he Y- ame model, he local na ow con igu a ion shows he leas impac on he seismic esponse (abou 15% educ ion on maximum d i and cho d o a ion demands). Wi h ega ds o beams, he e-CLT sys em leads o a educ ion o he cho d o a ion demand in beams only in he Y- ame model (−36% and −43% wi h sp ead con igu a ion in he ba e and pilo is building, espec i ely), whe e he displacemen demand was a he dis ibu ed along he heigh and he beams expe ienced a cho d o a ion demand compa able o ha o columns (as shown in Figu e 9). 1790 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License Ba e ame (wi hou in ills) Pilo is ame X- ame models (a) (b) Y- ame models (c) (d) Uns eng hened ame Sp ead e-CLT Local ex ended e-CLT Local na ow e-CLT 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 P(LS) PGA [g] 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 P(LS) PGA [g] 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 P(LS) PGA [g] 0 0.2 0.4 0.6 0.8 1 0 0.2 0.4 0.6 0.8 P(LS) PGA [g] FIGURE 14 F agili y cu es o NC limi s a e o he case s udy buildings be o e and a e he in oduc ion o e-CLT. Gene ally speaking, in he s eng hened X- ame models, espe- cially in he case o in illed and pilo is building, he sp ead o local ex ended con igu a ions (1) educe he d i demand con- cen a ion ha cha ac e izes he esponse o he uns eng hened coun e pa and (2) lead o an inc eased o he cho d o a ion demand in he columns o he s o eys wi h lowe d i demands, which a e o ced o pa icipa e in he dissipa ion p ocess. Thanks o he la ge numbe o RC membe s in ol ed in he dissipa i e p ocess and he addi ional con ibu ion o he dissipa i e capaci y p o ided by he dampe s, he esponse o he ame is d as ically educed, and he PGA capaci y is signi ican ly enhanced. In he case o Y- ames, whe e damage is no localized a a ew s o eys e en in he uns eng hened con igu a ion, he e-CLT sys em educes he cho d o a ion demand mainly hanks o he addi ional sou ce o seismic ene gy dissipa ion gi en by he dampe s, hus he bene i achie ed by he ame is less ema kable. 7.2 Mean Annual F equency o Exceedance o Case S udy Buildings a NC and SD Limi S a e The seismic esponse o he analyzed case s udy buildings is also assessed in e ms o mean annual equency o exceedance o he NC and SD limi s a e conside ing he X-andY- ame models. Fo all he conside ed cases, Figu es 16 and 17 show he a io o he mean annual equency o exceedance λo SD and NC limi s a es wi h espec o he ele an limi alues λ eq equi ed by [45]. I λ/λ eq o e comes uni y, he co esponding e i ica ion is no ul illed. The a io λ/λ eq is e alua ed conside ing he ou agg ega ion ules conside ed o he cons uc ion o he agili y cu es: only duc ile ailu e modes in all membe s, bo h duc ile and agile ailu e modes in all membe s, o all ailu e modes only in columns o all ailu e modes only in beams. The la ges alue among he ou a ios is he one ha quan i ies he seismic pe o mance o he ame. The ed his og am e e s o he building in he uns eng hened con igu a ion, while he ha ched his og ams e u n he seismic pe o mance achie ed by he in oduc ion o e-CLT in he local na ow (g ey hin ha ch), local ex ended (black hin ha ch) and sp ead (black hick ha ch) con igu a ions. When seismic exci a ion ac s in he X-di ec ion (Figu e 16), he building in he uns eng hened con igu a ion is a om ul illing ei he he NC o he SD limi s a e and shows alues o λ/λ eq always much la ge han 2.0. The e-CLT in he local na ow con igu a ion inc eases he alues o λ/λ eq, hus esul ing in an ine ec i e in e en ion, which con i ms he conclusions o Sec ion 7.1. Consis en ly, e-CLT in bo h he sp ead and he local ex ended con igu a ions signi ican ly enhances he seismic pe o mance o all he conside ed cases and dec eases he alue o λ/λ eq o he uns eng hened buildings by mo e han 50%. Fu he mo e, he ull upg ading, ha is he alue o λ/λ eq igo ously lowe han one, a bo h SD and NC limi s a es, is achie ed o all he conside ed buildings when he e-CLT sys em is loca ed acco ding o he local ex ended con igu a ion. In he case o seismic exci a ion ac ing in he Y-di ec ion, he buildings in he uns eng hened con igu a ion ul ill o a e e y close o ul illing NC and SD limi s a e e i ica ions. Anyway, he in oduc ion o he e-CLT sys em leads in all he cases o a signi ican educ ion o λ/λ eq,up oalmos 46%wi h espec o he building in he uns eng hened con igu a ion. 8P inciples and Guidelines o a Design P ocedu e Based on he esul s o he expe imen al es s and nume ical in es iga ion, a design p ocedu e is p oposed in his Sec ion. The nonlinea s a ic me hod o analysis, which is a well-known 1791 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License Ba e ame X- ame models Y- ame models Pilo is ame X- ame models Y- ame models (a) (b) (c) Uns eng hened ame Sp ead e-CLT Local ex ended e-CLT Local na ow e-CLT 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Beams 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Beams 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Beams 0 1 2 3 4 5 6 0% 1% 2% 3% 4% N 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Columns 0 1 2 3 4 5 6 0.0 0.5 1.0 1.5 2.0 N / NC Beams θ Δ Δ Δθθ θθ θθ θθθθ θθ θθ θθ FIGURE 15 Dis ibu ion along he heigh a he a ainmen o NC limi s a e in he uns eng hened ame o (a) d i demand; (b) cho d o a ion D/C a io o columns; (c) cho d o a ion D/C a io o beams. p o essional ool also allowed by seismic codes, is used o he p edic ion o he seismic esponse. In pa icula , he p elimi- na y seismic assessmen o he uns eng hened building can be pe o med by pusho e analysis, which is able o es ima e he collapse mechanism and he co esponding dis ibu ion along he heigh o he d i demand. Hence, he loca ion o he e-CLT sys em can be de e mined. I he d i demand is concen a ed a one s o ey (o a ew s o eys), he e-CLT sys em ollows he local ex ended con igu a ion. Ins ead, i he d i demand is widesp ead among he s o eys, he e-CLT sys em can be loca ed acco ding o he sp ead con igu a ion. A he selec ed s o eys, he numbe and loca ion o CLT panels depend on a chi ec u al ea u es o he açade, pa icula ly he numbe o spans wi hou la ge openings. A his s age o he design p ocedu e, he ac i a ion o ce o he dampe s is assumed equal o a easonable alue, o example, ha o he expe imen al es , and he s i ness o CLT panels is assumed in ini e. Hence, a second pusho e analysis is pe o med o assess he seismic esponse o he RC ame wi h he e- CLT sys ems so a designed. Gi en a a ge alue o PGA, he co esponding seismic demand o he s eng hened building is de e mined by nonlinea s a ic me hods o analysis (e.g., Capaci y spec um me hod o N2 me hod). I he a ge limi s a e has been o e come, he ac i a ion o ce o he dampe has o be inc eased, so ha he la e al s eng h o he s eng hened building inc eases in u n. E en ually, he pusho e analysis can be i e a i ely epea ed un il he s eng hened building sa is ies he a ge limi s a e. A e he ac i a ion o ce o he dampe has been designed, he size o he CLT panel and he s oke o he dampe can be de e mined o ul ill he d i demand a he a ge limi s a e. Speci ically, o ensu e ha he dampe s ully ac i a e and 1792 o 1796 Ea hquake Enginee ing & S uc u al Dynamics,2025 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License Ba e ame (wi hou in ills) In illed ame Pilo is ame e a s imilCNe a s imil DS Uns eng hened ame Sp ead e-CLT Local ex ended e-CLT Local na ow e-CLT 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -66.7% -67.7% 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -54.8% -47.4% 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -69.2% -68.3% 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -74.3% -64.0% 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -58.4% -58.3% 0 0.5 1 1.5 2 2.5 θ θ+V Col Beam / eq -67.9% -66.4% FIGURE 16 Ra io o mean annual equency o exceedance o X- ame models. Ba e ame (wi hou in ills) In illed ame Pilo is ame NC limi s a e SD limi s a e Uns eng hened ame Sp ead e-CLT Local ex ended e-CLT Local na ow e-CLT 0 0.5 1 1.5 2 2.5 3 θ θ+V Col Beam λ / λ eq -28.6% -1.3% 0 0.5 1 1.5 2 2.5 3 θ θ+V Col Beam λ / λ eq -30.2% -43.5% 0 0.5 1 1.5 2 2.5 3 θ θ+VCol Beam λ / λ eq -1.8% -26.3% -33.7% 0 0.5 1 1.5 2 2.5 3 θ θ+V Col Beam λ / λ eq -5.2% -24.8% 0 0.5 1 1.5 2 2.5 3 θ θ+V Col Beam λ / λ eq -40.4% -45.9% 0 0.5 1 1.5 2 2.5 3 θ θ+V Col Beam λ / λ eq -10.0% -42.7% -31.1% FIGURE 17 Ra io o mean annual equency o exceedance o Y- ame models. dissipa e ene gy, he in-plane s i ness o he CLT panel mus be se la ge enough o minimize he de o ma ion o he panel i sel and u n he d i demand mainly in o sliding displacemen o he dampe s. Hence, he CLT panel can be sized so ha he ho izon al ela i e displacemen be ween i s bo om and op sides induced by he ac i a ion o ce o he dampe s is equal o a small a e o he maximum d i demand a he a ge limi s a e. In u n, he s oke o he dampe is se equal o he di e ence be ween he d i demand a he a ge limi s a e and he ela i e displacemen be ween op and bo om sides o he panel. Since he CLT panels a e expec ed o emain elas ic du ing he seismic ac ion, s eng h and s abili y o he panels ha e o be e i ied as well. 1793 o 1796 10969845, 2025, 6, Downloaded om h ps://onlinelib a y.wiley.com/doi/10.1002/eqe.4334 by Uni e si ã Di Ca ania, Wiley Online Lib a y on [03/10/2025]. See he Te ms and Condi ions (h ps://onlinelib a y.wiley.com/ e ms-and-condi ions) on Wiley Online Lib a y o ules o use; OA a icles a e go e ned by he applicable C ea i e Commons License Once he e-CLT sys em has been ully designed (loca ion, numbe , size o CLT panels, ac i a ion o ce, and s oke o he dampe s), he s uc u al esponse o he s eng hened building can be assessed by pusho e analysis. I he d i demand o he s eng hened building a he a ge limi s a e s ill o e comes he capaci y, he ac i a ion o ce and/o he size o he CLT panel can be inc eased. Wi h ega ds o he uppe connec ions, hese can be ealized by con en ional mechanical and/o chemical ancho s widely a ail- able in he ma ke . The connec ion can be designed as las s ep o he design p ocedu e, o sus ain (1) he e ical eac ion o ce due o he sel -weigh o he CLT panel, plus (2) he ho izon al eac ion o ce ha esis s he ac i a ion o ce o he dampe s, plus (3) he e ical eac ion o ce ha a ises o balance he momen caused by he eccen ici y be ween o ce ansmi ed by dampe s and ho izon al eac ion o ce o connec ions. These o ces a e ob ained om he h ee igid body equilib ium equa ions o he CLT panel. The s eng h o he connec ions can be e i ied acco ding o p esc ip ions a ailable in seismic codes. 9 Conclusions The pape p oposes he e-CLT sys em as a e o i sys em sui able o an in eg a ed ene gy and seismic app oach o upg ading exis ing RC- amed building s uc u es. The quasi-s a ic expe - imen al es s ca ied ou on wo ull-scale one-s o ey one-bay RC in illed ames, wi hou and wi h e-CLT, demons a ed ha he e o i sys em beha es unde cyclic loading as planned. In pa icula , du ing he loading p o ocol, (1) he ic ion dampe s, connec ing he CLT panel o he RC beam, success ully ac i a ed and slid, (2) he CLT panel and he ic ion dampe as ening sys em sus ained he o ce deli e ed by he dampe emaining in he elas ic ange o beha io , (3) he join ac ion o CLT panel and dampe p o ided he RC ame wi h addi ional la e al s i ness, la e al s eng h and, e en mo e, ene gy dissipa ion capaci y. The ac i a ion o he dampe occu ed o he alue o o ce assumed in design and i s cyclic esponse was s able, wi hou app eciable s eng h deg ada ion e en a e many cycles o loading and unloading. A he end o he es , he dampe did no exhibi e idence o yielding, local ins abili ies, o ano he kind o damage, hus con igu ing i as a damage- ee de ice ha does no need o be eplaced e en a e a s ong g ound mo ion. A nume ical model o he RC in illed ame equipped wi h e- CLT sys em has been de eloped in OpenSees en i onmen and calib a ed based on he esul s p o ided by he expe imen al es s. A p ocedu e based on a sub-componen app oach was es ablished o he calib a ion o he model. The p ocedu e led o he calib a ion o he pa ame e s con olling he esponse o he componen s o he RC ame +e-CLT in subsequen s eps. Fi s , he mechanical p ope ies assigned o he elemen s simula ing he RC membe s a e calib a ed assuming as a ge he cyclic esponse, unde la ge ampli ude displacemen s, o he uns eng hened RC in illed ame (wi hou e-CLT). In he second s ep, he pa ame e s o in ill panel a e calib a ed o i he expe i- men al esponse o he uns eng hened RC ame unde low and in e media e ampli ude displacemen s. In he hi d ( inal) s ep, he pa ame e s ha con ol he beha io o he CLT panel a e calib a ed based on he expe imen al esponse o he ame wi h e-CLT. The cyclic esponse p o ided by he nume ical models i s well he expe imen al esponse o bo h he uns eng hened and s eng hened RC ame o low, in e media e, and la ge displacemen cycles: elas ic beha io , c acking o in ill panels and subsequen la e al s eng h deg ada ion, esidual s eng h o RC ame +addi ional s eng h p o ided by e-CLT. Finally, unning he nume ical model equi es a low compu a ional bu den, which makes i sui able o model mul is o ey buildings and pe o m ex ensi e pa ame ic in es iga ions. A pa ame ic analysis was conduc ed on i e-s o ey ames wi h h ee di e en con igu a ions o in ills (ba e ame, wi h ull heigh in ills, and pilo is ame) and wo di e en ypes o global nonlinea beha io (d i and cho d o a ion demand concen a ed a ew s o eys o widesp ead along he heigh o he ame). The esul s allowed he quan i ica ion o he impac o he e-CLT sys em on he seismic esponse o ealis ic RC buildings and p o ided basic guidelines o he design o seismic upg ading by e-CLT. I was ound ha he e ec i eness o he con igu a ion o e-CLT is ela ed o he global nonlinea beha io o he RC building o be s eng hened. The local ex ended con igu a ion (e- CLT in oduced in he s o ey whe e he d i demand is maximum plus one s o ey below and one s o ey abo e) is sui able o upg ade RC amed buildings wi h a concen a ion o d i demand a a ew s o eys. Ins ead, i he d i demand is widesp ead along he heigh o he building, he sp ead con igu a ion (e-CLT in oduced a all s o eys) should be p e e ed. The pusho e analysis can p edic he ype o global nonlinea beha io o he building o be s eng hened and, he e o e, can be used o selec he mos app op ia e con igu a ion o e-CLT. The applica ion o e-CLT on amed s uc u es wi h concen a ion o demand led o an inc ease o PGA capaci y by up o 40% and educed he mean annual equency o exceedance o he conside ed limi s a es by up o 74%. When e-CLT was used o upg ade amed s uc u es wi h widesp ead seismic demand, he inc ease o PGA capaci y and he dec ease o mean annual equency o exceedance o he conside ed limi s a es we e up o 15% and 46%, espec i ely. The hi d con igu a ion o e o i , named local na ow con igu a ion (e-CLT sys ems s ic ly in oduced in he s o ey whe e he d i demand is maximum), esul ed o be he leas e ec i e and somewha de imen al. Indeed, on one side, he e-CLT sys em educed he seismic demand a he s o ey whe e i was in oduced bu , on he o he hand, shi ed he seismic demand o he adjacen s o eys, which expe ienced an ab up and signi ican inc ease in he d i demand. Hence, he e-CLT sys em esul ed o be a p omising seismic upg ading echnique and he pa ame ic analysis conduc ed on ealis ic buildings con i med his esul . In he end, based on he expe imen al and nume ical esul s, p inciples and s eps o design seismic upg ading by e-CLT a e p o ided. Acknowledgmen s This pape was ca ied ou in he amewo k o he “Ene gy and seismic a o dable eno a ion solu ions” (e-SAFE) p ojec , which has ecei ed unding om he Eu opean Union’s Ho izon 2020 esea ch and inno a ion p og am unde g an ag eemen No. 893135. 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