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NEES Small-Group Research Project: Seismic Behavior, Analysis and Design of Complex Wall Systems (NSF Grant CMMI-0421577) Laura Lowes, Dawn Lehman, Anna Birely, Joshua Pugh, UW Dan Kuchma, Chris Hart, Ken Marley, UIUC UNIVERSITY of ILLINOIS
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Research Objective Establish the seismic performance of modern reinforced concrete walls and develop the response and damage-prediction models required to advance performance- based design of these systems Photo courtesy of MKA Seattle
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Research Activities to Date Experimental testing: – Testing of four planar walls completed in 2008 – Testing of a planar coupled wall to be completed Nov. 2010 – Testing of three c-shaped walls to be completed in 2011 Simulation: development, calibration and evaluation of – Elastic, effective stiffness models – Fiber-type beam-column models w/ and w/o flexure-shear interaction – Two-dimensional continuum models Performance-prediction models: – Development of data relating damage and demand – Development of fragility functions for walls
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Experimental Testing Of Planar Walls
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Experimental Test Program Prototype structure Experimental test matrix Core Wall under Construction (Courtesy of MKA, Seattle)
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NEES Experimental Testing Bottom three stories of 10-story of a planar prototype wall. Shear and moment applied to simulate lateral load distribution in 10-story prototype Target axial load of 0.1A g f c ’.
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Planar Wall Test Specimens 1/3-scale with details reflecting modern construction practice. Boundary Elements (3.5%) Splice at Base of Wall Full Scale: 12’ high/18 in. thick Lab: 4’ high/ 6 in. thick
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Planar Wall Test Matrix Moment-to Shear Ratio Distribution of Reinforcement Splices? STUDY PARAMETERS Wall 1 Wall 2 Wall 3 Wall 4 M b = 0.71hV b V b = 2.8 f’c = 0.7V n UNIFORM NO YES BE at EDGE YES M b = 0.50hV b V b = 4.0 f’c = 0.9V n M b = 0.50hV b V b = 4.0 f’c = 0.9V n M b = 0.50hV b V b = 4.0 f’c = 0.9V n
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Global Response: Base Moment v. 3 rd Floor Drift MnMn % Drift M, k-ft MnMn MnMn MnMn
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Response of PW 4: No Splice
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Final Damage States for Planar Walls Wall 1: V b = 3.6 f’c 1.5% drift (3 rd story) 2.1% drift (10 th story) Wall 2: : V b = 5.0 f’c 1.5% drift (3 rd story) 1.8% drift (10 th story) Wall 3: V b = 4.5 f’c 1.25% drift (3 rd story) 1.6% drift (10 th story) Wall 4: V b = 4.6 f’c 1.0% drift (3 rd story) 1.4% drift (10 th story)
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Experimental Testing of a Coupled Wall
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Objective: To determine what is the seismic behavior of a modern coupled wall Review inventory of modern coupled walls – 17 buildings with coupled-core wall systems designed for construction in CA or WA in last 10 years. – Information collected included geometry, aspect ratios, reinforcement ratios, degree of coupling, shear demand-capacity ratio, pier wall axial demand-capacity ratio, etc. Review previous experimental tests – Numerous tests of coupling beams with different reinforcement layouts, ratios and confinement details. – Only seven (7) coupled-wall tests found in the literature. – Coupled wall test specimens are not representative of current design practices. Design and evaluate multiple 10-story planar coupled walls – Design walls following the recommendations of the SEAOC Seismic Design Manual, Vol. III, using ASCE 7-05, and meeting requirements of ACI 318-08. – Progression of yielding and failure mechanism was evaluated via continuum finite- element analysis using VecTor2. – Design was updated to ensure yielding of coupling beams and wall piers.
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Coupled Wall Test Specimen Specimen is bottom three stories of a 10-story planar coupled wall. Coupling beams have aspect ratio of 2.0 and diagonal reinforcement. Seismic loading results in yielding in coupling beams and wall piers. Pier walls are capacity- designed for shear. Coupling beams: aspect ratio = 2.0 diag = 1.25% V n = Boundary Element long = 3.5% trans = 1.4% Web long = 0.27% horz = 0.27%
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Construction
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Testing of the Coupled Wall Specimen ∆ x - prescribed (i.e. disp. control) F z,total = constant - chosen as 0.1f c A g M y,total = k*F x,total - k is defined by chosen lateral load dist. - F x measured in lab for given x (edited image) x,F x,total M y,total F z,total
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Testing of the Coupled Wall Specimen ∆ x = (∆ x1 + ∆ x2 )/2 - prescribed (i.e. disp. control) F z1 + F z2 = constant - chosen as 0.1f c A g M y,total = k*(F x1 + F x2 ) - k is defined by chosen lateral load dist. F x2 – F x1 = f(F x,tot ) - f(F x,tot ) is determined by analysis before testing θ y1 = n*∆ x1 ; θ y2 = n*∆ x2 - n is determined by analysis before testing (edited image)
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Validation of the Loading Protocol Compare simulated response of 10-story prototype and 3-story laboratory test specimen 3 rd story load versus displacement response prototype specimen
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Validation of the Loading Protocol Compare simulated response of 10-story prototype and 3-story laboratory test specimen bottom 3 stories of 10-story prototype 3-story test specimen Principal concrete compressive strain field at 0.75 in. lateral displacement
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Simulation: Model Development and Evaluation
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Experimental Database 66 wall tests from 13 different test programs 60% are slender (AR > 2); 40% are squat (AR < 2) 78% tested cyclically; 22% tested monotonically Failure modes – Slender walls: 85% in flexure; 10% in shear; 5% in flex-shear – Squat walls: 40% in flexure; 60% in shear Design parameters: ParameterAverageMin.Max. f ’ c (psi) 5400237010250 vert (%) 1.900.403.00 horz (%) 0.600.001.70 P/A g f ’ c 0.040.000.20 V u f ’ c (psi) 5.701.1312.80
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Simulation Models and Software OpenSees fiber-type beam-column models – Force-based, distributed plasticity element without flexure-shear interaction 1 and with linear, calibrated shear flexibility 2 – Displacement-based, lumped-plasticity with flexure-shear interaction 3 Two-dimensional continuum model – Modified compression field theory as implemented in VecTor2 4 1.Neuenhofer and Filippou (1997, 1998), Taucer et al. (1991), Spacone and Filippou (1992) 2.Oyen (2006) 3.Massone et al. (2006), Massone (2006) 4.http://www.civ.utoronto.ca/vector/, Wong and Vecchio (2003)http://www.civ.utoronto.ca/vector/
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Ratio of Simulated-to-Observed Response Wall Config. Stiffness to YieldMaximum StrengthDisplacement Capacity Force- Based Flex- Shear 2D Force- Based Flex- Shear 2D Force- Based Flex- Shear 2D Rect. Slender (30/66) 0.91 (0.21) 1.23 (0.21) 1.02 (0.23) 0.99 (0.17) 1.07 (0.13) 1.09 (0.08) 0.66 (0.36) 1.00 (0.38) 1.14 (0.32) Barbell Slender (9/66) 1.55 (0.12) 1.72 (0.16) 1.36 (0.10) 1.00 (0.08) 1.18 (0.11) 1.01 (0.08) 0.41 (0.29) 2.23 (0.33) 1.12 (0.30) Rect. Squat (15/66) 0.89 (0.20) 1.63 (0.12) 1.28 (0.20) 1.00 (0.17) 1.01 (0.12) 1.02 (0.07) 1.11 (0.42) 0.65 (0.28) 0.69 (0.33) Flanged Squat (12/66) --- 3.99 (0.52) 1.57 (0.37) 1.25 (0.13) 2.49 (0.53) 0.49 (0.65) 0.66 (0.53)
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Damage Prediction Models Initial spalling Spalling at base Steel fracture
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Experimental Database 66 wall tests from 18 different test programs 100% are slender with AR > 2 83% tested cyclically; 17% tested monotonically 92% tested uni-directionally, 8% tested bi-directionally Design parameters: ParameterAverageMin.Max.Std. Dev. Scale0.40.25.00.5 f ’ c (psi) 55003000113002000 be (%) 3.50.811.42.0 web (%) 0.60.12.30.6 horz (%) 0.50.21.40.2 P/A g f ’ c 0.10.00.20.05 V u A cv f ’ c ) (psi) 4.81.011.02.0 VuVnVuVn 0.70.21.40.3
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Damage States / Method of Repair Damage State DescriptionMethod of Repair DS 1 Initial cracking Initial yielding of reinforcement Cosmetic Repair DS 2 Concrete crack widths > 1/16 in.Epoxy Injection of Cracks DS 3 Spalling that does expose long. reinforcement Epoxy Injection of Cracks and Patching of Concrete DS 4 Exposed longitudinal reinforcement Vertical cracks/splitting Cracks ≥ 1/8” Replace Concrete DS 5 Core crushing Bar buckling and/or fracture Web crushing Bond slip failure Shear failure Replace Wall
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Engineering Demand Parameters Maximum Drift – displacement at top of specimen / specimen height Maximum 1 st Story Drift – Assume full-scale is a story height of 10 ft. and wall thickness of 12 in. – Assume stiffness above the 1 st of the wall is defined by 0.10G c A cv (shear) and average E c I g for the entire wall. – 1 st story drift is then calculated using displacement measured at the top of the wall specimen and above assumptions. Maximum Rotation Demand for a Lumped-Plasticity Model – Hinge at base of the wall has a hinge length of ½ L w – Assume stiffness of the remaining height of the wall is defined by 0.50E c I g (flexure) and 0.10G c A cv (shear) – Hinge rotation is then calculated using displacement measured at the top of the wall specimen and above assumptions.
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Fragility Functions for Slender Walls Damage state – demand data are used to calibrate lognormal CDF Lognormal Distribution Parameters Damage State Median Drift (%) Dispersion DS10.090.78 DS20.630.85 DS30.960.50 DS41.100.64 DS51.600.59
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Investigation of the Impact of Design Parameters on Damage Progression Objective: Develop suites of fragilities for walls with different design parameter values ParameterImpact Axial load ratioSignificant Shear demandSignificant Aspect ratio / shear span (M base /V base /L w )Significant Displacement history (uni- versus bi- directional) Apparently significant* Shape (planar, flanged, c-shaped, etc.)Minimal ScaleMinimal Shear demand-capacity ratioMinimal DS versus drift with data grouped by axial load ratio * Too few test specimens with bi-directional displacement histories
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Conclusions Laboratory testing of rectangular planar walls – Drift capacity of rectangular concrete walls with modern detailing and representative load distributions ranges from 1.0% to 1.5% (1.4% to 2.0% at roof of 10-story structure). – Damage was concentrated in the first story; other stories cracked but otherwise pristine. – Drift was due to base rotation (15-25%), flexure (55-60%), and shear (~25%). Flexural deformation of 3 rd floor was much smaller than 1 st and 2 nd.
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Conclusions Simulation – Strength Planar walls: All models provide accurate and precise simulation of strength The continuum model also provides acceptable accuracy and precision for flanged, squat walls – Stiffness to yield For rectangular, slender walls the models provide reasonably accurate and precise simulation of stiffness: error in simulated stiffness ranges from 23% to 2% with a cov of approximately 20% The continuum model provides the best accuracy and precision for all of the wall configurations considered – Displacement capacity None of the models does a particularly good job of simulating displacement capacity for all of the wall configurations considered The continuum models provides acceptable accuracy and precision for slender walls; errors are less than 15% with a cov of approx. 30%
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Conclusions Performance-based design – For slender walls, the median drift at which wall replacement is required is 1.6%
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THANK YOU! Questions?
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Coupling Beam Reinforcement Ratio NEESR Wall
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Evaluation of Response Using Local Instrumentation Data
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Krypton and Disp. Transducer Data Drift at top of specimen Wall 1 Wall 2 Wall 3Wall 4 Cracking Yielding 3 rd floor shear 2 nd floor shear 1 st floor shear 3 rd floor flexural 2 nd floor flexural 1 st floor flexural Base rotation Base slip Contribution to total drift (%)
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Wall 4 Shear Strain from Krypton Data
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