INTERNATIONAL JOURNAL OF CIVIL AND STRUCTURAL ENGINEERING Volume 1, No 3, 2010

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Prbabilistic Analysis f Lateral Displacements f Shear in a 20 strey building Samir Benaissa 1, Belaid Mechab 2 1 Labratire de Mathematiques, Université de Sidi Bel Abbes BP 89, Sidi Bel Abbes 22000, Algerie. 2 LMPM, Department f Mechanical Engineering, Université de Sidi Bel Abbes BP 89, Sidi Bel Abbes 22000, Algerie. benaissamir@yah.fr ABSTRACT Lateral displacements f shear wall (SWII) analyzed by finite element methd. Keywrds: Prbabilistic, vibratin strengthened shear wall, Finite element methd, Cmpsite plates 1. Intrductin In many areas arund the wrld, reinfrced cncrete (RC) buildings designed using cdes that are nw knwn t prvide inadequate safety under seismic frces are ptential hazards. In such areas, the number f RC buildings built prir t 1980 utnumbers thse that are built accrding t the newer cdes. Therefre, these structurally deficient buildings shuld be retrfitted t withstand earthquake frces in cmpliance with mdern design cdes. The lateral lads that arise frm the effects f wind and earthquakes, are resisted by shear walls. These latter, are usually built ver the whle height f the buildings, as series f walls cupled by beams r slabs r as a central cre structure. Pagnini and Slari used the first rder and the secnd rder techniques in cmputing the acceleratin respnse f a square plan multistry steel building excited by the wind lading. Obviusly, the main purpse f these methds is t determine the secnd rder statistical quantities f dynamic structural respnse, such as the mean, the standard deviatin, etc. As far as the prbability density functin (PDF) f the respnse is cncerned, mst f these methds will be met with difficulty. Extensive testing has shwn that externally bnded carbn fiber reinfrced plymer (CFRP) laminates are particularly suited fr imprving the shrt term behavir f deficient reinfrced cncrete beams and slabs. Als nte that this technique f reparatin has been als used in aircraft structures. 373

Lateral displacements f shear wall (SWII) analyzed by finite element methd. 2. Gemetrical and mechanical prperties The numerical values f the gemetrical and material parameters were presented in Table 1 and Figure 1 fr shear walls structures: SWII.. Table 1: Material prperties f the shear walls in the cnvergence studies SWII SWII Mass density q (kg/m 2 ) 2400 Yung s mdulus E 11 = E 22 (GN m 2 ) 15 Shear mdulus G 12 (GN m 2 ) 6.25 Figure1: Shear wall structure SWII un strengthened 3. Numerical results and discussin Numerical results are presented in this study analyzed by finite element methd fr shear walls strengthened by a bnded cmpsite thin plate. We cnsider in the first example the free vibratin fr typical unstrengthened shear wall structure. Results f methd are listed in Table 2 and cmpared with thse f Syngellakis and Papulia. It can be seen frm the cmparisn that there is very little difference in the three first natural frequency results. 374

Table 2: Cnvergence and cmparisn studies f first five natural frequencies (Hz) fr shear wall type SWII N. mde Present study (FEM) Syngellakis and Papulia 1 2 3 4 5 0.902 5.630 10.430 12.60 18.52 0.897 5.624 10.417 15.749 The dimensins f shear wall structure SWII Strengthened and unstrengthened are shws in Figure 2 the results presented in Figure3 Figure2: Shear wall structure SWII Strengthened (a), unstrengthened (b) 375

15 12 Height (in) 9 6 3 unstrengthened strengthened 0 0,00 0,25 0,50 0,75 1,00 1,25 1,50 1,75 2,00 2,25 2,50 lateral displacement (10 3 x in) Figure3: Lateral displacements f shear wall (SWII). Figure 3 Shws the Effect f the bending and vibratin analysis f shear wall structures strengthened by bnded cmpsite plates and unstrengthened can be bserved. The Lateral displacement f shear wall (SWII) is prprtinally with height. 4. Prbabilistic analysis 4.1. Prbabilistic results and discussins Lateral displacements f shear wall (SWII) analyzed by finite element methd In this paper a methd is presented t calculate the prbability f a prblem, f which ne r mre f the mdel parameters are randm variables, i.e. statistically determined. Mathematically this can be stated as: def def F ( j ) = Pr U ( X ) < j = ƒ ( x ) dx (14) U U ( X ) < j x 376

f(x) the Jint Prbability Density Functin (JPDF) f the vectr f randm variables X, such as material parameters, dimensins and lads. The displacement U shuld be evaluated by the prbability r the prbability density. ƒ ( j ) = df U U ( j ) / dj Where F u (j 0 ) is the cumulative prbability distributin functin f U and ƒ x (x) is the knwn jint prbability density functin f X. Figure4 presents similar results f prbability Gaussian distributins f randm variables. U: Lateral displacements f shear wall structure (SWII). Prbability Density f U 1,0 0,8 0,6 0,4 0,2 Mean Gauss distributins 0,0 0,0 0,5 1,0 1,5 2,0 2,5 3,0 3,5 4,0 U (10 3 x in) 4. Cnclusins Figure 4: Presents similar results f prbability density f U Lateral displacements f shear wall (SWII) analyzed by finite element methd. The Effect f the bending and vibratin analysis f shear wall structures strengthened by bnded cmpsite plates and un strengthened can be bserved. The Lateral displacement f shear wall (SWII) is prprtinally with height. Prbability density functins f U see Figure 4 presents similar results f prbability Gaussian distributins f randm variables. 377

References 1. Pagnini, L.C., Slari, G., 1998. Service ability criteria fr wind induced acceleratin and damping uncertainties. J.Wind Eng.Ind. Aerdyn.74,pp 1067 1078 2. Shahaway MA, Beitelman T, Arckiasamy M, Swrirajan R. Experimental investigatin n structural repair and strengthening. f damaged prestressed cncrete slabes utilizing external bnded carbn laminates. Cmps B 1996;27:pp 217 24 3. Shen H S, Chen Y, Yang J. Bending and vibratin characteristics f a strengthened plate under varius bundary cnditins. Eng Struct 2003; 25:pp 1157 68. 4. Megueni A, Tunsi A, Bachir Buidjra B, Serier B. The effect f a bnded hygrthermal aged cmpsite patch n the stress intensity factr fr cracked metallic structures. Cmps Struct 2003:pp 171 6. 5. Baker AA, Callinan MJ, Jnes R, Williams JG. Repair f Mirage aircraft using BFRP crack patching technlgy. Ther Appl Fract Mech 1984;2:pp 1 16. 6. Syngellakis S, Papulia KD. A transfer matrix apprach t free vibratins f cupled shear walls. Eng Struct 1987;9:pp 265 71. 378