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N hi kwn Awn Xn Zn Bn An Q 3 3 331.77 0.5941 0.975 1.0088 0.5889 330 333.54 60.18 2 4 248.83 0.7218 0.975 1.0093 0.7152 246.68 250.97 111.76 1 5 199.06 1.1608 0.975 1.0141 1.1447 195.63 202.5 144 Awn = Area de las placas Bn = Kwn - 3*Zn ejemplo: B3 = kw3 - 3*Z3 330 An = Kwn + 3*Zn Cn = A2 = kw2 + 3*Z2 ejempl C1 = Armando la ecuacion de Osawa N 6*Kvn an bn dn an = 3 16.134 349.67 330 178.96 dn = 2 16.134 600.65 246.68 621.89 bn = Bn 1 16.134 469.6 195.63 1152.9 a3 - b3 0 * f3 = 178.96 - b3 a2 - b2 f2 621.89 0 - b2 a1 f1 1152.9 349.67 -330 0 f3 = 178.96 -330 600.65 -246.7 f2 621.89 0 -246.7 469.6 f1 1152.9 f3 = 8.768 f2 8.748 f1 7.051 Cortantes y Momentos (por las dos placas) N fn Zn Cn Qwn Qcn 3*kvn 3 8.768 52.5495721551 0.5889 178.96 49.339 10.841 8.067 2 8.748 47.3970938611 0.7152 442.92 102.26 9.5035 8.067 1 7.051 21.1519268006 1.1447 710.02 137.16 6.8392 8.067 S Dc An + An Cn + Cn 3*(fn-1+fn)

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Hoja1NhikwnS DcAwnXnZnBnAnQCn33331.7710.59410.9751.0088102130.5889115637330.0042653089333.537734691160.18178.963295253624248.8280.72180.9751.00929705740.7151511983246.6825464052250.9734535948111.76442.922127553315199.0631.16080.9751.01406049881.1447048784195.6288853647202.4971146353144710.0168094951 Awn = Area de las placas Bn =Kwn - 3*Zn ejemplo: B3 =kw3 - 3*Z3330.0042653089

An =Kwn + 3*Zn Cn =Qn*hn/xn A2 =kw2 + 3*Z2 ejemplo:

C1 =Q1*h1/X1

Armando la ecuacion de Osawa

N6*Kvnanbndnan =An + An+1+6*Kvn316.134349.6717346911330.0042653089178.9632952536dn =Cn + Cn+1216.134600.6451882859246.6825464052621.8854228069bn = Bn116.134469.60456823195.62888536471152.9389370484

a3 - b30*f3 =178.9632952536 - b3a2 - b2f2621.88542280690 - b2a1f11152.9389370484

349.6717346911-330.00426530890f3 =178.9632952536-330.0042653089600.6451882859-246.6825464052f2621.88542280690-246.6825464052469.60456823f11152.9389370484

f3 =8.768f28.748f17.051 Cortantes y Momentos (por las dos placas)Nfn3*(fn-1+fn)ZnCnQwnQcn3*kvnMvn38.76852.54957215510.5889115637178.963295253649.338748181310.84125181878.06770.732545299428.74847.39709386110.7151511983442.9221275533102.25650977129.50349022888.06770.573254225617.05121.15192680061.1447048784710.0168094951137.16081913976.83918086038.06756.8775311669TnTnTn-m Qcn = Corte que toman las columnas Qwn = corte que tomas las placas

Qwn =(Cn-3*(fn-1+fn)*zn)/hn Mvn =3*kvn*fn Qcn =Qn - Qwn Determinacin de la Deformacin por entrepiso

NhiDonQwn*hn/kwnQwn*hn/(G*Awn)derdetdtrdrrD332898.280.44613979080.00016761590.00629621490.0200.10510070520.0330551280.011018376241630.281.64381033920.00046318730.0080761440.01372296710.07204557720.0423997560.010599939151043.383.4451610580.0007766150.00564682310.00564682310.02964582120.02964582120.0059291642

der Desplazamiento relativo en el rango elasticoQcn/(Don*SDcn)det Desplazamientos absolutos en el rango elastico.dtr Desplazamientos absolutos en el rango nolineal-desplazamientos absolutos para el sismo de diseo Desplazamientos absolutos realesdet*3/4*Rdrr Desplazamiento relativo real - rango no lineal para el sismo de diseo - con esto nosotros diseamos la junta de separacion entre los elementos estructurales y no estructurales D Distorsion. Dual debe ser menor al 0.007