calculos muros ultimo(1).xls
TRANSCRIPT
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
1. CALCULO DE LOS ESPESORES DE ACI 9.5.3.2* Sin Vigas de Borde
hf1 =2370
hf2 =3500 hf1 = 71.82 mm
33 33
hf2 = 106.06 mm
POR LO TANTO h = 130 mm Valor Asumido
2. ESPESOR DEL MURO RNE E-070 19
t =2300 t = 115 mm POR LO TANTO t = 130 mm
20
3. RELACION DE E-070 15.3
1 <17.98
< 4 m8.56 1 < 2 < 4 m
*. Norma Peruana E-070 17.f Lado mas largo < 25 m ### < ### m
4. DENSIDAD MINIMA DE LOS MUROS REFORZADOS EN CADA DIRECCION E-070 19.2.b
=∑L*t
≥ZUSN
56
LADO X-X LADO Y-Y
MURO Lxx(M) MURO Lxx(M)
X1 3.14 Y1 1.94X2 3.04 Y2 2.74X3 3.04 Y3 3.58X4 4.08 Y4 4.08X5 2.44 Y5 3.24X6 2.74 Y6 3.58X7 3.44 Y7 3.58X8 3.44 Y8 3.24X9 2.74 Y9 4.08
X10 2.44 Y10 3.58X11 4.08 Y11 2.74X12 3.04 Y12 1.94X13 3.04 Y13 4.08X14 3.14X15 2.54
Amuro
Aplanta Ap
t≥ h20
h f 1=ln 133
h f 2=l233
h≥125mm
1< LadoMasLargoLadoMasCorto
<4
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
46.38 42.40
Z = 0.4 Ancash se encuentra Zona 3 Z = 0.4 ZUSN = 1.92 ZUSN= 0.032
U = 1 Edificaciones Comunes U = 1 60S = 1.2 Roca o Suelos Muy Rigidos S = 1.2 ZUSN = 1.92N = 4 Numero de Pisos N = 4 ZUSN
= 0.03260
LX = 17.98 = 154LX = 17.98 = 154
LY = 8.56 LY = 8.56=
=46.38 0.14
= 0.042 =42.40 0.14
= 0.039153.91 153.91
∑L*t≥
ZUSN0.042 ≥ 0.032
∑L*t≥
ZUSN0.039 ≥ 0.032
56 56Cumple la Condicion Cumple la Condicion
5. METRADO DE CARGAS* PESO DE CONCRETO
= 2.40E-05 N/mm3
* ACABADO
= 1.00E-03 N/mm2
* ALBAÑILERIA SOLIDA 0 0.14 0
= 1.80E-05 N/mm3
= 1.90E-05 N/mm3
= 1.90E-05 N/mm3 * 140 mm = 2.66E-03 N/mm2
* PARAPETROS Y TABIQUERIA
= 1.40E-05 N/mm3
= 1.40E-05 N/mm3 * 140 mm = 1.96E-03 N/mm2
* VENTANA
= 2.00E-04 N/mm2
* S/C
= 2.00E-03 N/mm2
* PARA EFECTOS SISMICOS S/C 25%
Aplanta Aplanta
Amuro Amuro Amuro Amuro
Aplanta Aplanta Aplanta Aplanta
Ap Ap
gc
gac
gal
gal
gal gal
gal
gal gal
gv
gslc
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
= 5.00E-04 N/mm2
* CARGAS PROVENIENTES DE LA LOSA
= 2.40E-05 N/mm3
INCLUYENDO ESPESOR DE LOSA = 2.40E-05 N/mm3 * 130 mm = 3.12E-03 N/mm2
Sin S/C 25% S/C 75%s/c 100%s/cCONCRETO REFORZADO 3.12E-03 3.12E-03 3.12E-03 3.12E-03
ACABADO 1.00E-03 1.00E-03 1.00E-03 1.00E-03S/C(Para Efecto Sismico) 0.00E+00 5.00E-04 1.50E-03 2.00E-03
W = 4.12E-03 4.62E-03 5.62E-03 0.00E+00
CARGA P(N) X-X CON SIN S/C CARGA P(N) Y-Y CON SIN S/C
MURO A(mm2) P(N) MURO A(mm2) P(N)X1 2.10E+06 8.65E+03 Y1 2.25E+06 9.27E+03X2 5.41E+06 2.23E+04 Y2 3.43E+06 1.41E+04X3 7.10E+06 2.93E+04 Y3 7.45E+06 3.07E+04X4 3.61E+05 1.49E+03 Y4 8.17E+06 3.37E+04X5 2.88E+06 1.19E+04 Y5 5.61E+06 2.31E+04X6 6.10E+06 2.51E+04 Y6 4.43E+06 1.83E+04X7 2.98E+06 1.23E+04 Y7 4.43E+06 1.83E+04X8 2.98E+06 1.23E+04 Y8 5.61E+06 2.31E+04X9 6.10E+06 2.51E+04 Y9 8.17E+06 3.37E+04
X10 2.88E+06 1.19E+04 Y10 7.45E+06 3.07E+04X11 3.61E+05 1.49E+03 Y11 3.43E+06 1.41E+04X12 7.10E+06 2.93E+04 Y12 2.25E+06 9.27E+03X13 5.41E+06 2.23E+04 Y13 4.20E+06 1.73E+04X14 2.10E+06 8.65E+03X15 5.21E+06 2.15E+04
5.91E+07 2.43E+05 6.69E+07 2.76E+05
6. CALCULO DE LA CARGA TOTAL DEL PISO
Carga Vertical 25% de Sobre Carga
MURO Lx(mm) Yi(mm) Wx P(N) WiYiX1 3140 0.00E+00 3.80E+04 1.52E+05 3.46E-01 0.00E+00X2 3040 1.34E+03 4.48E+04 1.79E+05 4.21E-01 6.00E+07X3 3040 4.48E+03 5.26E+04 2.10E+05 4.94E-01 2.36E+08X4 4080 8.42E+03 2.90E+04 1.16E+05 2.03E-01 2.44E+08X5 2440 8.42E+03 4.80E-05 1.92E-04 5.62E-10 4.04E-01X6 2740 4.48E+03 4.63E+04 1.85E+05 4.82E-01 2.07E+08X7 3440 0.00E+00 3.07E+04 1.23E+05 2.55E-01 0.00E+00X8 3440 0.00E+00 3.07E+04 1.23E+05 2.55E-01 0.00E+00X9 2740 4.48E+03 4.63E+04 1.85E+05 4.82E-01 2.07E+08
X10 2440 8.42E+03 4.80E-05 1.92E-04 5.62E-10 4.04E-01X11 4080 8.42E+03 2.90E+04 1.16E+05 2.03E-01 2.44E+08
gslc
gc
gc
σ(MPA)
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
X12 3040 4.48E+03 5.26E+04 2.10E+05 4.94E-01 2.36E+08X13 3040 1.34E+03 4.48E+04 1.79E+05 4.21E-01 6.00E+07X14 3140 0.00E+00 3.80E+04 1.52E+05 3.46E-01 0.00E+00X15 2540 4.48E+03 4.80E-05 1.92E-04 5.40E-10 2.15E-01
4.83E+05 1.49E+09
* CARGAS PARA X1 - X14 CON 25 % S/C
PLM = A1*25% S/CPS = L*(t+10+10)*(200+130)* Peso Especifico del Concreto
PEC = (t+10+10)*Espesor de la Losa*h*Peso Especifico del Concreto*2PMP = longitud sin columnas*altura*2.66E-3
PT = mitad de la ventana*alturadel piso a la ventana*1.96E-3
PARA CASO DE 0 % DE SOBRE CARGAPLM = 2.10E+06 * 4.12E-03 = 8.65E+03
PS = 3360 * 160 * 330 * 2.40E-05 = 4.26E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 400 * 900 * 1.96E-03 = 7.06E+02
Wx = 3.69E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 2.10E+06 * 4.62E-03 = 9.70E+03
PS = 3360 * 160 * 330 * 2.40E-05 = 4.26E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 400 * 900 * 1.96E-03 = 7.06E+02
Wx = 3.80E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 2.10E+06 * 5.62E-03 = 1.18E+04
PS = 3360 * 160 * 330 * 2.40E-05 = 4.26E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 400 * 900 * 1.96E-03 = 7.06E+02
Wx = 4.01E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 2.10E+06 * 0.00E+00 = 0.00E+00
PS = 3360 * 160 * 330 * 2.40E-05 = 4.26E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 400 * 900 * 1.96E-03 = 7.06E+02
Wx = 2.83E+04
* CARGAS PARA X2 - X13 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGA
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PLM = 5.41E+06 * 4.12E-03 = 2.23E+04PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wx = 4.21E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 5.41E+06 * 4.62E-03 = 2.50E+04
PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.48E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 5.41E+06 * 0.00562 = 3.04E+04
PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 5.02E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 5.41E+06 * 0.00 = 0.00E+00
PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 1.98E+04CARGAS PARA X3 - X12 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 7.10E+06 * 0.00 = 2.93E+04
PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.91E+04PARA CASO DE 25 % DE SOBRE CARGA
PLM = 7.10E+06 * 0.005 = 3.28E+04PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wx = 5.26E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 7.10E+06 * 0.006 = 3.99E+04
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 5.97E+04PARA CASO DE 100 % DE SOBRE CARGA
PLM = 7.10E+06 * 0.00 = 0.00E+00PS = 3040 * 160 * 330 * 2.40E-05 = 3.85E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2480 * 2100 * 2.66E-03 = 1.39E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wx = 1.98E+04
CARGAS PARA X4 - X11 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 3.61E+05 * 0.00 = 1.49E+03
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 2.88E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 3.61E+05 * 0.00 = 1.67E+03
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 2.90E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 3.61E+05 * 0.01 = 2.03E+03
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.80E-05
PARA CASO DE 100 % DE SOBRE CARGAPLM = 3.61E+05 * 0.000000 = 0.00E+00
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.80E-05
CARGAS PARA X5 - X10 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGA
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PLM = 2.88E+06 * 0.00 = 1.19E+04PS = 4840 * 160 * 330 * 2.40E-05 = 6.13E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04
PT = 600 * 900 * 1.96E-03 = 1.06E+03Wx = 4.80E-05
PARA CASO DE 25 % DE SOBRE CARGAPLM = 2.88E+06 * 0.00 = 1.33E+04
PS = 4840 * 160 * 330 * 2.40E-05 = 6.13E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wx = 4.80E-05
PARA CASO DE 75 % DE SOBRE CARGAPLM = 2.88E+06 * 0.01 = 1.62E+04
PS = 4840 * 160 * 330 * 2.40E-05 = 6.13E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wx = 4.80E-05
PARA CASO DE 100 % DE SOBRE CARGAPLM = 2.88E+06 * 0.00 = 0.00E+00
PS = 4840 * 160 * 330 * 2.40E-05 = 6.13E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3590 * 2100 * 2.66E-03 = 2.01E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wx = 2.93E+04
CARGAS PARA X6 - X9 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 6.10E+06 * 0.00 = 2.51E+04
PS = 2740 * 160 * 330 * 2.40E-05 = 3.47E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2240 * 2100 * 2.66E-03 = 1.25E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.32E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 6.10E+06 * 0.00 = 2.82E+04
PS = 2740 * 160 * 330 * 2.40E-05 = 3.47E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2240 * 2100 * 2.66E-03 = 1.25E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.63E+04
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PARA CASO DE 75 % DE SOBRE CARGAPLM = 6.10E+06 * 0.01 = 3.43E+04
PS = 2740 * 160 * 330 * 2.40E-05 = 3.47E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2240 * 2100 * 2.66E-03 = 1.25E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 5.24E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 6.10E+06 * 0.00 = 0.00E+00
PS = 2740 * 160 * 330 * 2.40E-05 = 3.47E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2240 * 2100 * 2.66E-03 = 1.25E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.80E-05
CARGAS PARA X7 - X8 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 2.98E+06 * 0.00 = 1.23E+04
PS = 3440 * 160 * 330 * 2.40E-05 = 4.36E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 1880 * 2100 * 2.66E-03 = 1.05E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 2.92E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 2.98E+06 * 0.00 = 1.38E+04
PS = 3440 * 160 * 330 * 2.40E-05 = 4.36E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 1880 * 2100 * 2.66E-03 = 1.05E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 3.07E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 2.98E+06 * 0.01 = 1.67E+04
PS = 3440 * 160 * 330 * 2.40E-05 = 4.36E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 1880 * 2100 * 2.66E-03 = 1.05E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 3.37E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 2.98E+06 * 0.00 = 0.00E+00
PS = 3440 * 160 * 330 * 2.40E-05 = 4.36E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 1880 * 2100 * 2.66E-03 = 1.05E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 1.70E+04
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
CARGAS PARA X15 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 5.21E+06 * 0.00 = 2.15E+04
PS = 2540 * 160 * 330 * 2.40E-05 = 3.22E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2390 * 2100 * 2.66E-03 = 1.34E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.01E+04PARA CASO DE 25 % DE SOBRE CARGA
PLM = 5.21E+06 * 0.00 = 2.41E+04PS = 2540 * 160 * 330 * 2.40E-05 = 3.22E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2390 * 2100 * 2.66E-03 = 1.34E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wx = 4.80E-05
PARA CASO DE 75 % DE SOBRE CARGAPLM = 5.21E+06 * 0.01 = 2.93E+04
PS = 2540 * 160 * 330 * 2.40E-05 = 3.22E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2390 * 2100 * 2.66E-03 = 1.34E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 4.79E+04PARA CASO DE 100 % DE SOBRE CARGA
PLM = 5.21E+06 * 0.00 = 0.00E+00PS = 2540 * 160 * 330 * 2.40E-05 = 3.22E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2390 * 2100 * 2.66E-03 = 1.34E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wx = 1.87E+04
Carga Vertical 25% de Sobre Carga ANALIZAMOS EJE Y - Y
MURO Ly(mm) Xi(mm) Wy P(N) WiXi MURO A(mm2)
Y1 1940 0 3.60E+04 1.44E+05 5.30E-01 0.00E+00 Y1 2.25E+06Y2 2740 0 4.69E+04 1.88E+05 4.89E-01 0.00E+00 Y2 3.43E+06Y3 3580 3940 6.03E+04 2.41E+05 4.81E-01 2.37E+08 Y3 7.45E+06Y4 4080 394 6.55E+04 2.62E+05 4.58E-01 2.58E+07 Y4 8.17E+06Y5 3240 7580 4.71E+04 1.88E+05 4.15E-01 3.57E+08 Y5 5.61E+06Y6 3580 7580 4.40E+04 1.76E+05 3.51E-01 3.33E+08 Y6 4.43E+06Y7 3580 10260 4.40E+04 1.76E+05 3.51E-01 4.51E+08 Y7 4.43E+06Y8 3240 10260 4.71E+04 1.88E+05 4.15E-01 4.83E+08 Y8 5.61E+06Y9 4080 13900 6.55E+04 2.62E+05 4.58E-01 9.10E+08 Y9 8.17E+06
Y10 3580 13900 6.03E+04 2.41E+05 4.81E-01 8.38E+08 Y10 7.45E+06Y11 2740 17840 4.69E+04 1.88E+05 4.89E-01 8.37E+08 Y11 3.43E+06Y12 1940 17840 3.60E+04 1.44E+05 5.30E-01 6.42E+08 Y12 2.25E+06Y13 4080 8920 4.63E+04 1.85E+05 3.24E-01 4.13E+08 Y13 4.20E+06
σ(MPA)
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
6.46E+05 5.53E+09 6.69E+07
CARGAS PARA Y1 - Y12 CON 25 % S/C
PLM = A1*25% S/CPS = L*(t+10+10)*(200+130)* Peso Especifico del Concreto
PEC = (t+10+10)*Espesor de la Losa*h*Peso Especifico del Concreto*2PMP = longitud sin columnas*altura*2.66E-3
PT = mitad de la ventana*alturadel piso a la ventana*1.96E-3
PARA CASO DE 0 % DE SOBRE CARGAPLM = 2.25E+06 * 0.00 = 9.27E+03
PS = 4480 * 160 * 330 * 2.40E-05 = 5.68E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3000 * 2100 * 2.66E-03 = 1.68E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03Wy = 3.49E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 2.25E+06 * 0.00 = 1.04E+04
PS = 4480 * 160 * 330 * 2.40E-05 = 5.68E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3000 * 2100 * 2.66E-03 = 1.68E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wy = 3.60E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 2.25E+06 * 0.01 = 1.26E+04
PS = 4480 * 160 * 330 * 2.40E-05 = 5.68E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3000 * 2100 * 2.66E-03 = 1.68E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wy = 3.82E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 2.25E+06 * 0.00 = 0.00E+00
PS = 4480 * 160 * 330 * 2.40E-05 = 5.68E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3000 * 2100 * 2.66E-03 = 1.68E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wy = 2.56E+04
* CARGAS PARA Y2 - Y11 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 3.43E+06 * 0.00 = 1.41E+04
PS = 5280 * 160 * 330 * 2.40E-05 = 6.69E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wy = 4.52E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 3.43E+06 * 0.00 = 1.58E+04
PS = 5280 * 160 * 330 * 2.40E-05 = 6.69E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03Wy = 4.69E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 3.43E+06 * 0.01 = 1.93E+04
PS = 5280 * 160 * 330 * 2.40E-05 = 6.69E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 4.93E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 3.43E+06 * 0.00 = 0.00E+00
PS = 5280 * 160 * 330 * 2.40E-05 = 6.69E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3800 * 2100 * 2.66E-03 = 2.12E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wx = 3.00E+04
* CARGAS PARA Y3 - Y10 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 7.45E+06 * 0.00 = 3.07E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3440 * 2100 * 2.66E-03 = 1.92E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 5.65E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 7.45E+06 * 0.00 = 3.44E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3440 * 2100 * 2.66E-03 = 1.92E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 6.03E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 7.45E+06 * 0.01 = 4.19E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3440 * 2100 * 2.66E-03 = 1.92E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 6.77E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 7.45E+06 * 0.00 = 0.00E+00
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3440 * 2100 * 2.66E-03 = 1.92E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 2.58E+04
CARGAS PARA Y4 - Y9 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 8.17E+06 * 0.00 = 3.37E+04
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3660 * 2100 * 2.66E-03 = 2.04E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 6.14E+04PARA CASO DE 25 % DE SOBRE CARGA
PLM = 8.17E+06 * 0.00 = 3.77E+04PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3660 * 2100 * 2.66E-03 = 2.04E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 6.55E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 8.17E+06 * 0.01 = 4.59E+04
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3660 * 2100 * 2.66E-03 = 2.04E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 7.36E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 8.17E+06 * 0.00 = 0.00E+00
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3660 * 2100 * 2.66E-03 = 2.04E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 2.77E+04
* CARGAS PARAY5 - Y8 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGA
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PLM = 5.61E+06 * 0.00 = 2.31E+04PS = 3240 * 160 * 330 * 2.40E-05 = 4.11E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2680 * 2100 * 2.66E-03 = 1.50E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 4.43E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 5.61E+06 * 0.00 = 2.59E+04
PS = 3240 * 160 * 330 * 2.40E-05 = 4.11E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2680 * 2100 * 2.66E-03 = 1.50E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 4.71E+04PARA CASO DE 75 % DE SOBRE CARGA
PLM = 5.61E+06 * 0.01 = 3.15E+04PS = 3240 * 160 * 330 * 2.40E-05 = 4.11E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 2680 * 2100 * 2.66E-03 = 1.50E+04
PT = 600 * 900 * 1.96E-03 = 1.06E+03Wy = 5.38E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 5.61E+06 * 0.00 = 0.00E+00
PS = 3240 * 160 * 330 * 2.40E-05 = 4.11E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 2680 * 2100 * 2.66E-03 = 1.50E+04PT = 600 * 900 * 1.96E-03 = 1.06E+03
Wy = 2.22E+04
CARGAS PARA Y6 - Y7 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 4.43E+06 * 0.00 = 1.83E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3020 * 2100 * 2.66E-03 = 1.69E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 4.18E+04
PARA CASO DE 25 % DE SOBRE CARGAPLM = 4.43E+06 * 0.00 = 2.05E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3020 * 2100 * 2.66E-03 = 1.69E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 4.40E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 4.43E+06 * 0.01 = 2.49E+04
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3020 * 2100 * 2.66E-03 = 1.69E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 4.84E+04
PARA CASO DE 100 % DE SOBRE CARGAPLM = 4.43E+06 * 0.00 = 0.00E+00
PS = 3580 * 160 * 330 * 2.40E-05 = 4.54E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3020 * 2100 * 2.66E-03 = 1.69E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 2.35E+04
CARGAS PARA Y13 CON 25 % S/C
PARA CASO DE 0 % DE SOBRE CARGAPLM = 4.20E+06 * 0.00 = 1.73E+04
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3520 * 2100 * 2.66E-03 = 1.97E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 4.42E+04PARA CASO DE 25 % DE SOBRE CARGA
PLM = 4.20E+06 * 0.00 = 1.94E+04PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3520 * 2100 * 2.66E-03 = 1.97E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 4.63E+04
PARA CASO DE 75 % DE SOBRE CARGAPLM = 4.20E+06 * 0.01 = 2.36E+04
PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03
PMP = 3520 * 2100 * 2.66E-03 = 1.97E+04PT = 0 * 900 * 1.96E-03 = 0.00E+00
Wy = 5.05E+04PARA CASO DE 100 % DE SOBRE CARGA
PLM = 4.20E+06 * 0.00 = 0.00E+00PS = 4080 * 160 * 330 * 2.40E-05 = 5.17E+03
PEC = 160 * 130 * 2100 * 2.40E-05 * 2 = 2.10E+03PMP = 3520 * 2100 * 2.66E-03 = 1.97E+04
PT = 0 * 900 * 1.96E-03 = 0.00E+00Wy = 2.69E+04
CALCULO DE CENTRO DE GRAVEDAD Y
Ly = ###=
8560- 3095 = 1185 mm
2Y CG=
∑Wi∗Yi
∑WiLy2
−YCG
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
ΣWiYi= 1.49E+09 Σwi= 482732.64 YCG= 3095.03 mm
CALCULO DE CENTRO DE GRAVEDAD X
LX = ###=
17980- 8561 = 429 mm
2
ΣWiXi= 5.53E+09 Σwi= 645713.47 YCG= 8560.54 mm
ESCALERAPeso de la Losa 1200 * 2680 * 4.62E-03 = 1.49E+04
Losa de la Escalera 2650 * 2050 * 5.10E-03 = 2.77E+04
Wescalera = 4.26E+04 N
PARA 4 PISOS We 4.26E+04 * 4 = 1.70E+05 N
7. CALCULO DE LAS CARGAS
NIVEL CM CV TOTAL4 1.16E+06 3.10E+04 1.19E+06
H =ZUSC*P
3 1.16E+06 6.21E+04 1.22E+06 R2 1.16E+06 6.21E+04 1.22E+061 1.16E+06 6.21E+04 1.22E+06 H = 1.95E+06 N
4.87E+06
8. VERFICACION DE LA RESISTENCIA ADMISIBLE DEL LADRILLO
MURO σ(MPA) MURO σ(MPA)X1 0.26 Y1 0.53X2 0.42 Y2 0.49X3 0.49 Y3 0.48X4 0.20 Y4 0.46X5 0.50 Y5 0.42X6 0.48 Y6 0.35X7 0.26 Y7 0.35X8 0.26 Y8 0.42X9 0.48 Y9 0.46
X10 0.50 Y10 0.48X11 0.20 Y11 0.49X12 0.49 Y12 0.53X13 0.42 Y13 0.32X14 0.26X15 0.48
ANALIZAMOS X5-X10 X5-X10 = 0.50
PX5 = Area Tributaria*Sobre Carga 75%*4 + Carga Permanente*4
PX5 = 2.44E+06 * 2.00E-03 * 4 + 2.50E+04 * 4
X CG=∑Wi∗Xi
∑WiLx2
−XCG
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
PX = 1.20E+05 N Pm = PX5
Pm=
1.20E+05= 0.35
RNE 19.1.b t*L 3.42E+05
Pm= 0.35
t*L fm= 3.4 MPA
= 1 0.15*fm = 0.51
0
0.35 £ 0.51 £ 0.51 CUMPLE CON LA CONDICION DEL PROBLEMA
Pm³ 0.05*fm
0 3 Pm= 0.35
0.05*fm = 0.17 Pm³ 0.05*fm
t*L t*L t*L### ###
0.35 ³ 0.17 CUMPLE CON LA CONDICION
9. CALCULO DE RIGIDEZHALLAMOS MURO EQUIVALENTE Datos Iniciales
t = 140 mmEa =500*fm fm = 3 MPA h = 2450 mm Ea = 1700 MPA
fy = 420 MPAGa = 0.4*Ea fc = ### MPA Ga = 680 MPA
n =Ec Ec = 21538.1 MPA n = 12.67Ea
nt = 12.67 * 140 nt = 1773.73 mm nt = 1800 mm
MURO A(mm2) f I(mm4) Ki(N/mm) Yi(mm) Ri(mm) V2i(N) V1i(N) Vt(N) Ki*Yi(N) Ki*Ri2X1 2E+06 4.29 8E+12 1.33E+05 0 4.0E+03 9.8E+04 1.66E+05 3E+05 0E+00 2E+12X2 2E+06 4.29 3E+12 8.82E+04 1270 2.7E+03 4.4E+04 1.10E+05 2E+05 1E+08 6E+11X3 2E+06 5.50 3E+12 8.83E+04 4480 -5.1E+02 -8.4E+03 1.10E+05 1E+05 4E+08 2E+10X4 2E+06 4.16 7E+12 1.32E+05 8420 -4.5E+03 -1.1E+05 1.64E+05 6E+04 1E+09 3E+12X5 2E+06 3.24 2E+12 1.12E+05 8420 -4.5E+03 -9.3E+04 1.40E+05 5E+04 9E+08 2E+12X6 2E+06 3.34 2E+12 1.18E+05 4480 -5.1E+02 -1.1E+04 1.47E+05 1E+05 5E+08 3E+10X7 1E+06 2.53 1E+12 1.08E+05 0 4.0E+03 7.9E+04 1.35E+05 2E+05 0E+00 2E+12X8 1E+06 2.53 1E+12 1.08E+05 0 4.0E+03 7.9E+04 1.35E+05 2E+05 0E+00 2E+12X9 2E+06 3.34 2E+12 1.18E+05 4480 -5.1E+02 -1.1E+04 1.47E+05 1E+05 5E+08 3E+10
X10 2E+06 3.24 2E+12 1.12E+05 8420 -4.5E+03 -9.3E+04 1.40E+05 5E+04 9E+08 2E+12X11 2E+06 4.16 7E+12 1.32E+05 8420 -4.5E+03 -1.1E+05 1.64E+05 6E+04 1E+09 3E+12X12 2E+06 5.50 3E+12 8.83E+04 4480 -5.1E+02 -8.4E+03 1.10E+05 1E+05 4E+08 2E+10X13 2E+06 4.29 3E+12 8.82E+04 1270 2.7E+03 4.4E+04 1.10E+05 2E+05 1E+08 6E+11
σm=Pm
t∗L≤0 .2∗f m
, ∗[1−( h35∗t )
2]≤0 .15∗f m,
0 .2∗f m, ∗[1−( h
35∗t )2]
σm=Pm
t∗L≤0 .2∗f m
, ∗[1−( h35∗t )
2]≤0 .15∗f m,
Ec=4700√ f c,
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
X14 2E+06 4.29 8E+12 1.33E+05 0 4.0E+03 9.8E+04 1.66E+05 3E+05 0E+00 2E+124.0E+03 0.0E+00 0.00E+00 0E+00 0E+00 0E+00
1.56E+06 6E+09 2E+13
XCR = Σ(KixXi)/Σki = 3.97E+03
CENTRO DE GRAVEDA MURO X1 -X14
Y =ΣYA
Y =4.36 X Y(m) A(m2) AY
ΣA 2.16 Y = 2.02 1 4.01 0.504 2.0212 4.08 0.252 1.0283 4.08 0.035 0.143
AREA = 2.16E+06 4 0.14 0.504 0.0715 0.14 0.252 0.035
FACTOR DE FORMA = 2.16E+06 6 0.14 0.105 0.015140 * 3590 f = 4.29 7 2.08 0.503 1.046
2.155 4.359
MOMENTO DE INERCIA
Ixx = 3.29E+09 + 1.78E+12 + 4.12E+08 + 8.91E+11 + 1.72E+08 + 3.71E+11
3.59
1.80 1.800.25
0.14
0.28
0.28
1.80 1.80 0.75
1 2 3
4 5 6
Para muro X1 - X14
7
2.021.
74
1.81
1.85
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
8.2E+08 + 3.3E+09 + 2.00E+12 + 4.12E+08 + 1.1E+12 + 5.72E+07 + 2.14E+12
Ixx = 8.26E+12 mm4
RIGIDEZ LATERAL
Kxx = 1.33E+05 N/mm
CENTRO DE GRAVEDA MURO X2 -X13
Y = ΣYA Y = 2.17 X Y(m) A(m2) AYΣA 1.86 Y = 1.16 1 0.07 0.252 0.018
2 0.14 0.504 0.071AR = 1.86E+06 3 0.07 0.252 0.018
4 3.04 0.504 1.532FACTOR DE FORMA = 1.86E+06 5 1.52 0.347 0.527
140 * 2480 6f = 5.35 7
1.859 2.165
MOMENTO DE INERCIA
Ixx = 4.12E+08 + 2.99E+11 + 3.29E+09 + 8.5176E+11 + 4.12E+08 + 2.99E+11 +
123
4
5
1.80 1.80 1.80
0.28
Para muro X2 - X13
2.48
1.16 1.02
1.60
1.80
0.14
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
5.67E+08 + 3.29E+09 + 1.53E+12
Ixx = 2.98E+12 mm4
RIGIDEZ LATERAL
Kxx = 8.82E+04 N/mm
CENTRO DE GRAVEDA MURO X3 -X12
Y = ΣYA Y = 2.17 X Y(m) A(m2) AYΣA 1.91 Y = 1.14 1 0.07 0.252 0.018
2 0.14 0.504 0.071ARE= 1.91E+06 3 0.07 0.252 0.018
4 3.04 0.504 1.532FACTOR DE FORMA = 1.91E+06 5 1.52 0.347 0.527
140 * 2480 f = 5.50 6 0.07 0.051 0.0047
1.91 2.17
MOMENTO DE INERCIAIxx = 4.1E+08 + 3.0E+11 + 3.3E+09 + 8.5E+11 + 4.1E+08 + 3.0E+11 + 5.7E+08 +
3.3E+09 + 1.5E+12 + 2.5E+08 + 6.0E+10Ixx = 3.05E+12 mm4
RIGIDEZ LATERAL
123
4
5
1.80 1.80 1.80
0.28
Para muro X3 - X12
2.48
1.16 1.02
1.60
1.80
6
0.36
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
Kxx = 8.83E+04 N/mm
CENTRO DE GRAVEDA MURO X4 -X11X Y(m) A(m2) AY
Y =ΣYA
Y =4.55 1 0.14 0.504 0.071
ΣA 2.09 Y = 2.18 2 0.07 0.126 0.0093 0.07 0.077 0.005
AREA = 2.09E+06 4 2.08 0.503 1.0465 4.01 0.504 2.021
FACTOR DE FORMA = 2.09E+06 6 3.73 0.252 0.94140 * 3590 7 3.73 0.123 0.459
f = 4.16 2.089 4.551
MOMENTO DE INERCIA
Ixx = 3.3E+09 + 2.2E+12 + 4.1E+08 + 1.1E+12 + 1.7E+08 + 3.7E+11 + 5.1E+10 +3.3E+09 + 1.7E+12 + 4.1E+08 + 8.4E+11 + 2.0E+08 + 4.1E+11
Ixx = 6.74E+12 mm4
1 2 3
4
5 6 7
1.80 1.80 0.55
3.59
1.80 1.80 0.88
Para muro X4 - X11
1.90
2.04
1.69 1.76
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
RIGIDEZ LATERAL
Kxx 1.32E+05 N/mm
CENTRO DE GRAVEDA MURO X5 -X10
Y =ΣYA
Y =2.43 X Y(m) A(m2) AY
ΣA 1.63 Y = 1.49 1 0.14 0.504 0.0712 2.37 0.504 1.194
AREA = 1.63E+06 3 2.37 0.251 0.5954 1.26 0.273 0.344
FACTOR DE FORMA = 1.63E+06 f = 3.24 5 2.37 0.094 0.223140 * 3590 6
71.626 2.427
MOMENTO DE INERCIAIxx = 3.3E+09 + 9.2E+11 + 3.3E+09 + 3.9E+11 + 4.1E+08 + 1.9E+11 + 8.7E+10 +
1.5E+08 + 7.3E+10Ixx = 1.67E+12 mm4
1.95
1
4
2 3 5
Para muro X5 - X10
1.80
1.80 1.79 0.67
0.28
1.21
0.74 0.81
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
RIGIDEZ LATERAL
Kxx = 1.12E+05 N/mm
CENTRO DE GRAVEDA MURO X6 -X9
Y =ΣYA
Y =2.77 X Y(m) A(m2) AY
ΣA 1.68 Y = 1.65 1 0.14 0.504 0.0712 2.62 0.504 1.32
AREA = 1.68E+06 3 2.62 0.252 0.664 1.4 0.314 0.44
FACTOR DE FORMA = 1.68E+06 f = 3.34 5 2.62 0.106 0.278140 * 3590 6
71.68 2.769
MOMENTO DE INERCIAIxx = 3.29E+09 + 1.1E+12 + 3.3E+09 + 5.1E+11 + + 2.6E+11 + 1.3E+11 + 1.7E+08 +
1.1E+11 + 4.1E+08
Ixx 2.17E+12 mm4
1
4
2 3 5
Para muro X6 - X9
1.80
1.80 1.80 0.76
2.24
0.28
1.37
0.87 0.94
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
RIGIDEZ LATERAL
Kxx 1.18E+05 N/mm
CENTRO DE GRAVEDA MURO X7 -X8
Y =ΣYA
Y =ΣYA
Y =1.55 X Y(m) A(m2) AY
ΣA ΣA 1.27 Y = 1.22 1 0.14 0.504 0.0712 2.3 0.504 1.159
ARE= 1.27E+06 3 1.22 0.263 0.3214
FACTOR DE FORMA = 1.27E+06 5140 * 3590 f = 2.53 6
71.271 1.551
MOMENTO DE INERCIAIxx 3.3E+09 + 5.9E+11 + 3.3E+09 + 5.9E+11 + 7.8E+10 + 1.7E+08 + 1.1E+11
Ixx = 1.37E+12 mm4
RIGIDEZ LATERAL
1
3
2
Para muro X7 - X8
1.80
1.88
1.80
0.94
0.94
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
AXcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
Kxx 1.08E+05 N/mm
*. HALLAMOS MURO EQUIVALENTE Datos Inicialest = 140 mm
Ea = 500*fm fm = 3.4 MPA Ea = 1700 MPA h = 2450 mmfy = 420 MPA
Ga = 0.4*Ea Ga = 680 MPAn =
Ec n = 12.67 fc = 21 MPAEa
Ec = 21538.11 MPA
nt = 12.67 * 140 nt = 1773.73 mm nt = 1800 mm
MUROA(mm2) f I(mm4) Ki(N/mm) Xi(mm Ri(mm) V2i(N) V1i(N) Vt(N) Ki*Yi(N) Ki*Ri2Y1 2.2E+06 4.3 8.3E+12 1.3E+05 0 4.0E+03 9.8E+04 1.7E+05 2.6E+05 0.0E+00 2.1E+12Y2 1.9E+06 4.3 3.0E+12 8.8E+04 1270 2.7E+03 4.4E+04 1.1E+05 1.5E+05 1.1E+08 6.4E+11Y3 2.2E+06 5.5 3.0E+12 8.8E+04 4480 -5.1E+02 -8.4E+03 1.1E+05 1.0E+05 4.0E+08 2.3E+10Y4 2.1E+06 4.2 6.7E+12 1.3E+05 8420 -4.5E+03 -1.1E+05 1.6E+05 5.6E+04 1.1E+09 2.6E+12Y5 1.6E+06 3.2 1.7E+12 1.1E+05 8420 -4.5E+03 -9.3E+04 1.4E+05 4.7E+04 9.5E+08 2.2E+12Y6 1.7E+06 3.3 2.2E+12 1.2E+05 4480 -5.1E+02 -1.1E+04 1.5E+05 1.4E+05 5.3E+08 3.1E+10Y7 1.7E+06 3.2 2.2E+12 1.2E+05 0 4.0E+03 8.7E+04 1.5E+05 2.3E+05 0.0E+00 1.9E+12Y8 1.7E+06 3.2 2.2E+12 1.2E+05 0 4.0E+03 8.7E+04 1.5E+05 2.3E+05 0.0E+00 1.9E+12Y9 1.7E+06 3.3 2.2E+12 1.2E+05 4480 -5.1E+02 -1.1E+04 1.5E+05 1.4E+05 5.3E+08 3.1E+10
Y10 1.6E+06 3.2 1.7E+12 1.1E+05 8420 -4.5E+03 -9.3E+04 1.4E+05 4.7E+04 9.5E+08 2.2E+12Y11 2.1E+06 4.2 6.7E+12 1.3E+05 8420 -4.5E+03 -1.1E+05 1.6E+05 5.6E+04 1.1E+09 2.6E+12Y12 2.2E+06 5.5 3.0E+12 8.8E+04 4480 -5.1E+02 -8.4E+03 1.1E+05 1.0E+05 4.0E+08 2.3E+10
1.4E+06 6.1E+09 0.0E+00XCR = Σ(KixXi)/Σki = 4.47E+03
CENTRO DE GRAVEDA MURO Y1 -Y12
Y = ΣYA Y = 4.36 X Y(m) A(m2) AYΣA 2.16 Y = 2.02 1 4.01 0.504 2.021
2 4.08 0.252 1.028AREA = 2.16E+06 3 4.08 0.035 0.143
4 0.14 0.504 0.071FACTOR DE FORMA = 2.16E+06 5 0.14 0.252 0.035
140 * 3590 f = 4.29 6 0.14 0.105 0.0157 2.08 0.503 1.046
2.155 4.359
3.59
1.80 1.800.25
0.14
0.28
0.28
1.80 1.80 0.75
1 2 3
4 5 6
Para muro Y1-Y12
7
2.021.
74
1.81
1.85
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
Ec=4700√ f c,
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 3.29E+09 + 1.8E+12 + 4.1E+08 + 8.9E+11 + 1.7E+08 + 3.7E+11 + 8.2E+08 +
3.29E+09 + 2.0E+12 + 4.1E+08 + 1.1E+12 + 5.7E+07 + 2.1E+12
Ixx = 8.26E+12 mm4
RIGIDEZ LATERAL
Kxx = 1.33E+05 N/mm
CENTRO DE GRAVEDA MURO Y2-Y11 X Y(m) A(m2) AY
Y =ΣYA
Y =2.17 1 0.07 0.252 0.018
ΣA 1.86 Y = 1.16 2 0.14 0.504 0.0713 0.07 0.252 0.018
AREA = 1.86E+06 4 3.04 0.504 1.5325 1.52 0.347 0.527
FACTOR DE FORMA = 1.86E+06 6140 * 2480 f = 5.35 7
1.859 2.165
3.59
1.80 1.800.25
0.14
0.28
0.28
1.80 1.80 0.75
1 2 3
4 5 6
Para muro Y1-Y12
7
2.021.
74
1.81
1.85
123
4
5
1.80 1.80 1.80
0.28
Para muro Y2-Y11
2.48
1.16 1.02
1.60
1.80
0.14
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 4.12E+08 + 3.0E+11 + 3.3E+09 + 8.5E+11 + 4.1E+08 + 3.0E+11 + 5.7E+08 +
3.29E+09 + 1.5E+12
Ixx = 2.98E+12 mm4
RIGIDEZ LATERAL
Kxx = 8.82E+04 N/mm
CENTRO DE GRAVEDA MURO Y3-Y10
Y = ΣYA Y = 2.17 X Y(m) A(m2) AYΣA 1.91 Y = 1.14 1 0.07 0.252 0.018
2 0.14 0.504 0.071AREA = 1.91E+06 3 0.07 0.252 0.018
4 3.04 0.504 1.532FACTOR DE FORMA = 1.91E+06 5 1.52 0.347 0.527
140 * 2480 f = 5.50 6 0.07 0.051 0.0047
1.91 2.169
123
4
5
1.80 1.80 1.80
0.28
Para muro Y2-Y11
2.48
1.16 1.02
1.60
1.80
0.14
123
4
5
1.80 1.80 1.80
0.28
Para muro Y3-Y10
2.48
1.16 1.02
1.60
1.80
6
0.36
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 4.12E+08 + 3.0E+11 + 3.3E+09 + 8.5E+11 + 4.1E+08 + 3.0E+11 + 5.7E+08 +
3.29E+09 + 1.5E+12 + 2.5E+08 + 6.0E+10
Ixx = 3.05E+12 mm4
RIGIDEZ LATERAL
Kxx = 8.83E+04 N/mm
CENTRO DE GRAVEDA MURO Y4-Y9
Y = ΣYA Y = 4.55 X Y(m) A(m2) AYΣA 2.09 Y = 2.18 1 0.14 0.504 0.071
2 0.07 0.126 0.009AREA = 2.09E+06 3 0.07 0.077 0.005
4 2.08 0.503 1.046FACTOR DE FORMA = 2.09E+06 5 4.01 0.504 2.021
140 * 3590 f = 4.16 6 3.73 0.252 0.947 3.73 0.123 0.459
2.089 4.551
KiVKiV
RiKiRt
eVMt
*1
*
*2
123
4
5
1.80 1.80 1.80
0.28
Para muro Y3-Y10
2.48
1.16 1.02
1.60
1.80
6
0.36
1 2 3
4
5 6 7
1.80 1.80 0.55
3.59
1.80 1.80 0.88
Para muro Y4-Y9
1.90
2.04
1.69 1.76
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 3.29E+09 + 2.2E+12 + 4.1E+08 + 1.1E+12 + 1.7E+08 + 3.7E+11 + 5.1E+10 +
3.29E+09 + 1.7E+12 + 4.1E+08 + 8.4E+11 + 2.0E+08 + 4.1E+11
Ixx = 6.74E+12 mm4
RIGIDEZ LATERAL
Kxx = 1.32E+05 N/mm
CENTRO DE GRAVEDA MURO Y5-Y8
Y = ΣYA Y = 2.43 X Y(m) A(m2) AYΣA 1.63 Y = 1.49 1 0.14 0.504 0.071
2 2.37 0.504 1.194AREA = 1.63E+06 3 2.37 0.251 0.595
4 1.26 0.273 0.344FACTOR DE FORMA = 1.63E+06 5 2.37 0.094 0.223
140 * 3590 f = 3.24 67
1.626 2.427
1 2 3
4
5 6 7
1.80 1.80 0.55
3.59
1.80 1.80 0.88
Para muro Y4-Y9
1.90
2.04
1.69 1.76
1.95
1
4
2 3 5
Para muro Y5-Y8
1.80
1.80 1.79 0.67
0.28
1.21
0.74 0.81
Kxx= Eah3
3∗I+ f∗h∗Ea /Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 3.29E+09 + 9.2E+11 + 3.3E+09 + 3.9E+11 + 4.1E+08 + 1.9E+11 + 8.7E+10 +
1.53E+08 + 7.3E+10
Ixx = 1.67E+12 mm4
RIGIDEZ LATERAL
Kxx = 1.12E+05 N/mm
CENTRO DE GRAVEDA MURO Y6-Y7
Y = ΣYA Y = 2.77 X Y(m) A(m2) AYΣA 1.68 Y = 1.65 1 0.14 0.504 0.071
2 2.62 0.504 1.32AREA = 1.68E+06 3 2.62 0.252 0.66
4 1.4 0.314 0.44FACTOR DE FORMA = 1.68E+06 5 2.62 0.106 0.278
140 * 3590 f = 3.34 67
1.68 2.769
1.95
1
4
2 3 5
Para muro Y5-Y8
1.80
1.80 1.79 0.67
0.28
1.21
0.74 0.81
1
4
2 3 5
Para muro Y6-Y7
1.80
1.80 1.80 0.76
2.24
0.28
1.37
0.87 0.94
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
ALBAÑILERIA ESTRUCTURAL
TRABAJO GRUPAL
MOMENTO DE INERCIAIxx = 3.29E+09 + 1.1E+12 + 3.3E+09 + 5.14E+11 + 4.1E+08 + 2.6E+11 + 1.3E+11 +
1.74E+08 + 1.1E+11
Ixx = 2.17E+12 mm4
RIGIDEZ LATERAL
Kxx = 1.18E+05 N/mm
1
4
2 3 5
Para muro Y6-Y7
1.80
1.80 1.80 0.76
2.24
0.28
1.37
0.87 0.94
Kxx= Eah3
3∗I+ f∗h∗Ea/Ga
A
Xcr=∑ (Ki∗Xi )
∑ (Ki )Ri=Xcr−Xi
V 2 i=Ki∗Ri∗MtRt
Mt=V∗eRt=∑ (Ki∗Ri2 )
V 1i=K∗V∑ (Ki )
* ANALISAMOS LA CORTANTE MAXIMA (Que se encuentra X1 - x14)
X1 = 1.66E+05 N
H = 1.66E+05 N
PISO Pi(N) hi(mm) Pi*hi Fi(N) Ve4 4.15E+04 9800 406700000 6.64E+04 6.64E+043 4.15E+04 7350 305025000 4.98E+04 1.16E+052 4.15E+04 4900 203350000 3.32E+04 1.49E+051 4.15E+04 2450 101675000 1.66E+04 1.66E+05
1.017E+09
0.13
0.20
2.10
140 3800
6.64E+04 6.64E+042450
4.98E+04 1.16E+052450
3.32E+04 1.49E+052450
1.66E+04 1.66E+052450
FUERZA CORTANTE
*1 ANALISIS MURO X1
H = 2100 + 200 + 130
Fi= Pi∗hi∗H∑ Pi∗hi
H = 2450 mm h = 2100
L = 3800 + 140 + 140
L = 4080 mm
t = 140 mm Espesor del Muro
A = t*L
A = 140 * 4080
A = 5.71E+05 mm2
I =3
I = 140 408012
I = 7.92E+11 mm4
fm = 6.4 MPA fc
PARA CASO DE 0 % DE SOBRE CARGAPLM = 2.10E+06 * 0.00412PS = 3360 * 160 * 330 * 0.000024
PEC = 160 * 130 * 2100 * 0.000024PMP = 3800 * 2100 * 0.00266PT = 400 * 900 * 0.00196
Wx
PARA CASO DE 25 % DE SOBRE CARGAPLM = 2.10E+06 * 0.00462PS = 3360 * 160 * 330 * 0.000024
PEC = 160 * 130 * 2100 * 0.000024PMP = 3800 * 2100 * 0.00266PT = 400 * 900 * 0.00196
Wx
PARA CASO DE 100 % DE SOBRE CARGA
(t*L3)/12
PLM = 2.10E+06 * 0.00612PS = 3360 * 160 * 330 * 0.000024PEC = 160 * 130 * 2100 * 0.000024PMP = 3800 * 2100 * 0.00266PT = 400 * 900 * 0.00196
Wx
CARGAS AXIALES DE SISMO
Pd = 1.48E+05 N Carga Axial con 0% de Sobre Carga
Pg = Px = 1.52E+05 N Carga Axial con 25% de Sobre Carga
Pm = 1.65E+05 N Carga Axial con 100% de Sobre Carga
Vx1 = 1.66E+05 N Cortante Basal
Mx1 = 4.07E+08 N-mm
VERIFICAMOS POR COMPRESION EL ESFUERZO ADMISIBLE RNE 19.1.61 - 30.7
Fa = 0.2 * 3.4 * 1 -
1 -Fa = 0.68 *
1 -Fa = 0.68 *
Fa = 0.53 < 0.51
fa+
fm<
1.33Fa Fm
Fa=0.20∗f m, ∗[1−( h
35∗t )2]≤0 .15∗f m
,
fa = PmA
fa = 1.65E+055.71E+05
fa = 0.29
fm = m*yI
fm = 4.07E+08 * 21107.92E+11
fm = 1.08 MPA
Fm = 0.4*fm
Fm = 0.4332009 MPA
0.29+
1.08<
1.330.53 0.4332009
0.543376876 + 2.5<
1.33
3.043377 < 1.33 NO CUMPLE LA CONDICION
VERIFICAMOS ESFUERZOS MAXIMOS Y MINIMOS PROVENIENTES DE LA CARGA AXIAL CON 100% DE SOBRECARGA
sh = Pmt*l
sh = 1.65E+05160 * 4080
sh = 0.25 MPA
0.05fm < sh < 0.15fm
0.05 3.40 < sh < 0.15 3.40
0.17 < 0.25 < 0.51 SI CUMPLE CON LA CONDICION
RESISTENCIA AL CORTE ANTE UN SISMO MODERADO Y SEVERO 26.3 RNE
Vm = Vr
Vm : Resistencia al agrietamiento Diagonal
Vm = + 0.23Pg
vm = 0.8 MPA 13.9 RNE
a = Ve L 26.3.a RNEMe
a = 1.66E+05 40804.07E+08
a = 1.67
0.33 < a < 1
POR LO TANTO a = 1
Pg = 1.52E+05 N
VM = 0.5 0.8 1 140 4080 +
VM = 2.63E+05 N
bw
f = 0.75280
Nu. = 2.72E+05 CARAGA AXIAL
Vm = 0.17 0.75 1 + 2.72E+0514 140
Vm = 0.1275 1 + 0.494716
0.5*vm*a*t*L
Vmc=Φ0 .17 (1+ Nu14 Ag )√ fc bwd
Vm = 3.18E+04 N
Vmc = 2 * 3.18E+04 2 numero de columnas
Vmc = 6.35E+04 N
Vmt = Vm + Vmc
Vmt = 2.63E+05 + 6.35E+04
Vmt = 3.27E+05 N Resistencia a la compresion del Muro
EXAMINAMOS EL ART 27.C RNE CORTANTE DE DISEÑO
Vut = Vet * VmtVet
2 £ Vmt £ 3Vet
2 £ 3.27E+05 £ 31.66E+05
2 £ 1.97 £ 3
POR LO TANTO ASUMIMOS 2
Vut = 2 Vet
Vut = 3.32E+05 N
CONTROL DE FISURACION ANTE LOS SISMOS MODERADOS
Vr £ 0.55*Vm Vm = 1.80E+05
PARA EL PRIMER PISO
Vu1 = 1.66E+05 £ 1.80E+05 N CUMPLE
PARA EL SEGUNDO PISO
Vu2 = 1.49E+05 £ 1.80E+05 N CUMPLE
PARA EL PRIMER PISO
Vu1 = 1.16E+05 £ 1.80E+05 N CUMPLE
PARA EL SEGUNDO PISO
Vu2 = 6.64E+04 £ 1.80E+05 N CUMPLE
MOMENTO FLECTOR ANTE SISMOS SEVEROS
Mut1 = Met * VmtVet
Vmt= 2
Vet
PARA EL PRIMER PISO
Mut1 = 8.13E+08 N-mm
PARA EL SEGUNDO PISO
Mut2 = 7.32E+08 N-mm
PARA EL TERCER PISO
Mut3 = 5.69E+08 N-mm
PARA EL CUARTO PISO
Mtu4 = 3.25E+08 N-mm
DISEÑO DE LAS COLUMNAS DE CONFINAMIENTO 27.3.a RNE
M = Mu - Vm*h2
Mu = 8.13E+08 N-mm
Vm = 1.66E+05 N
h = 2300 mm
M = 8.13E+08 - 1.66E+05 * 23002
M = 6.23E+08 N-mm
F = M 27.3 RNEL
F = 6.23E+084080
F = 1.53E+05
Pc = PgNc
Pc = 1.52E+052
Pc = 7.60E+04
MURO TRANSVERSAL O PERRPENDICULAR APORTA AL MURO X1 PY3
Pt = 25% PY3
PY3 = 2.41E+05
Pt = 6.03E+04 N
Pte = 0 Lado Izquierdo No existe Muro Portante
Pte = 6.03E+04 N Lado Derecho existe Muro Portante
DISEÑO POR TRACCION
T = F - Pc - Pet
PRIMER PISO
1. EXTERIOR
T = 1.53E+05 - 7.60E+04 - 0
T = 7.66E+04 N
2. INTERIOR
T = 0 NO EXISTE
COMPRESION DE ELEMENTOS CONFINATES
1. EXTERIORCe = Pc + F
Ce = 7.60E+04 + 1.53E+05
Ce = 2.29E+05 N
2. INTERIOR
NO EXISTE
MURO X1 MURO Q SOPORTA CARGA CORTANTE
140 3000
27.3.a EXTERIOR
Vce = 1.5*Vm*LmL*(Nc+1)
Vce = 1.5 3.32E+05 30004080 3
Vce = 1.49E+0912240
Vce = 1.22E+05 N
27.3.a INTERIOR
Vci = 0 NO EXISTE COLUMNAS INTERIORES
DETERMINACION REFUERZOS
REFUERZO VERTICAL PARA COLUMNAS EXTERIORES
POR FRICION
Asf= Vc
f u fy
f = 0.85
u = 1
fy = 420
Asf= 1.66E+05
0.85 1 420
Asf = 465 mm2
POR TENSION
Ast= T
f * fy
f = 0.85
fy = 420
Ast= 7.66E+04
0.85 1 420
Ast = 215 mm2
POR LO TANTO
AS = Asf + Ast
AS = 465 + 215
AS = 680 mm
AREA DEL NUCLEO norma establece 2 casos
DISEÑO POR COMPRESION
An = 680 + 3.27E+05 - 2.85E+0514.28
An = 3557 mm2
20
100
20d
20 240 20
An = 3557 > 100 * 240
An = 3557 > 24000 NO CUMPLE LA CONDICION
DISEÑO POR CORTE Y FRICCION
Acf = 1.66E+050.2 0.85 21
Acf = 46499 mm2
POR LO TANTO USAREMOS
140 * 332 mm2
140 * 400 mm2
d = 400 - 20 + 13 /
d = 373.5 mm
An=As+
CΦ−As∗fy0 .85∗δ∗fc
Acf= Vc0 .2 fc φ
VERIFICAMOS LA CUANTIA
CUANTIA = Ant*d
CUANTIA = 3557140 373.5
CUANTIA = 0.07
N13 : nv = AsArea de Acero
nv = 680133
nv = 5
N16 : nv = AsArea de Acero
nv = 680201
nv = 3
POR LO TANTO USAREMOS N13
170 17030 340 30
3800 140
1.63E+08
2.85E+08
3.66E+08
4.07E+08
MOMENTO FLECTOR
130 + 20
Fi= Pi∗hi∗H∑ Pi∗hi
+ 200 = 2300
t = 140 + 10 + 10 = 160
= 21.00 MPA
= 8.65E+03= 4.26E+03
* 2.00 = 2.10E+03= 2.12E+04= 7.06E+02
Wx = 3.69E+04
= 9.70E+03= 4.26E+03
* 2 = 2.10E+03= 2.12E+04= 7.06E+02
Wx = 3.80E+04
= 1.29E+04= 4.26E+03
* 2 = 2.10E+03= 2.12E+04= 7.06E+02
Wx = 4.11E+04
Carga Axial con 0% de Sobre Carga
Carga Axial con 25% de Sobre Carga
Carga Axial con 100% de Sobre Carga
VERIFICAMOS POR COMPRESION EL ESFUERZO ADMISIBLE RNE 19.1.61 - 30.7
22300
<0.15 * fm
35 * 140
20.469387755102041 < 0.15 * 3.4
0.220324864639733 < 0.51
NO CUMPLE CON LA CONDICION
NO CUMPLE LA CONDICION
VERIFICAMOS ESFUERZOS MAXIMOS Y MINIMOS PROVENIENTES DE LA CARGA AXIAL CON 100% DE SOBRECARGA
SI CUMPLE CON LA CONDICION
0.23 1.52E+05
d280
2.72E+05 4.58 140 260280
166712
2 numero de columnas
Resistencia a la compresion del Muro
N
MURO X1 MURO Q SOPORTA CARGA CORTANTE
3000 140
DETERMINACION REFUERZOS
2
MURO X1 MURO Q SOPORTA CARGA CORTANTE
4003410
PZ = 7.29E+04 NPG = 1.52E+05 N CON 25% DE SOBRECARGAPC = 7.60E+04 N
P = PZ + PG PC
P = 3.01E+05 N
M = 4.07E+08 N-mm DATOS GRAFICO
e = MP
e = 4.07E+083.01E+05
e = 1352 mm < L6
< 40806
< 680
st = 0.28 MPA
sa = 1.33 0.28
sa = 0.3724 MPA
VERIFICANDO DATOS
s = 6.02E+051.86E+06
s = 0.32 MPA
0.32 < 0.3724
CUMPLE LA CONDICION
σm=2 P
3B (L2−e)
MURO X1 MURO Q SOPORTA CARGA CORTANTE
4003410
mm no cumple