10
EJERCICIO DE ANALI Alumno: HERNANDEZ JANAMPA DANILO Curso : INGENIERIA SISMICA I.- HALLAR LOS DEZPLAZAMIENTOS DE CADA NIVEL ANLIZAR LOS EJES "X". 5.80 m 5.80 m 0.4 0.4 0.4 0.4 4.0 m 0.4 0.5 0.4 0.4 4.0 m 0.4 0.4 0.4 0.4 DATOS VP: 0.4 0.6 VS: 0.4 0.4 C: 0.4 0.6 e losa: ! # N$ %&sos: ' ()* Al+(,a: '. # (so: NIVERSIDAD / : 10 23 #1 /5: 4100 23 #1 Pa *os: 00 23 #1 P.losa 170 23 #1 P.+a &8. 40 23 #1 %. o) ,+ 1400 23 #' %. S C 400 23 #1 N$e9es ' ()* N$ e9es 5 ' ()* A ;

ANALISIS ESTATICO

Embed Size (px)

DESCRIPTION

sismica

Citation preview

M. DE RIGIDEZ LATERAL EJE "1"EJERCICIO DE ANALISIS ESTATICOAlumno:HERNANDEZ JANAMPA DANILOCurso :INGENIERIA SISMICA

I.- HALLAR LOS DEZPLAZAMIENTOS DE CADA NIVEL ANLIZAR LOS EJES "X".5.80 m5.80 m0.40.40.40.40.40.4

4.60 m

0.40.50.40.40.40.4

4.60 m

0.40.40.40.40.40.4

DATOSVP:0.40.6VS:0.40.4C:0.40.6e losa:17cmN pisos:3undAltura:3.5muso:UNIVERSIDADfc:210kg/cm2fy:4200kg/cm2Pacbdos:100kg/m2P.losa280kg/m2P.tabiq.140kg/m2p. concrt2400kg/m3p. S/C400kg/m2Nejes x3undN ejes y3und

3.50 m

3.50 mCUADRO: MODULO DE ELASTICIDAD E INERCIAE =15000(fc)^1/2 =2173706.51192842ton/m2Ivp=bxh3/12 =0.0072m43.50 mIvs=bxh3/12 =0.0021333333m4

5.80 m5.80 mII .-CALCULO DEL PESO DEL EDIFICIO.

DESCRIPCION CALCULOSNIVEL 1NIVEL 2NIVEL 3CARGA NUERTA:
daymer: daymer:Esta descripcion es solo referencial, en realidad las formulas estan de acuerdo a la forma de columnas y vigas LOSA[(4.4+4.4)x(6+6.4)]x28025401.625401.625401.6P.ACABADOS[(4.4+4.4)x(6+6.4)]x100907290729072P.VIGAS PRINCIPALES[(6+6.4)x0.4x0.6]x3x240018604.818604.818604.8P. VIGAS SECUNDA.[(4.4x0.4x0.4)]x6x24009676.89676.89676.8P. EN COLUMNAS[(0.4x0.4)x3.37]x9x2400124321243212432CARGA VIVA:S/C [(4.8x2+0.4)(6.4+6.8+0.4)x250]x50%230402304011520PESO PARCIAL98227.20 kgf98227.20 kgf86707.20 kgfPESO TOTAL283161.60 kgfo:283.16 tn

III .-CALCULO DEL CORTANTE BASAL:PR1 =98.23TnPR2 =98.23TnPR3 =80.49Tn

DONDE:NIVELPi(Tn)hipihi%FiViZ =0.4380.4910.50 m845.160.450380039233.48tnf33.48tnfU =1.5298.237.00 m687.590.366413307227.24tnf60.71tnfC=2.52.5198.233.50 m343.800.183206653613.62tnf74.33tnfS=1.41876.54R=8F3 =33.48 tnfVb =74.33TnVn3=33.48F2 =27.24 tnf

F1 =13.62 tnfVn2=60.71

Vn1=74.33

IV .- GRADOS DE LIBERTAD DE LA ESTRUCTURA :

N GDL =12

V.- MATRIZ DE RIGIDEZ DE LA ESTRUCTURA.12345678910111217787.3194223255-3893.70.000.000.000.00-2271.30-2271.30-2271.300.000.000.002-3893.77787.3194223255-3893.72271.302271.302271.300.000.000.00-2271.30-2271.30-2271.3030.00-3893.73893.70.000.000.002271.302271.302271.302271.302271.302271.3040.002271.300.0021392.9853970.002649.850.000.000.000.000.0050.002271.300.0053973218753970.002649.90.000.000.000.0060.002271.300.000.005397213930.000.002649.85174787460.000.000.007-2271.300.002271.302649.850.000.0021393.053970.002649.90.000.08-2271.300.002271.300.002649.90.00539732186.56131685665396.78858133950.002649.85174787460.009-2271.300.002271.300.000.002649.85174787460.005396.788581339521392.98415417760.000.002649.8517478746100.00-2271.302271.300.000.000.002649.90.000.001609353970.00110.00-2271.302271.300.000.000.000.002649.85174787460.00539726886.85782110735396.7885813395120.00-2271.302271.300.000.000.000.00.002649.85174787460.005396.788581339516093.2806584283

VI .- CALCULO DE LA MATRIZ DE RIGIDEZ LATERAL:

7787.3194223255-3893.70.00[K11] =-3893.77787.3194223255-3893.70.00-3893.73893.7

0.000.000.00-2271.30-2271.30-2271.300.000.000.00[K12] =2271.302271.302271.300.000.000.00-2271.30-2271.30-2271.300.000.000.002271.302271.302271.302271.302271.302271.30

0.002271.300.000.002271.300.000.002271.300.00-2271.300.002271.30[K21]=-2271.300.002271.30-2271.300.002271.300.00-2271.302271.300.00-2271.302271.300.00-2271.302271.30

0.00-00.00-0.000.00-0.000.00-0.000.00-00-00.00-0.00.00-0.000.00-0.000.00-00-0.000.00-0.00000685850.00-0.000.00-0.000.00-0.000.0-00.00-0.00.00-0.00.00-0.00.00-00.0000349199-0.00000945380.00-0.0000046990.00-0.000.00-0.00000685850.00-0.00000945380.0000511521-0.000.00-0.00000947290.00-0.000.00-0.00.00-0.000-00.00-0.000.00-0.000.00-0.0000046990.00-00.0000437532-0.00001518820.00-0.000.00-0.00.00-0.00000947290.00-0.00001518820.0000687908

VI.I.- ENTONCES LA MATRIZ DE RIGIDEZ LATERAL SERA:

7246.8843626988-3876.1790345156467.7106520782[KL]=-3876.17903451566595.9618412697-3242.7371897336467.7106520782-3242.73718973362821.529930233

&G&G

321ABC