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ɣh2o = 62.4 (lb/pie3)

Nivel Freatico = 16.40 pies

Nivel Freatico = 5.00 Mts

Diaetro = 3!.00 "#l$

Diaetro = 3.1% pie Diaetro = 0.&% ts

"ies Metros 'ipo e s#elo

De asta De asta0.00 61.20 0.00 1!.65 *re+a ,iosa

61.20 %5.2& 1!.65 22.&5 *re+a -ravosa%5.2& !3.66 22.&5 25.50 *rcilla ,iosa!3.66 &&.05 25.50 30.1& *re+a +a e+sa

=0

*re+a ,iosa ɣ = 1!00 ($/3) =16.4 112.3 (lb/pie3)

*re+a ,iosa ɣ = 2000 ($/3)124.!5 (lb/pie3)

=61.2*re+a -ravosa ɣ = 2000 ($/3)

=%5.2& 124.!5 (lb/pie3)ɣ = 2000 ($/3)

=!3.66 *rcilla ,iosa 124.!5 (lb/pie3)*re+a +a e+sa ɣ = 2000 ($/3)

124.!5 (lb/pie3)

=&&.05

"ies (pies) * (pie2)De asta0.00 16.40 !.20 1.11 112.30 &20.!6 1025.30 163.15

16.40 61.20 3!.!0 0.66 124.!5 3240.60 2135.!5 445.6&61.20 %5.2& 6!.25 0.3! 124.!5 50%&.44 1&54.35 140.1%%5.2& !3.66 %&.4! 0.30 124.!5 5%!0.%5 1%13.&5 !3.2%!3.66 &&.05 &1.36 0.21 124.!5 6522.66 136%.62 153.10

esiste+cia al F#ste (lb) =esiste+cia al F#ste (N) =

Deteri+ar la capacia e apoo aisible e #+ pilote vaciao i+sit# e 3! p#l$. e i7ee pro8#+ia. *s#ir el si$#ie+te estrato.

ɣ

(lb/pie3)

9:9 ;1?_

 

 _

 _

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2100 pa *c = 0.%30

3%1!.501N

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D = %5 ts

A = 1.22 ts

D/A = 61.4%5

%&.%%05&

Boo A C %5 p#l$ 1035.00 N/2

1.1% 2

120&.2& N

De hasta *lt#ra

0.00 1.50 1.50

" (lb) 1.50 20.00 1!.50 33.33 6&5.&3 1.0020.00 40.00 20.00 62.&6 1314.60 0.6416%2!0.&6 40.00 %0.00 30.00 &6.2& 2010.54 0.4!&51&15.%3 %0.00 %5.00 5.00 2%3&45.!&142%16.1%20&3!&.%% 5&!5.134% N 600.6%4&

1%4524!.51%%63.25214

ro &0 pies Deteri+ar la capacia e apoo para #+ pilote vaciao i+sit# e iaEl s#elo es arcilloso co+ #+ valor variable e # co+ la pro8#+ia. *s

B#(N/2)

B#(lb/pie2)

.2 @= ⁄

   ;=_ ;

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* (2) " (N)

33.33 %0.!% 2362.0&40.2& %6.62 30!%.2046.22 114.&2 5311.%0

10%61 (N)

 '+

etro 1.22 %5 etros e pro8#+ia.ir #+ 8actor e se$#ria e 2

=

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DETERMINAR LA CARGA DE SERVISIO "Q", PARA OBTENER UNA DEFORMACI

DEF. EN LA PUENTA ( Wz) = 0.16% 8t F. EN LA PUENTA ( Wz) =

Lon!#$ (L) = 100 8t Lon!#$ (L) =

N#%&'o D!!!on& (n) = 5 N#%&'o D!!!on& (n) =

Mo$#*o E*+!!+$+ (E-) = 4.00E?06 psi o$#*o E*+!!+$+ (E-) =

D!+%'o ($) = 1 8t D!+%'o ($) =

L = 20 8t L =

PERIMETRO DEL PILOTE "P-" AREA DEL PIL

P- = %5.40 p#l$ A- =

FGE* EN ,* "GN'*

&21600 lb

Ho =Ho =

'a+teolb lb lb lb/p#l$2

5 & 0.0! &21600 &&532! &5!464 0.00! 2.004 1!.044 6 0.0% &4!!04 1015220 &!2012 0.00& 2.012 12.0%3 4 0.06 &6%011 1025031 &&6021 0.00& 2.021 !.0!2 3 0.05 &%&200 102!160 10036!0 0.00& 2.030 6.0&

=_=_ _   =_

I_ J K )(   J Ks#p(   〖 )(   〗 )〖∆∆〗 _ L_

   4_

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2 10 0.05 &!!3!1 103%!00 10130&1 0.00& 2.030 20.30

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ON DE 2" EN LA PUNTA

2 p#l$

100 p#l$

5

3.00E?06 psi

24 p#l$

20 p#l$

TE "A-"

5%6.00 p#l$ 2

1600 lb/p#l$2

4&023&3 lb21!06.&3 N

lb lbError

2%204 &4!!04 4.%1!20% &6%011 4.%121!& &%&200 4.5&1!1 &!!3!1 3.&

_    J Ks#p(   〖 )(   〗 )

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30616 101!&&% 1.!