Raft Design
Short Description
Excel sheet for designing the Raft foundations...
Description
CHEC Bearing Capacity =
Tn9: 2
1.8
Qn = LEFT-OS TO-OS
LX-1
DX-1
0
D$-2
! ." #
31 8
0
1"#
!4
#!
1#1
%0
!%
2%2
41 2
0
2""
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
88 4
1 2#
8%#
! ." #
L$-3 D$-3 L$-4
1 # .3 3
D$-4
0
L$-# D$-#
0
L$-! D$-!
0
L$-" D$"
0
L$-8 D$-8
0
L$-% D$-%
0
L$-10 0
TOT&L-L
TOTAL-DY
LX-3
" .0 ! "
L$-2
BOT-OS
DX-2
! ." #
L$-1 D$-1
LX-2
4 .0 3 2
29.147 LE'(T) OF *&FT +,T) OFFSETS/
=
# % .2 #
)&LF LE'(T) OF *&FT +,T) OFFSETS/ 2
=
2%.!2#
LE'(T) OF *&FT +,T)OT OFFSETS/ L
=
# % .2 #
)&F LE'(T) OF *&FT +,T)OT OFFSETS/ L2
=
2%.!2#
,DT) OF *&FT +,T) OFFSETS/ y
=
2%.14"
)&LF ,DT) OF *&FT +,T) OFFSETS/ y2
=
14.#"3#
,DT) OF *&FT +,T)OT OFFSETS/ ,
=
2%.14"
)&LF ,DT) OF *&FT +,T)OT OFFSETS/ ,2
=
14.#"3#
= 56312
=
1 2 2 2 ! 1 .2 1
$ = 65312
=
# 0 # 2 1 ! .! 8
S OF &LL SE*CES LO&DS/
=
#0# 1
&*E& OF *&FT/ 5 X 6
=
1 " 2 ! .% # % 8
X7
=
31.1!"%3"
EX = X7 - +L2
=
1 .# 4 2 % 3 "
$ = EX
""%3.3"#
$ = EX
""%3.3"#
$7
=
1 4 .4 " " 1 8
E$ = $7 - +,2
=
-0.0%!31%!
= E$
- 4 8 ! .# 1 0 #
&
=
-2.%24"%31
+ $ . 2 $
=
0.4#!%8%#
+ X . y2 X
=
-0.0#"%%1%
;1 =-+& - ++ $ . 2 $ - ++ X . y2 X
=
-3.323"%0"
;2 = -+& < ++ $ . 2 $ - ++ X . y2 X
=
-2.40%811"
;3 = - +& < ++ $ . 2 $ < ++ X . y2 X
=
-2.#2#"%##
;4 =-+& - ++ $ . 2 $
E?ec@Ae E?ec@Ae 5earing 9tre99 r t6e 9i
100
S5 gra>e >9
20/000
Cncrete 9trengt6 ra:
1!.#
*einrceent 9tee 9trengt6
420
Why Raf should be used ;e
=
100 '2
ai >ea> a> n cn
=
3#0 '
ai iAe a> n cn
=
2#0 '
Tta ai 9erAice aia a>
=
!00 '
&rea 9inge 9;. @ng
=
!.!0 2
,i>t6 >ept6 t6e @ng
=
2 .# "
r
3
3
T6i9 area i9 cn9i>ere> t 5e Aery 5ig t 5e ecaAate> ecaAate> 9 ra: i9 re ecnica an> ecient r t6i9 n>a@n
Raf Thi!"ess n ra: ra: n> n>a@ a@n n t6ic t6icne ne99 99 can 5e >ete >eteri rine> ne> 5y c6ec c6ecing ing t6e >iagn >iagna a ten9i ten9in n 96ear 96ear t6at t6at Gi Gi 5e i i t6e ai @ate cn a> Gi 5e 9e> in t6e caca@n. = +5+>+H+0.34+ +5+>+H+0.34+ c7 = actre> cn a> H = re>c@n actr 5 = t6e perieter t6e 96eare> area > = e?ec@Ae >ept6 ra: c7 = cpre99iAe 9trengt6 cncrete n t6i9 ra:
>2 =
820 '
=
0.82 '
0.4
= 5 =
0.82 '
0.4
n >iaen9in
1.!
>2
> >2
=
+C%%+>+0."#+0.34+c7
SAe anay an> In> > a:er In>ing > a>> "# r cAer an> 2# r 5ar area CAer =
"#
0.82
=
+C%%>2 a=
= 4
5=
1.!
c=
-0."%2
+C%%>2 1.03! 0."%2
2.302
-#.#02
0.200
-0.!00
>=
300
S t6icne99 ra: =
300
Tae p9i@Ae Aae t t6e9e tG r J>J
11.81 in
Raf #e$%h he! One Gay S6ear =
ai 96ear - +d +w 9i
T >eterine t6e G9i/ t6e aAerage 9i pre99re 96> 5e >eterine> in t6e ai a>9 9trip9 &99e a. Aae 96ear i9 =
21"3 '
r t6e 9trip/ t6e @ate 5earing 9tre99 t6e 9i ;t
=
+Tta actre> a> in 9trip area t6e 9triparea 9trip 2%%!
44%!
44%4
2%%!
8.3#21 G9i
=
G9i
=
#184.08
>
=
22#
=
1"%4 '2 '
ai 96ear - +d +w 9i 21"3 +d +w 9i
= >=
100!.! ' +1000
=
+0."#+c7+1!+B >=
!8#.0
Not OK in one way Punching
TG Gay S6ear
0.#
>2
a
a Cn aia a> - +>=
-41.8
OK in two way Punching
& ' s%(i$ desi)"* Posi+,e -o.e"%s /Bo0o. (ei"1o(e.e"%2 >=
22#
< +a
3".4 '.
<
0.8"
! 374.3
r
p9i
H5>2 g t t6e ta5e ρ = ρ = K +9e> =
0.0088
re t6an
0.0088
e99 t6an
0.0088
&9 =
K5>
&9 =
1%80
Kin =
Ka = 0 .01%
103083#.08%
0.8#c5 a
=
c
=
=
+r !0/000 p9i an> 3/#00
2
C6ec c &9Fy
+r !0/000 p9i an> 3/#00
OK
use 3455 6 73 1o( $osi+,e .o.e"%s i" & di(e+o"' Bo0o. (ei"1o(e.e"%
a=
0.003#
1402# "3.#0 aB1
8!.4"
8
735455
.. 9
= >
=
>
=
Pt
=
8!.4" 6-cAer 22# M+>-ccN0.003 0.0048
t6en 9e H =
0.00#
+Ten9in Cntr
3".4
'.
0
c
=
H+&9+FyM+> - +a2N
=
0.00 '.
0
1o( $osi+,e .o.e"%s i" & di(e+o"' Bo0o. (ei"1o
6
73
8
735
Ne)a+,e -o.e"% /To$ (ei"1o(e.e"%2 >=
22#
< +a
3".4 '.
<
0.8"
=
H5>2 g t t6e ta5e ρ =
0.00!4
re t6an
ρ =
0.003#
e99 t6an
K +9e> =
0.00!4
&9 =
K5>
&9 =
1440
! 12".0
r Kin =
0.003#
Ka = 0 .01%
p9i
+r !0/000 p9i an> 3/#00 +r !0/000 p9i an> 3/#00
OK
2
use :455 6 73 1o( "e)i+,e .o.e"%s i" & di(e+o"' To$ (ei"1o(e.e"%
8
355455
.. 9
C6ec c a=
&9Fy
!18#01.0#3"
0.8#c5 a
=
c
=
1402# 44.10 aB1
= >
=
>
=
Pt
=
#1.88 6-cAer 22# M+>-ccN0.003 0.0100
t6en 9e H = c
0.00#
+Ten9in Cntr
3".4
'.
0.% =
H+&9+FyM+> - +a2N
=
112.%" '.
OK
1o( "e)i+,e .o.e"%s i" & di(e+o"' To$ (ei"1o(e
; ' s%(i$ desi)"*
Posi+,e -o.e"%s /Bo0o. (ei"1o(e.e"%2
6
73
8
355
Posi+,e -o.e"%s /Bo0o. (ei"1o(e.e"%2 >=
200
< +a
3".4 '.
< H5>2 g t ; ta5e ρ = ρ = K +9e> =
! 1#9.#0
1.10 r
= 0.00%
re t6an
0.003#
e99 t6an
K5>
&9 =
1800
Ka = 0 .01%
+r !0/000 p9i an> 3/#00 +r !0/000 p9i an> 3/#00
OK
0.00%
&9 =
Kin = 0.003#
$%i
2
use
=
>
=
Pt
=
!%.18 6-cAer 22# M+>-ccN0.003 0.00!8
t6en 9e H = c
0.00#
Ten9in Cntr
3".4
'.
0.% =
H+&9+FyM+> - +a2N
=
14#.1" '.
OK
1o( $osi+,e .o.e"%s i" ; di(e+o"' Bo0o. (ei"1o
6
73
8
::5
Ne)a+,e -o.e"% /To$ (ei"1o(e.e"%2 >=
200
< +a
3".4 '.
< H5>2
1.10
=
g t ; ta5e ρ =
0.00"!
re t6an
ρ =
0.003#
e99 t6an
K +9e> =
0.00"!
o&
! 1#9.#
Kin = 0.003# Ka = 0 .01%
$%i
+r !0/000 p9i an> 3/#00 +r !0/000 p9i an> 3/#00
OK
&9 =
K5>
&9 =
1#20
2
use
- +a2N
=
14#.1" '.
OK
1o( "e)i+,e .o.e"%s i" ; di(e+o"' To$ (ei"1o(e
'o(ent )a*ue +,N.(( / t&i$ oo( A% To$ A% Y t&i$ oo( A% To$ A%
3".4 3".4 3".4 3".4
6
73
'anua* De%ign H 2# 2#0 mm H 2# #00 mm H 2# 330 mm H 2# 330 mm
8
::5
K OF RAFT AREA AGAINST THE BEARING PRESSURE OF SOIL
DX-3
LX-4
DX-4
11.#
LX-#
DX-#
11.#
LX-!
DX-! LX-"
11.#
DX-"
11.2#
LX-8 0
204
22"
188
40#
0
0
0
0
24#
0
0
#10
0
24#
0
23#
2#2
20#
431
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
43%
%8%
3%3
132!
0
OR OR OR OR
'2 '3 a
2/3%3 p9i
a
!0/%1! p9i
9e> in t6e ra:
2
2.8%
a. 96ear 9trip 2.8%
>2
%42.8!!3
cncrete
cncrete area +2
H 5ar 10
"8.#
12
113.1
1!
201.1
20
314.2
22
380.1
2#
4%0.%
32
804.2
.. 9
cncrete
cncrete
.. 9
10
"8.#
12
113.1
1!
201.1
20
314.2
22
380.1
2#
4%0.%
32
804.2
cncrete
cncrete 10
"8.#
12
113.1
1!
201.1
20
314.2
22
380.1
2#
4%0.%
32
804.2
10
"8.#
12
113.1
1!
201.1
20
314 2
.. 9
cncrete
cncrete
20
314.2
22
380.1
2#
4%0.%
32
804.2
12
11.81
.. 9
ent +5-in
*n
2*nFy
*6
33101"."
3"4.3
2%.%
0.3"
0.00!8
33101"."
3"4.3
2%.%
0.3"
0.00!8
33101"."
3"4.3
2%.%
0.3"
0.00!8
33101"."
3"4.3
2%.%
0.3"
0.00!8
DX-8
LX-%
DX-% LX-10
0
TOTAL-D/
*()T-OS TOT&L-L
0
0
#9.2#
0
0
1#1"
0
0
#1!
0
0
120!
0
0
1812
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0 0
0
0
#0#1
#0#1
De%ign o oo5ng% +a6 oo5ng%
De%ign o oo5ng% +a6 oo5ng% Laye& A +*o8a* / Di&ec5on - To$ e8a&% *e;ire> reinrceent = *e;ire> era *einrceent = Dia. =
0.#
0.#
inc.2:
0.#
inc.2:
inc
9ing Bar '.
4
&rea ne 5ar =
' Bar9 re;. Spacing Bar9
= =
9ing B ar '.
4
' Bar9 re;.
=
3
Spacing Bar9
=
4
9ing Bar '.
4
' Bar9 re;. Spacing Bar9
= =
9ing B ar '.
4
' Bar9 re;.
= =
3 4
inc6 cc
Laye& A +*o8a* / Di&ec5on- oo( e8a&% *e;ire> reinrceent = *e;ire> era *einrceent = Dia. =
0.#
0.#0
inc.2:
0.#
inc2:
inc
&rea ne 5ar = inc6 cc
Laye& +*o8a* Y Di&ec5on- To$ e8a&% *e;ire> reinrceent = *e;ire> era *einrceent = Dia. =
0.#
0.!
inc.2:
0.!
inc.2:
inc
&rea ne 5ar =
3 4
inc6 cc
Laye& +*o8a* Y Di&ec5on- oo( e8a&% *e;ire> reinrceent =
0.44"! inc.2:
*e;ire> era *einrceent = Dia. =
0.#
0.4
inc2:
inc
Spacing Bar9
&rea ne 5ar =
3 #
inc6 cc
'ini(u( eino&ce(ent T6icne99 @ng Sa5 =
18
0.3888 inc.2:
in *einrceent = 0.0018. 5 .6 = 9ing
#
inc
%
inc6 cc
< < < <
4 4
= = = =
&rea ne 5ar =
:LT ; *o8a* /- Di&ec5on +To$ *o8a* /-Di&ec5on +ot. *o8a* Y- Di&ec5on +To$ *o8a* Y-Di&ec5on +ot.
A 'ODL
4 4
4 4 4 #
inch cc inch cc inch cc inch cc
0.2 inc.2
0.2 inc.2
0.2 inc.2
0.2 inc.2
0.31 inc.2
ent i9 nGn r cacate> r t6e ET&B9 / S&
ent i9 nGn r cacate> r t6e ET&B9 / S& >e etc t6en &rea Stee +& 9 c7 =
3000
psi
y =
60000
psi
Mu =
19
k-ft
Bea Dien9in +inc6 >=
18.25
%
21
inch
A&ea o tee* i% gi)en 8y ; As = (0.85.f c ' .b.d/f y )*(1-(1-(2.Mu /0.9.b.d 2 .0.85f c' )1/2 ) =
0.24
inch2/ft
ini &rea Stee = 0.0018.5.6 = Bar '
4
0.34
inch2/ft
t 5e 9e> / t6en Spacing G> 5e
!.%
inc6 cc
Design Data Fy= Fc'= $p%n= &ie &!%( De%( &!%( M!*ent !efficient +*i( sp%n,= M!*ent !efficient +$upp!"t,= ssu*e( $ef &!%(= !t% F%ct!"e( &!%(=
60000 2400 Density Of !nc"ete 15 Feets 350 &)/ft 350 &)/Ft 8 10 103.3435 &)/ft 1229.68125 &)/Ft
150 #cf
Design Solution h! +%,= 0.50 h! +%,= n= )(2=
0.011 0.0086 448.6153 #si 102.894 in3
F )= hen (= Depth "eui"e( f!" (efecti!n+sp%
12 inch 9.26 n( h= 11.25 inch
7$ i(th )= :ei;ht h=
12 nch 12 nch
O< in Defecti!n
Steel Calculations !tt!* !efficient M!*ents +&)-inch, M!*ents + !p
> !tt!*
10
8
10
0
332/014
41#/01"
332/014
D0U
28
28
28
28
450.836315985 360.6690928
?D@/0A
n
360.6690928
*
29.4116406
2*n/Fy
0.353591542
0.441996442 0.353591542
?D@/0A
h!
0.006664281
0.0086021239 0.006664281
?D@/0A
s
0.5920
0.9806421206 0.5920
?D@/0A
Bar Dia
No. Of Bars
29.41164059 29.4116406 29.41165
No. Of Bars
No. Of Bars
3
6.9
8.9
6.9
4
3.9
5.0
3.9
5
2.5
3.2
2.5
6.0 .0 8.0 9.0 10.0
1. 1.3 1.0 0.8 0.6
2.2 1.6 1.2 1.0 0.8
1. 1.3 1.0 0.8 0.6
Capacity Check of selected section $eecte( (i*ensi!ns )= (= Steel
12 12 4 s= %= #hi Mn=
4 0.9 1.9 402464.0 O<
5 0.98 2.4 488894.6 O<
33.5
4 0.9 1.9 402464.0 &)-inch O<
40.
33.5
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