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BEAM
IS456:
2000
I I
I
I
I
I
T-+----+-+----+---
Xl
I I
~
SECTION
XX
FIG.
3 TRANSVERSE
REINFORCEMENT IN
FLANGB
OFT-BEAM WHEN MAIN REINFORCEMENT Of
SLABIS
PARAIJ.EL
TO
THE
BEAM
e) For flanged beams, the values of a) or b) be
modified
as
per Fig. 6 and the reinforcement
percentage foruse inFig.4 and
5
should
be
based
on area of sectionequal
to
b d
NOTE-When
deflections
are
required
to
be calculated,
the
method given
inAnnex
C may be used.
2·0
,6
\
\ \
\ \
\
\
r-,
\
\
r
I
<
r-
\
<
r
-..
I -...
r ....
f
5
-
-,
<
I --
I-...
10. ,.
r---
f 90
r
I
f--...
fu240
-- -
h·290
,
I
Note: f . IS STEEL STRESS OF SERVICE
LOADS IN mm
2
I
o
0 4 0, ,2 1 6 2·0
PERCENTAGE TENSION
REINFORCEMENT
I .0.58 f ArMof
CI OII _tion
ohteel
required
•
.
Areaof
Cmll •
aection
of steel
provided
Flo. 4 MODIACATJON FAcroR
FOR
TENSION REINFORCEMENT
38
2 8 )0
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18456:
2000
100
. . .
L
V
/
V
/
0-50
00
1-50 2-00 2-50
PERCENT GE COMPRESSION REINFORCEMENT
F IG. 5
MOOIHCATION FACTOR FORCOMPRESSIONREtNPoRCBMENT
1/
/
/
/
0095
a:
e
e sc
L
z 0.85
Q
t
0·80
a:
1 1
0·75
0.70
o
0 2 0 4 0·8 0 8 1·0
RATIO
OF WEB
WIDTH
TO FLANGE WIDTH
FIG. 6 REDUCTION
FACTORS
FORRA 110S
OF
SPAN TO EJ rEcnVE DEPTH FOR FLANGED BEAMS
23.3 Slenderness Limit for Beams to Ensure
Lateral
Stability
A simply supported or continuous beam shall be so
proportioned that thecleardistance between the lateral
250b
z
restraints does not exceed 60
b
Of
whichever
d
is less, where d is the effective depth of the beamand
thebreadth of thecompression facemidwaybetwecn
the lateral restraints.
For a cantilever, the clear distance from the free end
of the cantilever to the lateral restraint shall not
100b
z
exceed 25
b
or _ - whichever is less.
24 SOLID SLABS
24.1 General
Th e
provisions of 13 .2 for beams apply to slabs
also.
NOTBS
1 Forslabsspanninl
in
twodirections,the shorterof the two
spans should
be
used for calculatingthe span to
etTective
depth ratios
2 Fortwo-wavslabsof shorterspans(up to m)withmild
stoelreinforcement, the span to overalldepth ratiosgiven
below may generally be assumed
10
satisfy vertical
deflectionlimits forloadingclassup to 3
kN m
J
•
Simplysupportedslabs
Continuous slabs 40
Forhighstn:ngthdefonnedbarsof
smde Fe
thevalues
givenaboveshouldbemultiplied by0.8.
24.2 Slabs Continuous Over Supports
Slabs spanning in one direction and continuous over
supports shallbedesigned according to the provisions
applicable to continuous beams.
24.3
S ~ ~ b s
Monolithic with Supports
Bendingmomentsin slabs(except
flat
slabs)constructed
monolithicallywith the supports shall becalculated by
takingsuch slabseitheras continuousover supports and
39
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d For cantilever solid slabs, the effective width
shall he calculated in accordance with the
followingequation:
b
er
=
2a
l
c For two or more loads not in a line in the
direction
of thespan if theeffective width of
slabforone load does notoverlaptheeffective
width
ofslab
foranotherload,
both
calculated
as in a above,thentheslabforeach loadcan
be designedseparately If theeffectivewidth
ofslabforoneload overlaps theeffective width
of
slabfor an
adjacent load
the
overlapping
portion
of the slab
shall
be
designed
for the
combined effectof the two
loads
Table14
Values
01k
for
Sbnply
Supported and
Continuous Slabs
Clause 24.3.2.1
where
ber = effective width,
=distanceof theconcentrated load from the
face of the cantilever support, and
=
widt h of contact area of the concentrated
load measured parallel to the supporting
edge.
Provided thattheeffective widthof thecantilever
slab shall not exceed one-third the lengthof the
cantilever slabmeasured
parallel
tothefixededge.
Andprovidedfurtherthatwhentheconcentrated
loadis
placed
nearthe
extreme
endsof
the length
of cantileverslab in the directionparallel to the
fixed edge. the effectivewidth shall not exceed
the above value, nor shall it exceed half the
abovevalueplusthedistanceof theconcentrated
load from the extreme end measured in the
direction parallel to the fixededge. .
24.3.2.2For slabs other than solid slabs, the effective
width shall depend on the ratio of the transverse and
longitudinalflexuralrigidities of the slab. Where this
ratio is one, that
is,
where the transverse and
longitudinal
flexural
rigidities arc approximately
equal, the value of effective width as found for solid
slabs
may
be used But as the ratio decreases,
proportionatelysmaller valueshall
he
taken.
IS 456: 2000
capableof freerotation.or as membersof a continuous
framework with the supports, taking into account the
stiffnessof suchsupports If suchsupports are
formed
dueto beamswhichjustify fixityat thesupportof slabs,
then the effects on the supportingbeam, such as, the
bending of the web in the transverse direction of the
hewn and
thetorsionin thelongitudinal directionofthe
beam.whereverapplicable, shallalso be consideredin
the designof the beam.
24.3.1 For the purpose of calculation of moments in
slabs in
a
monolithic structure,
it
will
generally
be
sufficiently accurateto assumethatmembersconnected
to the ends of such slabs are fixed in position and
direction at the ends remote from their connections
with the slabs.
24 3 1 Slabs CarryingConcentratedLoad
24 3 2 1
Ifa solidslabsupportedon twooppositeedges,
carries concentrated loads the maximum bending
moment caused y the concentrated loads shall be
assumed to be resisted by an effectivewidth of slab
measuredparallel to thesupportingedges as follows:
a For a single concentrated load. the effective
width shallbe calculatedin accordancewith the
following equation provided that it shall not
exceed the actual width of the slab:
b
r
kx
1
.. .. +
a
lef
where
d
= effective width of slab,
k constanthavingthevaluesgiveninTable
14dependingupon theratioof thewidth
of the
slab to the effective span {
x
=
distance
of the
centroid of
the
concentrated load from nearersupport,
I
r f
= effective span, and
a
width of the
contact area
of
the
concentrated load from nearer support
measuredparallel to thesupportededge.
And provided further that incase of a loadnear
the unsupported edge of a slab. the effective
width shall not exceed the above value nor half
theabovevalueplusthe
distance
ofthe
load from
the unsupported edge.
b For two or more concentrated loads placed in a
line in the direction of the span, the bending
moment per metre width of slab shall be
calculated separatelyfor each loadaccordingto
its appropriateeffectivewidthof slabcalculated
as in a above and added together for design
calculations.
40
0 1
0.2
0.3
0.4
S
0.6
0.7
0.8
0.9
1.0and above
i
lorSlmpl,
Supported S
0.4
0.8
1 16
1.48
1.72
1.96
2.12
2.24
2.36
2.48
i rCoatlDUQUI
0.4
0.8
1 16
1.44
1.68
1 84
1.96
2.08
2.16
2.24
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24.3.2.3
Any
other recognizedmethodof analysisfor
Casel
of Ilaba
covered
by
24.3. .1
and 24.3.2.2 and
fot all othet ~ s e of slabs may be used with the
approvai OfaM engineer*in-charge.
24.3.2.4 The critidilMedon for checking shearshall
be
as
Jiven
in
34.2.4.1.
24.4 Slabs SpaDllinllD two Directions at Rllbt
ADII_
The slabs spanning
in two directions at right angles
and carryinS uniformly distributed load may be
desilned by
any
acceptable theory or by usina
coefficients liven in
Annex
D. For determining
bending
moments in slabs
spanningin two directions
at right anales and carrying coaeentrered load, any
acceptedmethod approved
by
the engineer-In-charge
maybeadopted.
NOTS The IDOII
commonly UJed elasticmethods are based
onApaud , or
Wester-pard ,
theory
and
themost commonly
uled
limit
ItaJeof
coUapsemethod
is
based
onJohansen s
yield-
linetheory.
4 4
Restrained Slabwith
Unequal Conditions
at
Adjacent Pan
In some cases the support moments calculatedfrom
Table
26 for adjacent panelsmay differ significantly.
The following procedure may
be
adopted to adjust
them:
a) Calculate
the
sum of
moments at midspan
and
IUpports
(nea1ecting
signs).
b)
treat the values
from
Table 26 as fixed end
m<mieDts.
c) According t the relative stiffness of adjacent
spans, distribute the fixed end moments across
the supports,living new supportmoments.
d) Adjult midspanmomentsuch that, whenadded
to the support moments from c) neglecting
IS 56:2000
signs),the totalshouldbe equal to that from a).
If the resulting support moments are
signifi
cantlygreaterthan the value from Table26, the
tension steel over the supports will need to be
extended further. The procedure should be as
follows:
1) Takethe spanmomentas parabolic between
supports: its maximum value is as found
from d).
2)
Determine
thepoints of contraflexure of the
new support moments [from c)] with the
span moment[from 1)].
3) Extendhalfthesupporttensionsteelateach
end to at least an effective depth or 12bar
diameters beyond the nearest point of
contraflexure.
4)
Extend
the
full area of the support tension
steel at each end to half the distance from
3).
24.5 Loads on SuPportiDI Beams
The loads on beams supporting solid slabs spanning
in two directions at right angles and supporting
uniformly
distributed loads, may be assumed to bein
accordance withFig. 7.
25 COMPRESSION MEMBERS
25.1 Definitions
25.1.1Columnor strut is a compressionmember, the
effecti
velengthofwhichexceeds threetimes the least
lateral dimension.
25 2 ShortandSlenderCompression Members
A compression member may
be
considered as short
· I
h
when boththe slenderncb; ~
D
and b are less
than
12:
A
6 818 07 1
LO IN THIS SHADED
AREA T BE CARRIED
V BEAM e
LOAD IN THIS SH E AREA
TO BE
CARRIED
Y BEAN
FlO.
7 LO CARRJIID BY
SUPPORTING
BEAMS
41
B
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IS 456 : 2000
where
1
M
= effective length in respect of the major
axis,
== depth in respect of the major
axis,
I -
effective length in respect of the minor
ry
axis, and
b
=
width of the member,
It shall otherwise be considered as a slender
compression member,
25 1 3 Unsupported Length
The unsupported length, I of a compression member .
shall he taken as the clear
distance
between end
restraints except that:
a in flat slab construction, it shall be cleardistance
between the floor and the lower extremity of
the capital, the drop
panel
or
slab
whichever is
the least.
h
in
beam and
slab
construction,
it
shall be the
c lear d is tance between
the
floor and the
underside of the shallower beam framing into
the columns in each direction at the next higher
floor level.
c in columns
restrained
laterally
by
struts,
it
shall
be the
clear
distance between consecutive
struts in each vertical plane, provided that to be
an adequate support, two
such
struts shall
meet the columns at approximately the same
level and the
angle between vertical
planes
through the struts shall not vary more than
3Qt
from a right angle. Such struts shall be of
adequate dimensions and shall have sufficient
anchorage to restrain themember against lateral
deflection.
d in columns restrained laterally by struts or
beams,
with
bracketsused at thejunction, it shall
be
the
clear distance between the
floor and
the
lower edge of the bracket, provided that the
bracket width equals that of the beam strut and
is at least half that of the colurnn.
25.2 Effective Length of Compression Members
In the absence of more exact analysis, the effective
length ler of columns may
be
obtained as described in
Annex E.
25.3 Slenderness Limits for
Columns
25.3.1 The
unsupported
length between endrestraints
shall not exceed 60 times the least lateral dimension
of a column.
25.3.2 If,
in any given
plane, one end of
a column
is
unrestrained, its unsupportedlength,
it
shall notexceed
JOOb
2
[
where
b
= width-of that cross-section, and
= depthofthe
cross-section
measuredinthe
plane underconsideration.
25.4 Minimum Eccentricity
All columns shall be designed for mmrmum
eccentricity,
equalto theunsupported
length
of
column
500plus lateraldimensions/30, subject to a minimum
of20
rom.
Wherebi-axialbending
is
considered,it is
sufficient to ensure that eccentricity exceeds the
minimum aboutone axis at a time.
26 REQUIREMENTS GOVERNING
REINFORCEMENT
AND
DETAILING
26.1 General
Reinforcing steelof sametypeand
grade
shallbe used
as main
reinforcement
in a
structural
member
However.
simultaneous
use of
twodifferent
types or
grades
of steel for mainand
secondary
reinforcement
respectively is permissible.
26.1.1 Bars may be arranged singly. or in pairs in
contact,
or
in groups of three or four bars
bundled
in
contact. Bundledbarsshall
be
enclosedwithin
stirrups
or ties. Bundled bars shall be tied together to ensure
the bars remaining together. Bars larger than32 mm
diametershall notbe bundled.
except
in columns.
26 1 2
The
recommendations
for
detailing
for
earthquake-resistant construction given in IS 13920
should be taken into consideration, where applicable
seealso
IS 4326 .
26.2 Development
of
Stress in Reinforcement
The calculated tension or compressionin
any
bar at
any
section shall be developed on each side of the
section
by
an appropriate
developmentlength or end
anchorage or
by
a combination thereof.
26 2 1 Development Length
Bars
The development
length
L
d
is given by
L
_ a.
1
f d
where
, =
nominaldiameterof
the
bar,
a =stressinbarat the sectionconsideredat design
load,
and
t
hd
=design bond stress given in 26 Z
NOTES
1
he
development
IcnJlh
includca
anchomae
vDlues
of
hooks
in
tension reinforcement.
2 For barsof
sections
other th n
cireular.
the
development
lenathshould be sufficient to
develop
the stras in thebar
by bone
0°
...
:
..... l
42
I,
:i
c
.;.