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Selected
le Sections
1992, 2001, 2011Structural aU eee cern
    
‘ene 3
rainforest
‘of shear ° .
dicular co flex
fai members, mm:es
Sack
(ak as
Bese
factor relating shear and to!
Pee
~axy
distance from extreme compr
reinforcement, but need not be less t
(For circular section, d need not be
compression fiber to centroid of tension
member.)
sional stress properties
ession fiber to centroid of longi
jess than 0.80h for pr‘ stressed me
sg than the distance froi
nforcement in oppo
specified compressive strength of concrete, MPa
ength
due to un
is caused bye
mmpressive stress in concrete (att vs >
centroid of c i
and flange when the centroid lies with age, MPa.
member, fpc is resultant compressiv centroid of composit
at junction of web and flange when the centroid lies
both prestress and moments resisted by member acting alol
fye = Compressive stress in concrete due to
allowance for all prestress losses) at extreme fiber of section
__ stress is caused by externally applied loads, MPa #
pecified tensile strength of prestres:
ctive prestress force
sing tendons, MPa
eth of nonprestressed reinforcement,
a:nd Construction
Structural Engineering
longer overall dimension of rectangu
dimension of closed rectal g
“yx =longer center-to-center
| axis of gross Section, negl
” yc = distance from centroidal
extreme fiber in tension
= angle between inclined stirrups and long!
itudinal axis of memb
~ angle between shear-friction reinforcement and shear plane
constant used to compute Vein slabs
= coefficient as a function of yi/xs. See
ratio of stiffnes: hearhead arm to
5.111245
= ratio of lo:
constan|
1.
= number of identi earheads
= correction factor related to unit mass of concrete
= coefficient of friction. See Sec. 5.11.7,4.3
= ratio of nonprestressed tension reinforcementmembers,
be designed for the samme
‘face of support may
bers, brackets and corbels, wal
11.8 through Sec.
~ §.41,1.4 For deep flexural mem
Tootings, the special provisions of Sec
5.11.2 Lightweight Concrete
$.11,2.1 Provisions for shear strength V
to normal weight concrete. When lightwe'
the following modification shall a
and torsional moment strenga
ight aggregate concrete 15.4
§,11.2.1.1 When fa is specifi proportioned in a¢ed
with Sec. 5.5.2, p i by substitutiny
Teal
0.85 for 4
partial $4
Members”
$.11.3,1.2 For me41.3.2 Shear strength Ve m: +
51132.) through $1395 ee
but r
than
simu!
5.11.3 ubject to-axial compression ‘Eq.
ituted for My and Va. d/Me
aken greater than
lowever, V; shall not be tnd Construction i !
wl v Nu/Ag shall be express
neve Na is negative for tension, Quantity 1v/Ay shall be express
where Nu a
5.11.4 Shear Strength cre Prestressed Members —
ovide rete fo
11. ength Provi :
44.44 For members with effective prestress force not I spe 40 perce
tb th of flexure reinforcement, unless a more detailed caleuat
the tensile strength of flexure
made in accordance with Sec. 5.11.4
n applying Eq.
me compression
5.11.42 Shear
be computed in accordance with See: a
where V- shall be
the lesser of Va or V.
5114.21 Shear strength Vx shall be computed by
yas 0 VM,
Vas X—* bwd + Va 4 wie
20 agSa
Peed
(e) Combin
ad 7 hall not e
: en yield strength of shear reinforcement <
or her bars or wires used as shear Height. ae a
5:11.5.3 Stirrups and five compression fiber and shall be anchored al Bi
to a distance d from extreme co! on ne
2.13 to develop the
according to Sec. 5.12.13 to develop
¢ Shear Reinforcement
woe g Limits for Shear Rein’ :
5.11.54 Spacing Lim ed. perpendicular to
ed members and (3/4)
e provided in all
i - nofprestres:
ength provided B
1155.2 Minim ements of Sec. 5.14,5:60
ee ots oy by nominal flexural and shear!
simulate sreloPed when shear reinforcement is omittiar Such test
aries elects of different settlement, creep, shrinkage, and
lange, based on a realistic assessmentt of saci ving
ti ‘ment of such effects occurring]
nt is required by Sec.
malySis, and where factored torsional moment
5:11.5.5.3 Where shear reinforceme;
it Tu does
abi
Sanit atea of shear reinforcement for pres
+554) and nonprestressed member41.5.5.4 For
prestresse
an 40 percent of the ie h
shear reinforcement shall Tete a than tie
less than the
he
Alas Eee
me
80fd Yb,
all be $0
epth of
at least
1 in Seem
6 Design of Shear Reinforcement
shear force Va
nrovided to satisty Bg. (11
inforcement
accordance:
mngth Vs shall be computed in“511564 When shear a renforcement const 0
of parallel bars, al
forcement is 4
stressed Memb
re where fa
be taken as a solid
x section with wall t$1.63. Insuc
u a case the cor por ;
palo rsshallbrwed neal aaa
$.11.6.3.2
oa ; ' jorsional loa fr
dong the ae
611.64 t t
han a distance d from fee of
desigr
§.11.¢
shall
d to
mputed)
) bw di
dered and Ts
where
accor
provid
nt strength Provit
eth Te
§.11.6.6 Torsional Mome
§.11.6.6.1 Torsional moment strenST
Engineering and Construction
T
by Eq. (11-5) shall be multiplied by (1 + 0.3NW/Ag),
tension
5.11.6.7 Torsion Reinforcement Requirements ae
5.11.6.7.1 Torsion reinforcement, where required, Shall be pROW
addition to reinforcement required to resist shear, flexure, and axial cl
5.11.6.7.2 Reinforcement required for torsion shall be combined
réquired for other forces, provided the area furnished is) the:
individually required areas and the most restrictive requirements fOr Sp
and placement are 1
Torsion reinforc
nforcement shall not exceed 4
‘i
a torsion reinforceme
>mpression fiber and shall
> the design yield sthengtfi
e
in
(least a distance (bias
Bi
a
nforcement
ips shall not exceed the smaller
5.11.6.8.2 Spacing of longitudinal bars, not less than 10 mm, distri
‘ound the perimeter of the closed stirrups, shall not exceed 00) mi
one longitudinal bar shall be placed in each corner of the closed!
5.11.6.9 Design of Torsion Reinforcement
5.11.6.9.1 Where factored torsional moment Ty exe
strength $T., torsion reinforcement shall be provided to
(11-21), where torsional moment strength Ts shall be co mpF where Ac is the area of |
distance s, and a. =
Perimeter
Provided in accordance with Sec. 511 64)
$:11.6.9.2 A minimum area of dosed stirrups
with Sec. 5.11,5.5.5, i :
§.11.6.9.3 Required area of longitudinal bars Ar di
‘ter of the closed stirrups at shall be computed by:
Bu: for 2Ae
3f,
116.94 Torsional moment strengt Te
5.11. orsion:where pis coefficient of
5.11.7.4.2 When shea
that the shear force produc
gth Va shall be computed by
v (sin cw + cos or}
uctural ste
einforcing ba
where A= 1.0 for normal weight concrete, 0.85 fot
and 0.75 for “ali light-weight” concrete.
when partial sand replacement is used,
5.11.7.5 Shear strength V,
shall not be taken greater than 0.
Newtons, where Ac is area o
f concrete section resisting shea
5.1.7.6 Design yield strength of shear-friction reinf
415 MPa.
5.11.7.7 Net tension across shear plane
© reinfor net
| additii eam
aceon) ements
44.7.9 For the purrs
Purpose of Section 5.147, when
Concrete, the interface for shear b
FIs assume equal to 1.0%, interface shall
ximately 5 mm,
or Deep Flexural Members
5.11.8 shall apply to members with!
‘ace and supported on the opposite face
op between the loads and the supports,
ported deep flexural members for
he shear strength Vesshall bel
shear strength Vs shall be!
en V; for deep flexural members sell iia
j s
when ln/a is between 2and Se
a 10+ bed
ial 4
‘ection for sheat measured
5.11.8,5 Critical 5 oi
jformly,
a distance 0.15%ls oF Ut ter thal
concentrated loa
5.1.8.6 Unless 4 ™°!
51187,Pees
eer Rist cna
all not exceed 2.5 and V- shall not be taken greater th
factored moment occurring simult: he
in Sec.5.11.85.
5.11.8.8 Where factored
reinforcement sh
strength Vs s
§.11.8.11 Shear r
5.1.8.5 shall be used
5.11.9 Special Provisions for Brackets and Corbels
11.9.1 Provisions of Sec, 5.11.9 shall apply to brackets and
‘span-to-depth ratio a/d not greater than unity, and subject toa
ee Nuc not larger than V., Distance d shall be measured at
11.9. ‘outside edge of bearing aréa shall
‘i : Dena
shall5.11.9.3.2.1 For normal
eater than 0.2,
Weight bie
bod nor 55 bud i
me An to resist tensile force
sile force Nuc shall not be
tension reinforeement Ac é
Ave + An). Viagag
5.11.9
05
adja
$11.5 ii not b
511.9 ¢ or corbel, primary fen
‘be anch: lowing: (a) by a structural
atlea be designed to develop 
 Le
: Ses Mp
smodulus of elasticity o
torsional c
‘The limiting |Structural Engineering and Construction
Note: rs
may be approximated accurately and conservatively as the ra
of
the compression flanges plus one-sixth of the web: