This document discusses shear and torsion strength design of beams. It introduces the concepts of shear stress and torsion stress, and how they are related to the internal forces in a beam. The document explains homogeneous and non-homogeneous beam behavior under shear and torsion loading based on classical beam mechanics. It provides equations to calculate maximum shear stresses and strains in homogeneous and non-homogeneous beams. Failure modes such as flexural failure, diagonal tension failure, and shear compression failure are also discussed for beams without diagonal tension reinforcement.
2. NPIC
TajEkg (tensile normal stress) ft nigkugRtaMgkat; v CatMélenAkñúgFatu A1 enAelIkat;bøg; a − a
Rtg;cMgay y BIG½kSNWt.
BIeKalkarN_ classical emkanic eKGacsresrkugRtaMgEkg (normal stress) f nigkugRtaMg
kat; v sMrab;Fatu A1 dUcxageRkam³
My
f = (5.1)
I
nig v=
VA y VQ
Ib
=
Ib
(5.2)
Edl M nig V = m:Um:g;Bt; nigkMlaMgkat;enARtg;muxkat; a − a
A = RkLaépÞrbs;muxkat;enARtg;bøg;Edlkat;tamTIRbCMuTMgn;rbs;Fatu A1
y = cMgayBIFatuGnnþtUceTAG½kSNWt
y = cMgayBITIRbCMuTMgn;rbs; A eTAG½kSNWt
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 215
3. T.Chhay
m:Um:g;niclPaBrbs;muxkat;
I=
Q = m:Um:g;sþaTicrbs;RkLaépÞmuxkat;EdlenABIxagelI b¤BIxageRkamG½kSNWt
b = TTwgrbs;Fñwm
rUbTI 5>2 bgðajBIkugRtaMgxagkñúgEdlmanGMeBIelIFatuGnnþtUc A1 nig A2 . edayeRbIrgVg;m:
(Mohr’s cicle) enAkñúgrUbTI 5>2(b) kugRtaMgemsMrab;Fatu A1 enAkñúgtMbn;TajxageRkamG½kSNWtkøayCa
2
⎛f ⎞
f t (max)
f
= t + ⎜ t ⎟ + v2
2 ⎝2⎠
kugRtaMgTajem (5.3a)
2
⎛f ⎞
f c (max ) =
ft
2
− ⎜ t ⎟ + v2
⎝2⎠
kugRtaMgsgát;em (5.3b)
nig tan 2θ max =
v
ft / 2
Shear and Torsion Strength Design 216
6. NPIC
enAkñúgFñwmeRbkugRtaMg muxkat;esÞIrEtrgkugRtaMgsgát;TaMgGs;eRkamGMeBIbnÞúkeFVIkar (service
load). BIrUbTI 5>2 (c) nig (d) kugRtaMgemsMrab;Fatu A2 KW
f t (max ) = − c + ( f c / 2)2 + v 2
f
2
kugRtaMgTajem (5.4a)
f c (max ) = − c − ( f c / 2)2 + v 2
f
2
kugRtaMgsgát;em (5.4b)
nig tan 2θ max =
v
f /2 c
k> KMrU)ak;rbs;FñwmEdlKμanEdkTajGgát;RTUg
Modes of Failure of Beams without Diagonal Tension Reinforcement
pleFobElVgkat;elIkMBs; (slenderness ratio) rbs;FñwmkMNt;nUvKMrU)ak;rbs;Fñwm. rUbTI 5>5
bgðajBIkar)ak;sMrab;EdnkMNt;én slenderness ratio epSg². RbEvgElVgkMlaMgkat; (shear span) a
sMrab;bnÞúkcMcMnucCacMgayrvagcMnucénkarGnuvtþbnÞúk nigépÞénTMr. sMrab;bnÞúkBRgay shear span lc Ca
clear beam span. CaeKalkarN_ KMrUénkar)ak;manbIEbbKW kar)ak;edaykarbegáag (flexural failure),
kar)ak;edaykMlaMgTajGgát;RTUg (diagonal tension failure) nigkar)ak;edaybnSMkarkat; nigkarsgát;
(shear compression failure or web shear). Fñwmkan;EtRsav kareFVIkarrbs;vakan;EtxiteTArklkçN³
begáagdUckarerobrab;xageRkam.
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 219
11. T.Chhay
BIsmIkar 5.2 kugRtaMgkat;ÉktþasuT§ v enARtg;kMBs;Nak¾edayrbs;muxkat;KW
Vc Q
vc = (5.6)
Ib
karEbgEckkugRtaMgsréssgát; fc EdlbNþalBIm:Um:g;Bt;xageRkAKW
Pe Pe ec M T c
fc = − ± m (5.7)
Ac Ic Ic
ehIyBIsmIkar 5.4a kugRtaMgTajemKW
f 't = ( f c / 2)2 + vc2 − fc
(5.8)
2
k> Flexural-Shear Strength
edIm,IsikSaKNnasMrab;kMlaMgkat; eKcaM)ac;kMNt;faetI flexural shear b¤ web shear lubedIm,I
eFVIkareRCIserIsersIusþg;kat; Vc rbs;ebtug. sñameRbHeRTtEdlmanlMnwg (inclined stabilized crack)
enAcMgay d / 2 BI flexural crack EdlekItmanenAeBlrg first cracking load enAkñúgkrNI flexure
shear RtUv)anbgðajenAkñúgrUbTI 5>8. RbsinebI kMBs;RbsiT§PaBCa d p ¬kMBs;BIsréssgát;eTATIRbCMu
TMgn;rbs;EdkeRbkugRtaMgbeNþay¦ bMErbMrYlm:Um:g;rvagmuxkat; @ nig # KW
Vd p
M − M cr ≅ (5.9a)
2
b¤ V=
M cr
M /V − d p / 2
(5.9b)
Shear and Torsion Strength Design 224
12. NPIC
Edl V CakMlaMgkat;enARtg;muxkat;EdlBicarNa. lT§plénkarBiesFCaeRcInbgðajfaeKRtUvkar
kMlaMgkat;bBaÄrbEnßmEdlmanTMhM 0.6bwd p f 'c sMrab;xñat US nig bwd p f 'c / 20 sMrab;xñat SI
edIm,IeFVIeGaymansñameRbHeRTtenAkñúgrUbTI 5>8 eBjelj. dUcenH kMlaMgkat;bBaÄrsrubEdleFVIGMeBI
enARtg;bøg;elx @ rbs;rUbTI 5>8 KW
Vci =
M cr
M /V − d / 2
+ 0.6bw d p f 'c + Vd ¬xñat US¦ (5.10)
p
Vci =
M cr
M /V − d p / 2
+
bw d p f 'c
20
+ Vd ¬xñat SI¦
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 225
14. NPIC
Edl ersIusþg;sgát;rbs;ebtugEdlbNþalBIeRbkugRtaMgRbsiT§PaBeRkaykMhatbg;enARtg;
f ce =
srésxageRkAbMputrbs;muxkat;EdlkugRtaMgTajRtUv)anbgáeLIgedaybnÞúkxageRkA.
enARtg;TIRbCMuTMgn; fce = f c .
f d = kugRtaMgEdlbNþalBIbnÞúkGefrKμanemKuNenARtg;srésxageRkAbMputrbs;muxkat;Edl
bNþalEtBIbnÞúkpÞal;EdlkugRtaMgTajRtUv)anbgáedaybnÞúkxageRkA.
yt = cMgayBIG½kSTIRbCMuTMgn;eTAsrésrgkarTajxageRkA
ehIy M cr = EpñkxøHrbs;m:Um:g;énbnÞúkxageRkAEdlbgáeGaymansñameRbH. CakarsMrYl eKGacCMnYs
Sb CMnYseGay I c / yt .
rUbTI 5>9 bgðajBIdüaRkamrbs;smIkar 5.10 CamYynwgTinñn½yénkarBiesaF.
cMNaMfa eKeRbIkarsikSaKNnadUcKñaEdlGnuvtþsMrab;muxkat;cak;Rsab; sMrab;karsikSaKNna
kMlaMgkat;énmuxkat;smas. BIeRBaHkarsikSaKNnasMrab;kMlaMgkat;KWQrelIsßanPaBkMNt;edA
eBl)ak;eRkamGMeBIbnÞúkemKuN. eTaHbICa muxkat;TaMgmUlrbs;muxkat;smasTb;Tl;nwgkMlaMgkat;
smasdUcmuxkat;Edlcak;kñúgeBlEtmYy (monolithic section) k¾eday k¾karKNnaersIusþg;kMlaMg
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 227
15. T.Chhay
kat; Vc KYrQrelIlkçN³rbs;muxkat;cak;Rsab; edaysarersIusþg;kMlaMgkat;PaKeRcInpþl;eGayeday
RTnugrbs;muxkat;cak;Rsab;. dUcenH fce nig f d enAkñúgsmIkar 5.12 RtUv)anKNnaedayeRbIragFrNI
maRtrbs;muxkat;cak;Rsab;.
x> ersIusþg;kMlaMgkat;RTnug Web-Shear Strength
sñameRbHkMlaMgkat;RTnug (web-shear crack) enAkñúgFñwmeRbkugRtaMgekIteLIgedaysarkugRtaMg
EdlminGackMNt;)an (indeterminate stress) EdlCakarRbesIreKKYrKNnavaedaykugRtaMgTajemenA
Rtg;bøg;eRKaHfñak;BIsmIkar 5.8. eKGaccat;TukkugRtaMgkat; vc CakugRtaMgkat;RTnug vcw nigmantMél
GtibrmaenAEk,rTIRbCMuTMgn; cgc énmuxkat;EdlsñameRbHGgát;RTUgCak;EsþgekItman dUckarBiesaFeTA
dl;kar)ak;CaeRcIn)anbgðaj. RbsinebIeKCMnYs vc sMrab; vcw nig fc sMrab; f c ¬EdlCakugRtaMgeb-
tug fc EdlbNþalBIeRbkugRtaMgRbsiT§PaBenARtg;nIv:U cgc¦ enAkñúgsmIkar smIkarEdleGaykugRtaMg
TajemenAkñúgebtugesμInwgersIusþg;TajpÞal; (direct tensile strength) køayCa
( f c / 2) + vcw − f2c
f 't = 2
(5.13)
Edl vcw = Vcw / (bwd p ) CakugRtaMgkat;enAkñúgebtugEdlbNþalBIbnÞúkTaMgGs;EdleFVIeGayman
ersIusþg;kMlaMgkat;bBaÄrFmμta Vcw enAkñúgRTnug. edaHRsayrk vcw enAkñúgsmIkar 5.13
vcw = f 't 1 + f c / f 't (5.14a)
edayeRbI f 't = 3.5 f 'c psi(0.3 f 'c MPa) CatMéld¾smrmüsMrab;kugRtaMgTajedayQrelIlT§pl
énkarBiesaFCaeRcIn smIkar 5.14(a) køayCa
vcw = 3.5 f 'c ⎛ 1 + f c / 3.5 f 'c ⎞
⎜
⎝
⎟
⎠
¬xñat US¦ (5.14b)
vcw = 0.3 f 'c ⎛ 1 + f c / 0.3 f 'c ⎞
⎜
⎝
⎟
⎠
¬xñat SI¦
EdleyIgGacsMrYl)andUcxageRkam
vcw = 3.5 f 'c + 0.3 f c ¬xñat US¦ (5.14c)
vcw = 0.3( f 'c + f c ) ¬xñat SI¦
enAkñúg ACI Code eKeRbI f pc CMnYseGay f c . nimitþsBaØaEdleRbIenATIenHKWcg;bBa¢ak;favaCakugRtaMg
enAkñúgebtugminEmnenAkñúgEdkeRbkugRtaMgeT. ersIusþg;kMlaMgkat;Fmμta Vcw EdleGayedayebtugenA
eBlsñameRbHGgát;RTUgekItBIkugRtaMgTajemd¾FMenAkñúgRTnugkøayCa
Vcw = (3.5λ f 'c + 0.3 f c )bw d p + V p ¬xñat US¦ (5.15)
Shear and Torsion Strength Design 228
16. NPIC
( )
Vcw = 0.3 λ f 'c + f c bw d p + V p ¬xñat SI¦
Edl V p = bgÁúMbBaÄrénkMlaMgeRbkugRtaMgRbsiT§PaBenARtg;muxkat;BiessEdlcUlrYmnwgersIusþg;
FmμtabEnßm
λ = 1.0 sMrab;ebtugTMgn;Fmμta nigmantMéltUcCagenHsMrab;ebtugTMgn;Rsal
d p = cMgayBIsréssgát;xageRkAeTATMRbCMuTMng;rbs;EdkeRbkugRtaMg b¤ 0.8h edayykmYy
NaEdlFMCag
ACI Code yktMél f c CakugRtaMgsgát;pÁÜbrbs;ebtugenARt;gTIRbCMuTMgn;rbs;muxkat; b¤Rtg;
kEnøgEdlkat;KñarvagRTnug nigsøabenAeBlEdlTIRbCMuTMgn;sßitenAkñúgsøab. enAkñúgkrNImuxkat;smas
eKKNna f c edayQrelIkugRtaMgEdlekIteLIgedaykMlaMgeRbkugRtaMg nigm:Um:g;EdlTb;Tl;eday
Ggát;cak;Rsab;EdleFVIkarEtÉg. düaRkaménTMnak;TMngrvagkugRtaMgkat;RTnugFmμta (nominal web
shear stress) vcw nigkugRtaMgsgát;rbs;ebtugRtg;TIRbCMuTMgn;RtUv)aneGayenAkñúgrUbTI 5>10. cMNaMfa
PaBdUcKñarvagExSekagénsmIkar 5.14b nig c bgðajfasmIkar 5.14c RtUv)anEktMrUvBIsmIkar 5.14b
edIm,IeGaymanlkçN³bnÞat;. Code GnuBaØateGayeRbIemKuN 1.0 CMnYseGayemKuN 0.3 sMrab;tYTIBIr
énsmIkar 5.15.
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 229
17. T.Chhay
K> karRtYtBinitütMélrbs;V nigV sMrab;KNnaersIusþg;ebtugRTnugV
ci cw c
Controlling Values of Vci and Vcw for the Determination of the
Web Concrete Strength Vc
ACI Code mansmIkarbEnßmsMrab;kMNt;Vci nig Vcw edIm,IeRCIserIstMél Vc EdlRtUvkarenA
kñúgkarKNna³
(a) enAkñúgGgát;eRbkugRtaMgEdlmuxkat;enAcMgay h / 2 BIépÞénTMrenAEk,rcugénGgát;CagRbEvgepÞr
rbs;EdkeRbkugRtaMg enaHeKRtUvBicarNatMéleRbkugRtaMgkat;bnßyenAeBlKNna Vcw . tMél
Vcw enHRtUv)anKitCaEdlGtibrmarbs; Vc enAkñúgsmIkar
⎛ Vu d p ⎞
Vcw = ⎜ 0.6λ f 'c + 700
⎜ ⎟bw d p ≥ 2λ f 'c bw d p
⎝ Mu ⎟ ⎠
≤ 5λ f 'c bw d p ¬xñat US¦ (5.16)
⎛ Vu d p ⎞
Vcw = ⎜ 0.05λ f 'c + 5
⎜ ⎟bw d p ≥ 0.2λ f 'c bw d p
⎝ Mu ⎟ ⎠
≤ 0.4λ f 'c bw d p ¬xñat SI¦
tMél Vu d p / M u minGacFMCag 1.0 eT.
(b) enAkñúgGgát;eRbkugRtaMgEdl bonding rbs; tendon xøHmin)anBnøÚtdl;cugrbs;Ggát; enaHeKRtUv
KiteRbkugRtaMgkat;bnßyenAeBlkMNt; Vc edayeRbIsmIkar 5.16 b¤eRbItMéltUcCageKkñúg
cMeNamtMél Vc EdlTTYl)anBIsmIkar 5.11 nigBIsmIkar 5.15. dUcKña tMélrbs; Vcw Edl
KNnaedayeRbIeRbkugRtaMgkat;bnßyRtUvyktMélGtibrmaénsmIkar 5.16.
(c) eKGaceRbIsmIkar 5.16 kñúgkarkMNt; Vc sMrab;Ggát;EdlkMlaMgeRbkugRtaMgRbsiT§PaBmintUc
Cag 40% énersIusþg;Tajrbs;EdkrgkarBt; (flexural reinforcement) ebImindUcenaHeT luH
RtaEteKGnuvtþkarviPaKlMGitedayeRbIsmIkar 5.11 sMrab; Vci nigsmIkar 5.15 sMrab; Vcw
ehIyedayeRCIserIsyktMéltUcCageKéntMélTaMgBIrCatMélkMNt; Vc edIm,IeRbICaersIusþg;
rbs;RTnugkñúgkarKNnaEdkRTnug.
(d) bøg;dMbUgsMrab;ersuIsþg;kat;FmμtaEdlRtUvkarsrub (total required nominal shear strength)
Vn = Vu / φ EdlRtUv)aneRbIsMrab;KNnaEdkRTnugk¾sßitenARtg;cMgay h / 2 BIépÞrbs;TMr.
Shear and Torsion Strength Design 230
21. T.Chhay
Ts Ts V 1
= = s (5.18c)
s1 ns sin α d (cos α + cos β )
RbsinebIeKmanEdkkgeRTtcMnYn n Edlman analoguos truss chord RbEvg s1 ehIyRbsin
ebI Av CaRkLaépÞénEdkkgeRTtmYy enaH
Ts = nAv f y (5.19a)
dUcenH nAv =
Vs ns
d sin α (cot β + cot α ) f y
(5.19b)
b:uEnþGacsnμt;fa enAkñúgkrNI)ak;edaykMlaMgTajGgát;RTUg (diagonal tension failure) Ggát;RTUgrgkar
sgát;manmMu β = 45o dUcenHsmIkar 5.19b nwgkøayCa
Av f y d
Vs = [sin α (1 + cot α )]
s
Av f y d
b¤ Vs =
s
(sin α + cos α ) (5.20a)
edaHRsayrk s edayeRbI Vs = Vu − Vc
Av f y d
s= (sin α + cos α ) (5.20b)
Vu − Vc
RbsinebIEdkRTnugeRTtpÁúMeLIgedayEdkeTal b¤RkuménEdkeTalEdlEdkTaMgenARtUv)anBt; nigRtUv)an
dak;enAcMgaydUcKñaBIépÞénTMr enaH
Vs = Av f y sin α ≤ 3.0 f 'c bw d ¬xñat US¦
Vs = Av f y sin α ≤ 0.25 f 'c bw d ¬xñat SI¦
RbsinebIeKeRbIEdkkgbBaÄr mMu α nwgesμInwg 90o enaHeK)an
Av f y d
Vs = (5.21a)
s
Av f y dAvφf y d
b¤ s= =
(Vu / φ ) − Vc Vu − φVc
(5.21b)
enAkñúgsmIkar 5.21a nig b/ d p CacMgayBIsréssgát;xageRkAbMputeTAkan;TIRbCMuTMgn;rbs;EdkeRbkug
RtaMg ehIy d CacMgayBIsréssgát;xageRkAbMputeTATIRbCMuTMgn;rbs;EdkFmμta. tMélrbs; d p min
RtUvtUcCag 0.80h eT.
Shear and Torsion Strength Design 234
22. NPIC
K> EdlkMNt;énTMhM nigKMlatrbs;Edkkg
Limitation on Size and Spacing of Stirrups
smIkar 5.20 nig 5.21 eGaynUvTMnak;TMngRcasKñarvagKMlatEdkkg nigkMlaMgkat; b¤kugRtaMg
kat;EdlvaRtUvTb;Tl;. enAeBlEdl s fycuH (Vu − Vc ) nwgekIneLIg. edIm,IeGayEdkkgbBaÄrTb;Tl;
sñameRbHGgát;RTUg dUcbgðajenAkñúgrUbTI 5>11 (c) eKRtUvGnuvtþEdnkMNt;KMlatGtibrmasMrab;Edkkg
bBaÄrdUcxageRkam³
(a) smax ≤ 3 h ≤ 24in.(60cm) Edl h CakMBs;srubrbs;muxkat;
4
(b) RbsinebI Vs > 4λ f 'c bw d p ¬xñat US¦ Vs > λ f 'c bw d p / 3 ¬xñat SI¦ eKRtUvkat;
bnßyKMlatGtibrmarbs; (a) Bak;kNþal ¬ smax ≤ 83 h ≤ 12in.(30cm)
(c) RbsinebI Vs > 8λ f 'c bw d p ¬xñat US¦ Vs > 2λ f 'c bw d p / 3 ¬xñat SI¦
eKRtUvBRgIkmuxkat;.
(d) RbsinebI Vu = φVn > φVc / 2 / eKRtUvdak;EdkkMlaMgkat;Gb,brma. eKKNnaRkLaépÞ
EdkGb,brmaenHedaysmIkar
Av = 0.75 f 'c w
b s
f
b¤ Av = 50fbws edayykmYyNaEdlFMCag
y y
RbsinebIkMlaMgeRbkugRtaMgRbsiT§PaB Pe FMCag b¤esμInwg 40% énersIusþg;Tajrbs;EdkBt;
(flexural reinforcement) enaH
A ps f pu s dp
Av = (5.22b)
80 f y d bw
Edlvapþl;nUv Av Gb,brmaRtUvkartUcCag ehIyEdleKGaceRbIvaCMnYs)an.
(e) edIm,IRbsiT§PaB EdkRTnugRtUvEtmanRbEvgbgáb; (development lengt) RtUvkareBjelj.
enHmann½yfaEdkkgRtUvBnøÚtcUleTAkñúgEpñkrgkarsgát; nigEpñkrgkarTajrbs;muxkat;/
RtUvkarkMras;ebtugkarBarEdk (clear concrete cover) tUc nigeKGaceRbITMBk; 90o b¤
135o enAkñúgtMbn;sgát;.
rUbTI 5>13 bgðajBIdüaRkaménkardak;EdkkgRTnugeTAtamtMbn;énRbEvgElVgrbs;FñwmeRbkug
RtaMgEdlrgGMeBIénbnÞúkBRgayesμI. épÞqUtCakMlaMgkat;elIs Vs EdlRtUvkarEdkRTnug.
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 235
23. T.Chhay
7> ersIusþg;kMlaMgkat;edkenAkñúgeRKOgbgÁúMsmas
Horizontal Shear Strength in Composite Construction
snμt;fakMlaMgkat;tamTisedkepÞreBjeljRtg;épÞb:HénkEnøgEdlCYbKña.
k> eRkamGMeBIbnÞúkeFVIkar Service-Load Level
eKGackMNt;kugRtaMgkat;tamTisedkGtibrma vh BIeKalkarN_mUldæanrbs;emkanic
VQ
vh = (5.23)
I c bv
Edl V= kugRtaMgkat;KNnaKμanemKuN (unfactored design vertical shear) EdleFVIGMeBIelImux
kat;smas
Q = m:Um:g;RkLaépÞeFob cgc énkMNt;muxkat;EdlenABIxagelI b¤BIxageRkam cgc
I c = m:Um:g;niclPaBénmuxkat;smasTaMgmUl
bv = TTwgRtg;kEnøgb:Hrbs;muxkat;RTnugénGgát;cak;Rsab; b¤TTwgénmuxkat;EdleKKNna
kMlaMgkat;edk
Shear and Torsion Strength Design 236
24. NPIC
eKGacsMrYlsmIkar 5.23 dUcxageRkam
V
vh = (5.24)
bv d pc
Edl d pc CakMBs;RbsiT§PaBBIsréssgát;xageRkAénmuxkat;smaseTATIRbCMuTMgn; cgc rbs;EdkeRbkug
RtaMg.
x> Ultimate-Load Level
Direct Method: sMrab;kar)ak;enAkñúgsßanPaBkMNt; eKGacEkERbsmIkar 5.24 edayCMnYs V
eday Vu dUcenHeyIgTTYl)an
Vu
vuh = (5.25a)
bv d pc
b¤ sMrab;ersIusþg;kMlaMgkat;bBaÄrFmμta Vn
Vu / φ V
vnh = = n (5.25b)
bv d pc bv d pc
Edl φ = 0.75 / RbsinebI Vnh CaersIusþg;kMlaMgkat;edkFmμta enaH Vu ≤ Vnh ehIyersIusþg;kMlaMgkat;
FmμtasrubKW
Vnh = vnhbv d pc (5.25c)
ACI Code kMNt; vnh Rtwm 80 psi(0.55MPa ) RbsinebIeKmineRbIEdkEdkrgcaM (dowel) b¤EdkkgbBaÄr
ehIyépÞ b:HmanlkçN³eRKIm b¤RbsinebIeKeRbIEdkkgbBaÄrGb,brma b:uEnþépÞb:HminmanlkçN³eRKIm.
vnh GaceTAdl; 500 psi (3.45MPa ) EteKRtUveRbI friction theory CamYynwgkarsnμt;xageRkam
(a) enAeBlEdlminmanEdkkgbBaÄr b:uEnþépÞb:HénGgát;cak;Rsab;manlkçN³eRKIm
enaHeKeRbI
Vnh ≤ 80 Ac ≤ 80bv d pc (5.26a)
Edl Ac CaRkLaépÞrbs;ebtugEdlTb;Tl;kMlaMgkat; = bv d pc
(b) enAeBlEdleKeRbIEdkkgGb,brma Edl Ac = 50(bws ) / f y b:uEnþépÞb:Hrbs;Ggát;cak;
Rsab;minmanlkçN³eRKIm
vnh ≤ 80bv d pc
(c) RbsinebIépÞb:Hrbs;Ggát;cak;Rsab;manlkçN³eRKImEdlmankMBs; 1 / 4in.(6mm) ehIy
EdkbBaÄrGb,brmaenAkñúg (b) RtUv)andak; enaHeKeRbI
Vnh ≤ 500bv d pc (5.26b)
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 237
25. T.Chhay
(d) RbsinebIkMlaMgkat;emKuN Vu > φ (500bv d pc )/ eKGaceRbI shear friction theory edIm,I
KNnaEdk dowel. enAkñúgkrNIenH kMlaMgkat;edkTaMgGs;RtUv)anKitedaybøg;EkgEdl
Vnh = μAvf f y (5.27)
Edl Avf = RkLaépÞén shear-friction reinforcement/ in.2
f y = design yield strength/ minRtUvelIs 60,000 psi (414 MPa )
μ = emKuNkkit
= 1.0λ sMrab;ebtugEdlcak;elIépÞebtugEdlmaneRKIm
= 0.6λ sMrab;ebtugEdlcak;elIépÞebtugEdlminmaneRKIm
λ = emKuNsMrab;RbePTebtug
enAkñúgkrNITaMgGs; ersIusþg;kat;Fmμta Vn ≤ 0.20 f 'c Acc ≤ 800 Acc Edl Acc CaRkLaépÞb:Hrbs;
ebtugEdlTb;Tl;nwgkMlaMgkat;epÞr (shear transfer). cMNaMfa enAkñúgkrNICaeRcIn kugRtaMgkat; vuh
EdlTTYl)anBIkMlaMgkat;emKuNGt;FMCag 500 psi(3.45MPa ) eT. dUcenH eKmincaM)ac;RtUvkareRbIEt
shear friction theory kñúgkarKNnaEdkrgcaM (dowel) sMrab;skmμPaBsmas (composite action)
enaHeT.
KMlatGnuBaØatGtibrmaénEdkrgcaM (dowel) b¤ tie sMrab;kMlaMgkat;edkKWtMéltUcCageKkñúg
cMeNam 4 dgénTMhMtUcCageKénmuxkat;TMr nig 24in.(60cm) .
Basic Method: ACI Code GnuBaØateGayeRbIviFIepSgeTotEdlkMlaMgkat;edkRtUv)anGegát
edayKNnabMErbMrYlCak;EsþgénkMlaMgsgát; b¤kMlaMgTajenAkñúgbøg;NamYy nigedayepþrkMlaMgkat;edk
enaHeTAGgát;EdlCaTMr. eKCMnYsRkLaépÞb:H Acc sMrab; bv d pc enAkñúgsmIkar 5.25b nig c enaHeK
TTYl)an
Vnh = vnh Acc (5.28)
Edl Vnh ≥ Fh / kMlaMgkat;edk ehIyy:agehacNas;vaRtUvesμInwgkMlaMgsgát; C b¤kMlaMgTaj T enA
kñúgrUbTI 5>14. ¬emIlsmIkar 5.30 sMrab;tMélrbs; Fh ¦
eKGackMNt;RkLaépÞb:H Acc dUcxageRkam
Acc = bv lvh (5.29)
Edl lvh CaRbEvgkMlaMgkat;edk (horizontal shear length) EdlkMNt;enAkñúgrUbTI 5.15(a) nig (b)
sMrab;Ggát;TMrsamBaØ nigsMrab;Ggát;TMrCab; erogKña.
Shear and Torsion Strength Design 238
27. T.Chhay
K> karKNnaEdkrgcaMskmμsmas
Design of Composite-Action Dowel Reinforcement
Edk tie sMrab;kMlaMgkat;edkGacpSMeLIgBIr)arEdkeTal (single bars or wires)/ BIEdkkgeCIg
eRcIn (multiple leg stirrup) b¤BI vertical legs of welded wire fabric. KMlatrbs;vaminGacFMCagbYn
dgénTMhMEdltUcCageKénGgát;TMr b¤ 24in.(60cm) edayykmYyNaEdltUcCageK. RbsinebI μ Ca
emKuNkMlaMgkkit enaHeKGackMNt;kMlaMgkat;edkFmμta Fh enAkñúgrUbTI 5>14 dUcxageRkam
Fh = μAvf f y ≤ Vnh (5.30)
tMél ACI rbs; μ KWQrelIersIusþg;kkit-kMlaMgkat;kMNt; (limit shear-friction strength) 800 psi
(5.5MPa ) ¬vaCatMélEdlmanlkçN³suvtßiPaBbnþicEdlbgðajedaykarBiesaF¦. viTüasßanebtugeRb
kugRtaMg (Prestressed Concrete Institute) ENnaM μe = 2.9 CMnYseGay μ = 1.0λ sMrab;ebtug
Edlcak;elIépÞebtugeRKIm ehIykMlaMgkat;KNnaGtibrma (maximum design shear force)
Vu ≤ 0.25λ2 f 'c Ac ≤ 1,000λ2 Acc (5.31a)
CamYynwgRkLaépÞcM)ac;rbs;Edkkkit-kMlaMgkat; (shear-friction steel)
Vuh
Avf = (5.31b)
φf y μ e
b¤ Avh =
Vnh F
= h
μe f y μe f y
(5.31c)
edayeRbItMél PCI EdlminsUvsuvtßiPaB smIkar 5.31c køayCa
Fh ≤ μ e Avf f y ≤ Vnh (5.32)
λ 2
CamYynwg μe = 1,000F bv I vh ≤ 2.9
h
Edl bvlvh = Acc / EdkGb,brmaKW
50bv s 50bv lvh
Av = = (5.33)
fy fy
8> CMhanKNnaEdkRTnugsMrab;kMlaMgkat;
Web Reinforcement Design Procedure for Shear
xageRkamCakarsegçbBICMhanénkarKNnaEdkRTnugsMrab;kMlaMgkat;³
!> kMNt;tMélersIusþg;kMlaMgkat;FmμtaEdlRtUvkar Vn = Vu / φ enARtg;cMgay h / 2 BIépÞénTMr Edl
φ = 0.75 .
Shear and Torsion Strength Design 240
28. NPIC
@> KNnaersIusþg;kMlaMgkat;Fmμta (nominal shear strength) Vc EdlRTnugmanedayeRbIviFImYy
kñúgcMeNamviFIBIrxageRkam³
(a) ACI conservative method RbsinebI f pe > 0.40 f pu
⎛ 700Vu d p ⎞
Vc = ⎜ 0.60λ f 'c +
⎜ ⎟bw d p ¬xñat US¦
⎟
⎝ M u ⎠
⎛ λ f 'c V d⎞
Vc = ⎜
⎜ 20
+ 5 u ⎟bw d p
Mu ⎟
¬xñat SI¦
⎝ ⎠
Edl 2λ f 'c bw d p ≤ Vc ≤ 5λ f 'c bw d p sMrab;xñat US
λ f 'c bw d p / 5 ≤ Vc ≤ 0.4λ f 'c bw d p sMrab;xñat SI
Vu d p
≤ 1.0
Mu
ehIyeKKNna Vu enARtg;muxkat;dUcKñasMrab;karKNna M u .
RbsinebIersIusþg;eRcokTajmFüm (average tensile splitting strength) fct sMrab;
ebtugTMgn;Rsal enaH λ = fct / 6.7 f 'c sMrab;xñat US b¤ λ = fct / 0.556 f 'c
sMrab;xñat SI CamYynwg f 'c Gt;FMCag 100 psi(0.67MPa ) .
(b) Detailed analysis Edl Vc CatMéltUcCageKkñúgcMeNam Vci nig Vcw
¬xñat US¦ 1.7λ f 'c bw d p ≤ Vci = 0.60λ f 'c bw d p + Vd +
Vi
M max
(M cr ) ≤ 5.0λ f 'c bwd p
λ f 'c bw d p λ f 'c bw d p
¬xñat SI¦ 7
≤ Vci =
20
+ Vd +
Vi
M max
(M cr ) ≤ 0.4λ f 'c bwd p
¬xñat US¦ ( )
Vcw = 3.5λ f 'c + 0.3 f c bw d p + V p
¬xñat SI¦ ( )
Vcw = 0.3 λ f 'c + f c bw d p + V p
edayeRbItMélNaEdlFMCageKkñúgcMeNam d p nig 0.8h
Edl M cr = (I c / yt )(6λ f 'c + fce − f d ) ¬xñat US¦
M cr = (I c / yt )(0.5λ f 'c + f ce − f d ) ¬xñat SI¦
b¤ M cr = Sb (6λ f 'c + fce − f d ) ¬xñat US¦
M cr = Sb (0.5λ f 'c + f ce − f d ) ¬xñat SI¦
Vi = kMlaMgkat;emKuNEdlbNþalBIbnÞúkGnuvtþn_BIxageRkAEdlekItmankñúg
eBldMNalKñaCamYynwg M max
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 241
29. T.Chhay
kugRtaMgsgát;enAkñúgebtugeRkayekItmankMhatbg;TaMgGs;enARtg;
f ce =
srésxageRkArbs;muxkat;EdlbnÞúkxageRkAbgáeGaymankugRtaMgTaj.
f ce køayCa f c sMrab;kugRtaMgenARtg;TIRbCMuTMgn;rbs;muxkat;.
#> RbsinebI Vu / φ ≤ Vc / 2 vaminRtUvkarEdkRTnugeT. RbsinebI Vc / 2 < Vu / φ < Vc vaRtUvkar
EdkGb,brma. RbsinebI Vu / φ > Vc nig
RbsinebI Vs = Vu / φ − Vc ≤ 8λ f 'c bw d p ¬xñat US¦
Vs = Vu / φ − Vc ≤ 2λ f 'c bw d p / 3 ¬xñat SI¦
eKRtUvKNnaEdkRTnug.
RbsinebI Vs = Vu / φ − Vc > 8λ f 'c bw d p b¤ Vs > φ (Vc + 8λ f 'c bw d p ) ¬xñat US¦
Vs = Vu / φ − Vc > 2λ f 'c bw d p / 3 ¬xñat SI¦
eKRtUvtMeLIgmuxkat;.
$> KNnaEdkRTnugGb,brmaEdlRtUvkar. KMlatKW s ≤ 0.75h b¤ 24in.(60cm) edayykmYyNa
EdltUcCageK.
Av min = 0.75 f 'c w b¤ Av min = ¬US¦ edayykmYyNaEdlFMCag
b s 50bw s
f y f y
Av min = f 'c
bw s
16 f y
b¤ Av min = 50fbws ¬SI¦ edayykmYyNaEdlFMCag
y
RbsinebI /
f pe ≥ 0.40 f pu Av min EdlmanlkçN³suvtßiPaBticCagCatMéltUcCageKkñúg
cMeNam
A ps f pu s dp
Av =
80 f y d p bw
Edl d p ≥ 0.80h
CamYynwg Av min = 0.75 f 'c
bw s
fy
b¤ Av min = 50fbws ¬US¦
y
Av min = f 'c
bw s
16 f y
b¤ Av min = 50fbws ¬SI¦
y
%> KNnaTMhM nigKMlatEdkRTnugEdlRtUvkar. RbsinebI
¬xñat US¦
Vs = (Vu / φ − Vc ) ≤ 4λ f 'c bw d p
Vs = Vu / φ − Vc ≤ λ f 'c bw d p / 3 ¬xñat SI¦
enaHKMlatEdkkg s EdlRtUvkarKWesμInwgtMélEdlKNnaedaysmIkarEdleGayenAkñúgCMhan ^.
Shear and Torsion Strength Design 242
30. NPIC
EtRbsinebI
¬xñat US¦
Vs = (Vu / φ − Vc ) > 4λ f 'c bw d p
Vs = Vu / φ − Vc > λ f 'c bw d p / 3 ¬xñat SI¦
enaHKMlatEdkkg s EdlRtUvkarKWesμInwgBak;kNþaléntMélEdlKNnaedaysmIkarEdleGay
enAkñúgCMhan ^.
^> s = (VAvφf)y− V = VAv −yφdVp ≤ 0.75h ≤ 24in.(60cm) ≥ s Gb,brmaEdl)anBICMhan $
dp f
u c u c
&> sg; shear envelope enAelIElVgFñwm nigKUsbBa¢ak;tMbn;EdlRtUvkarEdkRTnug
*> KUrBRgayEdkRTnugtambeNþayElVgedayeRbIEdkkgTMhM #3 b¤ #4 tamEdlcUlcitþ b:uEnþEdk
kgminRtUvmanTMhMFMCag #6 eT.
(> KNnaEdkrgcaM (dowel reinforcement) bBaÄrkñúgkrNImuxkat;smas
(a) Vnh ≤ 80bv d pc sMrab;TaMgépÞb:HeRKImedayKμanEdkrgcaM b¤Edk tie bBaÄr nigsMrab;TaMgépÞb:H
EdlmineRKImb:uEnþeRbIEdk tie bBaÄrGb,brma. eRbI
50bw s 50bv I vh
Av = =
fy fy
(b) Vnh ≤ 500bw d pcsMrab;épÞeRKImEdlmanecjk,alfμkMBs; 1 / 4in.(6mm)
(c) sMrab;krNIEdl Vnh > 500bw d pc / KNnaEdk tie bBaÄrsMrab; Vnh = Avf f y μ
Edl Avf = RkLaépÞrbs;EdkrgcaMEdlmanlkçN³kkit (frictional steel dowel)
μ = emKuNkkit = 1.0λ sMrab;épÞEdlmanlkçN³eRKIm Edl λ = 1.0 sMrab;
ebtugTMgn;Fmμta. sMrab;RKb;krNITaMgGs; Vn ≤ Vnh ≤ 0.2 f 'c Acc
≤ 800 Acc Edl Acc = bv lvh .
viFIepSgeToténkarKNnaRkLaépÞEdkrgcaM Avf KWedayKNnakMlaMgedk Fh enARtg;épÞkkit
rbs;ebtugEdl
Fh ≤ μ e Avf f y ≤ Vnh
1,000λ2bv lvh
Edl μe =
Fh
≤ 2.9
rUbTI 5>16 bgðajBICMhanKNnaEdl)anerobrab;xagelICaTMrg; flowchart.
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 243
39. T.Chhay
bw = 6in.(15cm )
ec = 15in.(38cm )
ee = 12.5in.(32cm )
(
I c = 70,700in.4 18.09 × 106 cm 4 )
(
Ac = 377in.2 2,432cm 2 )
(
r 2 = 187.5in.2 1,210cm 2 )
cb = 18.84in.(48cm )
ct = 21.16in.(54cm )
Pe = 308,255lb(1.371kN )
bnÞúkemKuN Wu = 1.2D + 1.6L
= 1.2(100 + 393) + 1.6 × 1,100 = 2,352 plf
kMlaMgkat;enARtg;épÞTMr Vu = Wu L / 2
= (2,352 × 65) / 2 = 76,440lb
Vn tMrUvkar = Vu / φ = 76,440 / 0.75 = 101,920lb enARtg;TMr
bøg;enARtg; 12 d p BIépÞénTMr
!> ersIusþg;kMlaMgkat;Fmμta (nominal shear strength) Vc rbs;RTnug ¬CMhanTI2 nigTI3¦
1 36.16
dp = ≅ 1.5 ft
2 2 × 12
Vn = 101,920 ×
[(65 / 2) − 1.5] = 97,216lb
65 / 2
Vu enARtg;1
2
d p = 0.75 × 97,216 = 72,912lb
f pe = 155,000 psi
0.40 f pu = 0.40 × 270,000 = 108,000 psi (745MPa )
< f pe = 155,000 psi (1,069 MPa )
eRbI ACI alternate method
edaysar d p > 0.8h / eRbI d p = 36.16in. edaysnμt;faEdkeRbkugRtaMgxøHRtg;rhUtdl;TMr.
BIsmIkar 5.16
Shear and Torsion Strength Design 252
40. NPIC
⎛ Vu d p ⎞
Vc = ⎜ 0.60λ f 'c + 700
⎜ ⎟bw d p ≥ 2λ f 'c bw d p ≤ 5λ f 'c bw d p
⎝ Mu ⎟ ⎠
λ = 1 .0sMrab;ebtugTMgn;Rsal
Wu (1.5)2
M u enARtg; d / 2 BIépÞ = Rbtikmμ × 1.5 −
2
2,352(1.5)2
= 76,440 × 1.5 − = 112,014 ft − lb
2
= 1,344,168in. − lb
Vu d p 72,912 × 36.16
= = 1.96 > 1.0
Mu 1,344,168
dUcenHeRbI Vu d p / M u = 1.0 enaH
Vc Gb,brma = 2λ f 'c bw d p = 2 × 1.0 5,000 × 6 × 36.16 = 30,683lb
Vc Gtibrma = 5λ f 'c bw d p = 76,707lb(341kN )
Vc = (0.60 × 1.0 5,000 + 700 × 1.0 )6 × 36.16
= 161,077lb > Vc Gtibrma = 76,707lb
bnÞab;mk Vc = 76,707lb / lub. dUcKña Vu / φ > Vc / 2 dUcenH eKRtUvkarEdkRTnug.
Vu
Vs = − Vc = 97,216 − 76,707 = 20,509lb
φ
8λ f 'c bw d p = 8 × 1.0 5,000 × 6 × 36.16 = 122,713lb(546kN )
> Vs = 20,509lb
dUcenHkMBs;rbs;muxkat;RKb;RKan;.
@> EdkRTnugGb,brma ¬CMhanTI4¦
BIsmIkar 5.22b
Av
s
Gb,brma = 80psf fdpu d p
A
b y p w
1.99 × 270,000 36.16
= = 0.0076in.2 / in.
80 × 60,000 × 36.16 6
#> EdkRTnugtMrUvkar ¬CMhanTI5 nigTI6¦
BIsmIkar 5.21b
Av f y d p
s= ≤ 0.75h ≤ 24in.
Vu / φ − Vc
b¤ Av
s
V
= s =
20,509
f y d p 60,000 × 36.16
= 0.0095in.2 / in.
karKNnaersIusþg;kMlaMgkat; nigersIusþg;kMlaMgrmYl 253