32
Design Assumption 1. All the designs comply with COP Structure Use of Concrete 2004 Cl 7.3.5 2. Elastic stress box is adopted 3. Section is assumed to be plane remaining plane 4. Concrete tensile stress for short term and long term are 1 N/mm2 and 0.55 N/mm2 5. For uncrack section, the I includes the stiffness of rebar Notes 1.Don’t move any cells 2. Don't change the name of cells 3. Don't change the name of worksheet 4. This entire workbook only serves for one beam.

3.00 Deflection Rev 0 8HB10

Embed Size (px)

DESCRIPTION

3.00 Deflection Rev 0 8HB10

Citation preview

Design AssumptionDesign Assumption1. All the designs comply with COP Structure Use of Concrete 2004 Cl 7.3.52. Elastic stress box is adopted3. Section is assumed to be plane remaining plane4. Concrete tensile stress for short term and long term are 1 N/mm2 and 0.55 N/mm2 respectively5. For uncrack section, the I includes the stiffness of rebarNotes1.Dont move any cells2. Don't change the name of cells3. Don't change the name of worksheet4. This entire workbook only serves for one beam.

xpsHyder Consulting LimitedBy :Job No.Job :Date :SheetSubject :Check x for short term permanent loadMp=4017kN*mH=2300mmb=1000mmd=2240mmdc=30mmAst=12560mm^2Asc=2010mm^2Es=205000N/mm^2Ecs=26400N/mm^2ftd=0.55N/mm^2fct=(H-xps)/(d-xps)*ftd=0.5705543315fst=(M-(fct*b*(H-xps)*(H/3)))/((Ast*(d-xps/3))+(((xps-dc)/(d-xps))*(Ec/Es)*(xps/3-dc)*Asc))=128.9815245368fsc=((xps-dc)/(d-xps))*(Ec/Es)*fst=6.25fc1=xps/(d-xps)*(Ec/Es)*fst=6.56fc2=(fst*Ast+(1/2*fct*b*(H-xps))-(fsc*Asc))/(1/2*b*xps)=6.56fc1-fc2 =-0.00xps=634.50mmChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xtsChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xts

xtsHyder Consulting LimitedBy :Job No.Job :Date :SheetSubject :Check x for short term temporary loadMt=6735kN*mH=2300mmb=1000mmd=2240mmdc=30mmAst=12560mm^2Asc=2010mm^2Es=205000N/mm^2Ecs=26400N/mm^2ftd=0.55N/mm^2fct=(H-xts)/(d-xts)*ftd=0.5702086836fst=(M-(fct*b*(H-xts)*(H/3)))/((Ast*(d-xts/3))+(((xts-dc)/(d-xts))*(Ec/Es)*(xts/3-dc)*Asc))=234.0964568866fsc=((xts-dc)/(d-xts))*(Ec/Es)*fst=10.65fc1=xts/(d-xts)*(Ec/Es)*fst=11.21fc2=(fst*Ast+(1/2*fct*b*(H-xts))-(fsc*Asc))/(1/2*b*xts)=11.21fc1-fc2 =-0.00xts=607.04mmChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xtsChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xts

xplHyder Consulting LimitedBy :Job No.Job :Date :SheetSubject :Check x for Long term permanent loadMp=4017kN*mH=2300mmb=1000mmd=2240mmdc=30mmAst=12560mm^2Asc=2010mm^2Es=205000N/mm^2Ecl=15161N/mm^2ftd=1N/mm^2fct=(H-xpl)/(d-xpl)*ftd=1.043054378fst=(Mp-(fct*b*(H-xpl)*(H/3)))/((Ast*(d-xpl/3))+(((xpl-dc)/(d-xpl))*(Ecl/Es)*(xpls/3-dc)*Asc))=115.9808764555fsc=((xpl-dc)/(d-xpl))*(Ecl/Es)*fst=5.02fc1=xpl/(d-xpl)*(Ec/Es)*fst=5.21fc2=(fst*Ast+(1/2*fct*b*(H-xpl))-(fsc*Asc))/(1/2*b*xpl)=5.21fc1-fc2 =-0.00xpl=846.41mmChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xtsChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xts

creep coeff & shrinkage strainHyder Consulting LimitedBy :Job No.Job :Date :SheetSubject :KLc=2.3Fig 3.1Km=1.0Fig 3.2Kc=0.8Fig 3.3Kec=0.7Fig 3.4Kj=0.6Fig 3.5Ks=1/(1+r*ae)=0.96modular ratio (r)=Es/Ecs=7.77steel ratio (ae)=As/Ac=Ast/(b*H)=0.005cs=3.0KLs=275.0x10^-6Fig 3.6Kes=0.5Fig 3.7creep coefficient (fc)=KLc*Km*Kc*Kec*Kj*Ks=0.74free shrinkage strain (ecs)=cs*KLs*10^-6*Kc*Kes*Kj=1.98E-04Checked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xtsChecked byFileRef.K:\EB000376 City U 334 Phase 3 (Academic and Admin Bldg)\D-Calcs\4th Submission(Superstructure)\Deflection Check\[Deflection_rev_0_8HB10.xls]xts

DEFLECTIONHyder Consulting LimitedBy :KWJob No.EB000376Job :CityU 334 Phrase 3 (AAB)Date :May-10SheetSubject :8HB10Beam Deflection CheckingCONCRETE GRADEElastic Modulus Ec (N/mm^2)Complying with COP Structure Use of Concrete 2004 Cl 7.3.5C2018700PARAMETERSC2520500C3022200Total Moment (Mt)=6735kN*mBasic CheckingC3523700Permanent Moment (Mp)=4017kN*mConcrete Compressive stressC4025100def=11mmfcts11.21C4526400H=2300mmL/250=48mmfcps6.56C5027700b=1000mmfcpl5.21C5528900d=2240mmDeflectionSectionC6030000dc=30mmShort term total9.869(cracked)C6531100Ast=12560mm^2Short term perm5.530(cracked)C7032200Asc=2010mm^2Long term perm5.729(cracked)C7533200Effective span (l)=12000mmShrinkage0.699C8034200Second moment of area (I)=1031360546666.67mm^4I is considered rebar = H^3*b/12+Ast*(H/2-d)^2+Asc*(H/2-dc)^2C8535100C9036000Concrete Grade=C45C9536900Short-term modulus of concrete (Ecs)=26400N/mm^2Cl. 7.1.5C10037800KLc=2.3Fig 3.1Km=1.0Fig 3.2Kc=0.8Fig 3.3Kec=0.7Fig 3.4Kj=0.6Fig 3.5Creep coefficient (fc)=0.74Cl. 3.1.7Long-term modulus of concrete (Ecl)=15160.54N/mm^2Modulus of elasticity of reinforcement (Es)=205000N/mm^2cs=3.0KLs=275.0x10^-6Fig 3.6Kes=0.5Fig 3.7Free shrinkage strain (ecs)=1.98E-04ro=0.56Table 7.7K=0.098Table 7.6Total short term fcts=11.21N/mm^2Permanent short term fcps=6.56N/mm^2Permanent long term fcpl=5.21N/mm^2Total short term cracked xts=607.04mmPermanent short term cracked xps=634.50mmPermanent long term cracked xpl=846.41mmCURVATURE1) Instantaneous Curvature under Total Loada) Cracked Section (Partially)1/rb=fcts/(xts*Ecs)=11.2068950362/(607.038609514431x26400)=6.99E-07mm^-1b) Uncracked Section1/rb=Mt/(Ecs*I)=6735x1000^2/(26400x1031360546666.67)=2.47E-07mm^-11/rb (cracked)=6.99E-07mm^-1>=1/rb (uncracked)=2.47E-07mm^-11/rb=6.99E-07mm^-1(cracked)(1)2) Instantaneous Curvature under Permanent Loada) Cracked Section (Partially)1/rb=fcps/(xps*Ecs)=6.5644436389/(634.498990187979x26400)=3.92E-07mm^-1b) Uncracked Section1/rb=Mp/(Ecs*I)=4017x1000^2/(26400x1031360546666.67)=1.48E-07mm^-11/rb (cracked)=3.92E-07mm^-1>=1/rb (uncracked)=1.48E-07mm^-11/rb=3.92E-07mm^-1(cracked)(2)3) Long-term Curvature Under Permanent Loada) Cracked Section (Partially)1/rb=fcpl/(xpl*Ecl)=5.2094972962/(846.41349926246x15160.5389753453)=4.06E-07mm^-1b) Uncracked Section1/rb=Mp/(Ecl*I)=4017x1000^2/(15160.5389753453x1031360546666.67)=2.57E-07mm^-11/rb (cracked)=4.06E-07mm^-1>=1/rb (uncracked)=2.57E-07mm^-11/rb=4.06E-07mm^-1(cracked)(3)4) Shrinkage Curvature1/rcs=ro*ecs/d=0.56x1.98E-04/2240=4.95E-08mm^-1(4)Total Long-term Curvature1/rtotal=(3) + (1) - (2) + (4)=4.06E-07+6.99E-07-3.92E-07+4.95E-08=7.63E-07mm^-1DEFLECTIONa=K*L^2(1/rtotal)=0.098x12000^2x7.63E-07=11mm