03 300x300x118 Beam
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7/23/2019 03 300x300x118 Beam http://slidepdf.com/reader/full/03-300x300x118-beam 1/4 Autodesk Robot Structural Analysis Professional 2013 Author: WBB File: Address: Harvest Consulting Engineers LLP Project: Structure Date : 14/12/15 Page : 1 STEEL DESIGN ---------------------------------------------------------------------------------------------------------------------------------------- CODE: BS-EN 1993-1:2005/NA:2008/AC:2009, Eurocode 3: Design of steel structures. ANALYSIS TYPE: Member Verification ---------------------------------------------------------------------------------------------------------------------------------------- CODE GROUP: MEMBER: 7 Beam_7 POINT: 3 COORDINATE: x = 1.00 L = 2.85 m ---------------------------------------------------------------------------------------------------------------------------------------- LOADS: Governing Load Case: 9 ULS:STD/1=1*1.35 + 2*1.50 1*1.35+2*1.50 ---------------------------------------------------------------------------------------------------------------------------------------- MATERIAL: S275 ( S275 ) fy = 275.000 MPa ---------------------------------------------------------------------------------------------------------------------------------------- SECTION PARAMETERS: UC 305x305x118 h=315 mm gM0=1.00 gM1=1.00 b=307 mm Ay=12040 mm2 Az=4296 mm2 Ax=15000 mm2 tw=12 mm Iy=276700000 mm4 Iz=90590000 mm4 Ix=1610000 mm4 tf=19 mm Wply=1958000 mm3 Wplz=895000 mm3 ---------------------------------------------------------------------------------------------------------------------------------------- INTERNAL FORCES AND CAPACITIES: N,Ed = 30.676 kN My,Ed = -55.646 kN*m Mz,Ed = 0.000 kN*m Vy,Ed = -0.000 kN Nc,Rd = 4125.000 kN My,pl,Rd = 538.450 kN*m Mz,pl,Rd = 246.125 kN*m Vy,T,Rd = 1911.508 kN Nb,Rd = 4125.000 kN My,c,Rd = 538.450 kN*m Mz,c,Rd = 246.125 kN*m Vz,Ed = -50.541 kN MN,y,Rd = 538.450 kN*m MN,z,Rd = 246.125 kN*m Vz,T,Rd = 682.093 kN Mb,Rd = 538.450 kN*m Tt,Ed = -0.001 kN*m Class of section = 1 ---------------------------------------------------------------------------------------------------------------------------------------- LATERAL BUCKLING PARAMETERS: z = 1.00 Mcr = 2775.924 kN*m Curve,LT - b XLT = 0.98 Lcr,low=2.85 m Lam_LT = 0.44 fi,LT = 0.58 XLT,mod = 1.00 ---------------------------------------------------------------------------------------------------------------------------------------- BUCKLING PARAMETERS: About y axis: About z axis: kyy = 1.00 kzz = 1.00 ---------------------------------------------------------------------------------------------------------------------------------------- VERIFICATION FORMULAS: Section strength check: N,Ed/Nc,Rd = 0.01 < 1.00 (6.2.4.(1)) (My,Ed/MN,y,Rd)^ 2.00 + (Mz,Ed/MN,z,Rd)^1.00 = 0.01 < 1.00 (6.2.9.1.(6)) Vy,Ed/Vy,T,Rd = 0.00 < 1.00 (6.2.6-7) Vz,Ed/Vz,T,Rd = 0.07 < 1.00 (6.2.6-7) Tau,ty,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6) Tau,tz,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6) Global stability check of member: My,Ed/Mb,Rd = 0.10 < 1.00 (6.3.2.1.(1)) N,Ed/(Xy*N,Rk/gM1) + kyy*My,Ed/(XLT*My,Rk/gM1) + kyz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4)) N,Ed/(Xz*N,Rk/gM1) + kzy*My,Ed/(XLT*My,Rk/gM1) + kzz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4)) ---------------------------------------------------------------------------------------------------------------------------------------- Section OK !!! STEEL DESIGN
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Transcript of 03 300x300x118 Beam
7/23/2019 03 300x300x118 Beam
http://slidepdf.com/reader/full/03-300x300x118-beam 1/4
Autodesk Robot Structural Analysis Professional 2013 Author: WBB File: Address: Harvest Consulting Engineers LLP Project: Structure
Date : 14/12/15 Page : 1
STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------
CODE: BS-EN 1993-1:2005/NA:2008/AC:2009, Eurocode 3: Design of steel structures.
ANALYSIS TYPE: Member Verification----------------------------------------------------------------------------------------------------------------------------------------CODE GROUP:
MEMBER: 7 Beam_7 POINT: 3 COORDINATE: x = 1.00 L = 2.85m----------------------------------------------------------------------------------------------------------------------------------------
LOADS:
Governing Load Case: 9 ULS:STD/1=1*1.35 + 2*1.50 1*1.35+2*1.50----------------------------------------------------------------------------------------------------------------------------------------
MATERIAL:
S275 ( S275 ) fy = 275.000 MPa----------------------------------------------------------------------------------------------------------------------------------------
SECTION PARAMETERS: UC 305x305x118
h=315 mm gM0=1.00 gM1=1.00 b=307 mm Ay=12040 mm2 Az=4296 mm2 Ax=15000 mm2tw=12 mm Iy=276700000 mm4 Iz=90590000 mm4 Ix=1610000 mm4tf=19 mm Wply=1958000 mm3 Wplz=895000 mm3----------------------------------------------------------------------------------------------------------------------------------------
INTERNAL FORCES AND CAPACITIES:
N,Ed = 30.676 kN My,Ed = -55.646 kN*m Mz,Ed = 0.000 kN*m Vy,Ed = -0.000 kN Nc,Rd = 4125.000 kN My,pl,Rd = 538.450 kN*m Mz,pl,Rd = 246.125 kN*m Vy,T,Rd = 1911.508 kN Nb,Rd = 4125.000 kN My,c,Rd = 538.450 kN*m Mz,c,Rd = 246.125 kN*m Vz,Ed = -50.541 kN MN,y,Rd = 538.450 kN*m MN,z,Rd = 246.125 kN*m Vz,T,Rd = 682.093 kN
Mb,Rd = 538.450 kN*m Tt,Ed = -0.001 kN*mClass of section = 1
----------------------------------------------------------------------------------------------------------------------------------------
LATERAL BUCKLING PARAMETERS: z = 1.00 Mcr = 2775.924 kN*m Curve,LT - b XLT = 0.98Lcr,low=2.85 m Lam_LT = 0.44 fi,LT = 0.58 XLT,mod = 1.00----------------------------------------------------------------------------------------------------------------------------------------
BUCKLING PARAMETERS:
About y axis: About z axis: kyy = 1.00 kzz = 1.00
----------------------------------------------------------------------------------------------------------------------------------------VERIFICATION FORMULAS: Section strength check:
N,Ed/Nc,Rd = 0.01 < 1.00 (6.2.4.(1))(My,Ed/MN,y,Rd)^ 2.00 + (Mz,Ed/MN,z,Rd)^1.00 = 0.01 < 1.00 (6.2.9.1.(6))Vy,Ed/Vy,T,Rd = 0.00 < 1.00 (6.2.6-7)Vz,Ed/Vz,T,Rd = 0.07 < 1.00 (6.2.6-7)Tau,ty,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Tau,tz,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Global stability check of member:My,Ed/Mb,Rd = 0.10 < 1.00 (6.3.2.1.(1)) N,Ed/(Xy*N,Rk/gM1) + kyy*My,Ed/(XLT*My,Rk/gM1) + kyz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4)) N,Ed/(Xz*N,Rk/gM1) + kzy*My,Ed/(XLT*My,Rk/gM1) + kzz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4))----------------------------------------------------------------------------------------------------------------------------------------
Section OK !!!
STEEL DESIGN
7/23/2019 03 300x300x118 Beam
http://slidepdf.com/reader/full/03-300x300x118-beam 2/4
Autodesk Robot Structural Analysis Professional 2013 Author: WBB File: Address: Harvest Consulting Engineers LLP Project: Structure
Date : 14/12/15 Page : 2
----------------------------------------------------------------------------------------------------------------------------------------
CODE: BS-EN 1993-1:2005/NA:2008/AC:2009, Eurocode 3: Design of steel structures.ANALYSIS TYPE: Member Verification----------------------------------------------------------------------------------------------------------------------------------------
CODE GROUP: MEMBER: 8 Beam_8 POINT: 1 COORDINATE: x = 0.00 L = 0.00m----------------------------------------------------------------------------------------------------------------------------------------
LOADS:
Governing Load Case: 9 ULS:STD/1=1*1.35 + 2*1.50 1*1.35+2*1.50----------------------------------------------------------------------------------------------------------------------------------------
MATERIAL:
S275 ( S275 ) fy = 275.000 MPa----------------------------------------------------------------------------------------------------------------------------------------
SECTION PARAMETERS: UC 305x305x118
h=315 mm gM0=1.00 gM1=1.00 b=307 mm Ay=12040 mm2 Az=4296 mm2 Ax=15000 mm2tw=12 mm Iy=276700000 mm4 Iz=90590000 mm4 Ix=1610000 mm4tf=19 mm Wply=1958000 mm3 Wplz=895000 mm3----------------------------------------------------------------------------------------------------------------------------------------
INTERNAL FORCES AND CAPACITIES:
N,Ed = 35.713 kN My,Ed = -72.420 kN*m Mz,Ed = 0.000 kN*m Vy,Ed = 0.000 kN Nc,Rd = 4125.000 kN My,pl,Rd = 538.450 kN*m Mz,pl,Rd = 246.125 kN*m Vy,T,Rd = 1911.518 kN Nb,Rd = 4125.000 kN My,c,Rd = 538.450 kN*m Mz,c,Rd = 246.125 kN*m Vz,Ed = 74.459 kN MN,y,Rd = 538.450 kN*m MN,z,Rd = 246.125 kN*m Vz,T,Rd = 682.095 kN
Mb,Rd = 454.612 kN*m Tt,Ed = 0.000 kN*mClass of section = 1
----------------------------------------------------------------------------------------------------------------------------------------
LATERAL BUCKLING PARAMETERS: z = 1.00 Mcr = 851.601 kN*m Curve,LT - b XLT = 0.82Lcr,low=6.25 m Lam_LT = 0.80 fi,LT = 0.80 XLT,mod = 0.84----------------------------------------------------------------------------------------------------------------------------------------BUCKLING PARAMETERS:
About y axis: About z axis: kyy = 1.00 kzz = 1.00
----------------------------------------------------------------------------------------------------------------------------------------VERIFICATION FORMULAS: Section strength check: N,Ed/Nc,Rd = 0.01 < 1.00 (6.2.4.(1))(My,Ed/MN,y,Rd)^ 2.00 + (Mz,Ed/MN,z,Rd)^1.00 = 0.02 < 1.00 (6.2.9.1.(6))Vy,Ed/Vy,T,Rd = 0.00 < 1.00 (6.2.6-7)Vz,Ed/Vz,T,Rd = 0.11 < 1.00 (6.2.6-7)Tau,ty,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Tau,tz,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Global stability check of member:My,Ed/Mb,Rd = 0.16 < 1.00 (6.3.2.1.(1)) N,Ed/(Xy*N,Rk/gM1) + kyy*My,Ed/(XLT*My,Rk/gM1) + kyz*Mz,Ed/(Mz,Rk/gM1) = 0.17 < 1.00 (6.3.3.(4)) N,Ed/(Xz*N,Rk/gM1) + kzy*My,Ed/(XLT*My,Rk/gM1) + kzz*Mz,Ed/(Mz,Rk/gM1) = 0.17 < 1.00 (6.3.3.(4))----------------------------------------------------------------------------------------------------------------------------------------
Section OK !!!
STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------
7/23/2019 03 300x300x118 Beam
http://slidepdf.com/reader/full/03-300x300x118-beam 3/4
Autodesk Robot Structural Analysis Professional 2013 Author: WBB File: Address: Harvest Consulting Engineers LLP Project: Structure
Date : 14/12/15 Page : 3
CODE: BS-EN 1993-1:2005/NA:2008/AC:2009, Eurocode 3: Design of steel structures.ANALYSIS TYPE: Member Verification----------------------------------------------------------------------------------------------------------------------------------------
CODE GROUP:
MEMBER: 9 Beam_9 POINT: 3 COORDINATE: x = 1.00 L = 2.85m----------------------------------------------------------------------------------------------------------------------------------------
LOADS:
Governing Load Case: 9 ULS:STD/1=1*1.35 + 2*1.50 1*1.35+2*1.50----------------------------------------------------------------------------------------------------------------------------------------
MATERIAL:
S275 ( S275 ) fy = 275.000 MPa----------------------------------------------------------------------------------------------------------------------------------------
SECTION PARAMETERS: UC 305x305x118
h=315 mm gM0=1.00 gM1=1.00
b=307 mm Ay=12040 mm2 Az=4296 mm2 Ax=15000 mm2tw=12 mm Iy=276700000 mm4 Iz=90590000 mm4 Ix=1610000 mm4tf=19 mm Wply=1958000 mm3 Wplz=895000 mm3----------------------------------------------------------------------------------------------------------------------------------------
INTERNAL FORCES AND CAPACITIES:
N,Ed = 30.676 kN My,Ed = -55.646 kN*m Mz,Ed = -0.000 kN*m Vy,Ed = 0.000 kN Nc,Rd = 4125.000 kN My,pl,Rd = 538.450 kN*m Mz,pl,Rd = 246.125 kN*m Vy,T,Rd = 1911.508 kN Nb,Rd = 4125.000 kN My,c,Rd = 538.450 kN*m Mz,c,Rd = 246.125 kN*m Vz,Ed = -50.541 kN MN,y,Rd = 538.450 kN*m MN,z,Rd = 246.125 kN*m Vz,T,Rd = 682.093 kN
Mb,Rd = 538.450 kN*m Tt,Ed = 0.001 kN*mClass of section = 1
----------------------------------------------------------------------------------------------------------------------------------------
LATERAL BUCKLING PARAMETERS:
z = 1.00 Mcr = 2775.924 kN*m Curve,LT - b XLT = 0.98Lcr,low=2.85 m Lam_LT = 0.44 fi,LT = 0.58 XLT,mod = 1.00----------------------------------------------------------------------------------------------------------------------------------------
BUCKLING PARAMETERS:
About y axis: About z axis: kyy = 1.00 kzz = 1.00
----------------------------------------------------------------------------------------------------------------------------------------VERIFICATION FORMULAS: Section strength check: N,Ed/Nc,Rd = 0.01 < 1.00 (6.2.4.(1))(My,Ed/MN,y,Rd)^ 2.00 + (Mz,Ed/MN,z,Rd)^1.00 = 0.01 < 1.00 (6.2.9.1.(6))Vy,Ed/Vy,T,Rd = 0.00 < 1.00 (6.2.6-7)Vz,Ed/Vz,T,Rd = 0.07 < 1.00 (6.2.6-7)Tau,ty,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Tau,tz,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Global stability check of member:My,Ed/Mb,Rd = 0.10 < 1.00 (6.3.2.1.(1)) N,Ed/(Xy*N,Rk/gM1) + kyy*My,Ed/(XLT*My,Rk/gM1) + kyz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4)) N,Ed/(Xz*N,Rk/gM1) + kzy*My,Ed/(XLT*My,Rk/gM1) + kzz*Mz,Ed/(Mz,Rk/gM1) = 0.11 < 1.00 (6.3.3.(4))----------------------------------------------------------------------------------------------------------------------------------------
Section OK !!!
STEEL DESIGN----------------------------------------------------------------------------------------------------------------------------------------
CODE: BS-EN 1993-1:2005/NA:2008/AC:2009, Eurocode 3: Design of steel structures.
7/23/2019 03 300x300x118 Beam
http://slidepdf.com/reader/full/03-300x300x118-beam 4/4
Autodesk Robot Structural Analysis Professional 2013 Author: WBB File: Address: Harvest Consulting Engineers LLP Project: Structure
Date : 14/12/15 Page : 4
ANALYSIS TYPE: Member Verification----------------------------------------------------------------------------------------------------------------------------------------
CODE GROUP:
MEMBER: 10 Beam_10 POINT: 1 COORDINATE: x = 0.00 L = 0.00
m----------------------------------------------------------------------------------------------------------------------------------------LOADS:
Governing Load Case: 9 ULS:STD/1=1*1.35 + 2*1.50 1*1.35+2*1.50----------------------------------------------------------------------------------------------------------------------------------------
MATERIAL:
S275 ( S275 ) fy = 275.000 MPa----------------------------------------------------------------------------------------------------------------------------------------
SECTION PARAMETERS: UC 305x305x118
h=315 mm gM0=1.00 gM1=1.00 b=307 mm Ay=12040 mm2 Az=4296 mm2 Ax=15000 mm2
tw=12 mm Iy=276700000 mm4 Iz=90590000 mm4 Ix=1610000 mm4tf=19 mm Wply=1958000 mm3 Wplz=895000 mm3----------------------------------------------------------------------------------------------------------------------------------------INTERNAL FORCES AND CAPACITIES:
N,Ed = 35.713 kN My,Ed = -72.420 kN*m Mz,Ed = -0.000 kN*m Vy,Ed = -0.000 kN Nc,Rd = 4125.000 kN My,pl,Rd = 538.450 kN*m Mz,pl,Rd = 246.125 kN*m Vy,T,Rd = 1911.518 kN Nb,Rd = 4125.000 kN My,c,Rd = 538.450 kN*m Mz,c,Rd = 246.125 kN*m Vz,Ed = 74.459 kN MN,y,Rd = 538.450 kN*m MN,z,Rd = 246.125 kN*m Vz,T,Rd = 682.095 kN
Mb,Rd = 454.612 kN*m Tt,Ed = -0.000 kN*mClass of section = 1
----------------------------------------------------------------------------------------------------------------------------------------
LATERAL BUCKLING PARAMETERS:
z = 1.00 Mcr = 851.601 kN*m Curve,LT - b XLT = 0.82Lcr,low=6.25 m Lam_LT = 0.80 fi,LT = 0.80 XLT,mod = 0.84----------------------------------------------------------------------------------------------------------------------------------------
BUCKLING PARAMETERS:
About y axis: About z axis: kyy = 1.00 kzz = 1.00
----------------------------------------------------------------------------------------------------------------------------------------VERIFICATION FORMULAS: Section strength check: N,Ed/Nc,Rd = 0.01 < 1.00 (6.2.4.(1))(My,Ed/MN,y,Rd)^ 2.00 + (Mz,Ed/MN,z,Rd)^1.00 = 0.02 < 1.00 (6.2.9.1.(6))Vy,Ed/Vy,T,Rd = 0.00 < 1.00 (6.2.6-7)Vz,Ed/Vz,T,Rd = 0.11 < 1.00 (6.2.6-7)Tau,ty,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Tau,tz,Ed/(fy/(sqrt(3)*gM0)) = 0.00 < 1.00 (6.2.6)Global stability check of member:My,Ed/Mb,Rd = 0.16 < 1.00 (6.3.2.1.(1)) N,Ed/(Xy*N,Rk/gM1) + kyy*My,Ed/(XLT*My,Rk/gM1) + kyz*Mz,Ed/(Mz,Rk/gM1) = 0.17 < 1.00 (6.3.3.(4)) N,Ed/(Xz*N,Rk/gM1) + kzy*My,Ed/(XLT*My,Rk/gM1) + kzz*Mz,Ed/(Mz,Rk/gM1) = 0.17 < 1.00 (6.3.3.(4))----------------------------------------------------------------------------------------------------------------------------------------
Section OK !!!
