Sheet1--------------------------------------------------------------------------------------------------------Connection Template : BEP_BCF_E_20PL_3B_M24 G8_8Connection ID : BCF - N(2) - M(1,3)Design Code: BS5950-01:2000(amendments 2001)--------------------------------------------------------------------------------------------------------Connection Template : BEP_BCF_E_20PL_3B_M24 G8_8Connection ID : BCF - N(2) - M(1,3)Design Code : BS5950-01:2000GENERAL DATAIs column end:YesConsider sheared edges in shapes:NoExists opposite connection:NoConsider sheared edges in shapes:NoWind provisions:NoCorrosive influences:NoMEMBERS:BeamSection=ISHB350 Material=STEEL SupportSection=ISHB350 Material=STEEL CONNECTION(S):Connection: Extended end plateExtended end plateSection=PL 20x200x475 Material=S275 tp=20.00 [mm]bolt=M24 G8_8 nt=3Tension bolts row numbernc=1Shear bolts row numberp=90.00 [mm]Longitudinal spacingg=90.00 [mm]Transversal spacinge=55.00 [mm]Horizontal end distance to bolt centerpf=60.00 [mm]Distance from internal bolt to beam flangeex=50.00 [mm]Vertical end distance to bolt centerx=40.00 [mm]Distance from external bolt to beam flangeef=35.00 [mm]Flush extension lengthswf=10.00 [mm]Weld size to column flangesww=8.00 [mm]Welding electrode to column webLOADSMembersLoadTypeV2V3M33M22Axial[KN][KN][KN*m][KN*m][KN]--------------------------------------------------------------------------------------------------------ColumnLC-1Design---------15Right beamLC-1Design15---75------------------------------------------------------------------------------------------------------------GEOMETRIC CONSIDERATIONSDimensionsUnitValueMin. valueMax. valueSta.References--------------------------------------------------------------------------------------------------------Extended end plateVertical center-to-center spacing (pitch)[mm]9060162.4 Cl.6.2.1.1,Cl.6.2.1.2IsStandardHole Truespamin = 2.5*d = 2.5*24[mm] = 60[mm]Cl. 6.2.1.1CorrosiveInfluences Falsespamax = 14*t = 14*11.6[mm] = 162.4[mm]Cl. 6.2.1.2Horizontal center-to-center spacing (gage)[mm]9060110 Cl.6.2.1.1,Cl.6.3.4.2IsStandardHole Truespamin = 2.5*d = 2.5*24[mm] = 60[mm]Cl. 6.2.1.1spamax = 0.55*B = 0.55*200[mm] = 110[mm]Cl. 6.3.4.2Vertical edge distance[mm]5032.5224.11 Cl.6.2.2.4,Cl.6.2.2.5ShearedEdges Falsedemin = 1.25*d = 1.25*26[mm] = 32.5[mm]Cl. 6.2.2.4CorrosiveInfluences Falsee = (275*[N/mm2]/py)1/2 = (275*[N/mm2]/0.265[KN/mm2])1/2 = 1.018693Cl. 1.4demax = 11*t*e = 11*20[mm]*1.018693 = 224.11[mm]Cl. 6.2.2.5Horizontal edge distance[mm]5532.5224.11 Cl.6.2.2.4,Cl.6.2.2.5ShearedEdges Falsedemin = 1.25*d = 1.25*26[mm] = 32.5[mm]Cl. 6.2.2.4CorrosiveInfluences Falsee = (275*[N/mm2]/py)1/2 = (275*[N/mm2]/0.265[KN/mm2])1/2 = 1.018693Cl. 1.4demax = 11*t*e = 11*20[mm]*1.018693 = 224.11[mm]Cl. 6.2.2.5Flush extension length[mm]3530-- BCSA-JSCMC p143dmin = tp + s = 20[mm] + 10[mm] = 30[mm]BCSA-JSCMC p143SupportHorizontal center-to-center spacing (gage)[mm]90--137.5 Cl. 6.3.4.2spamax = 0.55*B = 0.55*250[mm] = 137.5[mm]Cl. 6.3.4.2Horizontal edge distance[mm]8032.5132.98 Cl.6.2.2.4,Cl.6.2.2.5ShearedEdges Falsedemin = 1.25*d = 1.25*26[mm] = 32.5[mm]Cl. 6.2.2.4CorrosiveInfluences Falsee = (275*[N/mm2]/py)1/2 = (275*[N/mm2]/0.2532[KN/mm2])1/2 = 1.04216Cl. 1.4demax = 11*t*e = 11*11.6[mm]*1.04216 = 132.98[mm]Cl. 6.2.2.5Vertical edge distance[mm]5032.5-- Cl. 6.2.2.4ShearedEdges Falsedemin = 1.25*d = 1.25*26[mm] = 32.5[mm]Cl. 6.2.2.4WARNINGSThe tension zone bolts overlap the compression zone boltsThe plate width is less than the beam width--------------------------------------------------------------------------------------------------------DESIGN CHECKVerificationUnitCapacityDemandCtrl EQRatioReferences--------------------------------------------------------------------------------------------------------Tension zoneNegative moment capacity[KN*m]81.675LC-10.92BCSA-JSCMC p30Mc = S(Fri x hi ) = 81.603815[KN*m]BCSA-JSCMC p30Final force at the bolt row 1[KN]162.23 BCSA-JSCMC p18Column flange bending[KN]162.23 BCSA-JSCMC p18LeffPatternV = 2*m + 0.625*e + ex = 2*36.21[mm] + 0.625*80[mm] + 50[mm] = 172.42[mm]BCSA-JSCMC Table 2.4LeffPatternII = 4*m + 1.25*e = 4*36.21[mm] + 1.25*80[mm] = 244.84[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*36.21[mm] = 227.51[mm]BCSA-JSCMC Table 2.4Leff = min(LeffPatternV, LeffPatternII, LeffPatternI) = min(172.42[mm], 244.84[mm], 227.51[mm]) =172.42[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (172.42[mm]*11.6[mm]2*0.2532[KN/mm2])/4 = 1.468613[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*1.468613[KN*m]/36.21[mm] = 162.23[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*1.468613[KN*m] + 45.2625[mm]*395.36[KN])/(36.21[mm] + 45.2625[mm]) = 255.7[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(162.23[KN], 255.7[KN], 395.36[KN]) = 162.23[KN]BCSA-JSCMC p. 18Column flange tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24End plate bending[KN]293.26 BCSA-JSCMC p18LeffPatternVII = bp/2 = 200[mm]/2 = 100[mm]BCSA-JSCMC Table 2.4LeffPatternVIII = 2*mx + 0.625*ex + g/2 = 2*32[mm] + 0.625*50[mm] + 90[mm]/2 = 140.25[mm]BCSA-JSCMC Table 2.4LeffPatternIX = 2*mx + 0.625*ex + e = 2*32[mm] + 0.625*50[mm] + 55[mm] = 150.25[mm]BCSA-JSCMC Table 2.4LeffPatternX = 4*mx + 1.25*ex = 4*32[mm] + 1.25*50[mm] = 190.5[mm]BCSA-JSCMC Table 2.4LeffPatternXI = 2*Pi*mx = 2*Pi*32[mm] = 201.06[mm]BCSA-JSCMC Table 2.4Leff = min(LeffPatternVII, LeffPatternVIII, min(LeffPatternIX, LeffPatternX, LeffPatternXI)) =min(100[mm], 140.25[mm], min(150.25[mm], 190.5[mm], 201.06[mm])) = 100[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (100[mm]*20[mm]2*0.265[KN/mm2])/4 = 2.65[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*2.65[KN*m]/32[mm] = 331.25[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*2.65[KN*m] + 40[mm]*395.36[KN])/(32[mm] +40[mm]) = 293.26[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(331.25[KN], 293.26[KN], 395.36[KN]) = 293.26[KN]BCSA-JSCMC p. 18Beam web tension[KN]N/A Triangular limit[KN]N/A Final force at the bolt row 2[KN]-21.1 BCSA-JSCMC p18Column flange bending[KN]-21.1 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*36.21[mm] + 1.25*80[mm] = 244.84[mm]BCSA-JSCMC Table 2.4Leff = min(ex, LeffPatternII/2) + pn = min(50[mm], 244.84[mm]/2) + 100[mm] = 150[mm]BCSA-JSCMC Table 2.6Mp = (Leff*t2*py)/4 = (150[mm]*11.6[mm]2*0.2532[KN/mm2])/4 = 1.277647[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 4*197.68[KN] = 790.72[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*1.277647[KN*m]/36.21[mm] = 141.14[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*1.277647[KN*m] + 45.2625[mm]*790.72[KN])/(36.21[mm] + 45.2625[mm]) = 470.65[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(141.14[KN], 470.65[KN], 790.72[KN]) = 141.14[KN]BCSA-JSCMC p. 18Column flange tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24End plate bending[KN]367.65 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*34.45[mm] + 1.25*55[mm] = 206.55[mm]BCSA-JSCMC Table 2.4LeffPatternIII = a*m1 = 6.283185*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4Leff = min(max(LeffPatternII, LeffPatternIII), LeffPatternI) =min(max(206.55[mm], 216.46[mm]), 216.46[mm]) = 216.46[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (216.46[mm]*20[mm]2*0.265[KN/mm2])/4 = 5.736077[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*5.736077[KN*m]/34.45[mm] = 666.02[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*5.736077[KN*m] + 43.0625[mm]*395.36[KN])/(34.45[mm] + 43.0625[mm]) = 367.65[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(666.02[KN], 367.65[KN], 395.36[KN]) = 367.65[KN]BCSA-JSCMC p. 18Beam web tension[KN]N/A Triangular limit[KN]N/A Final force at the bolt row 3[KN]84.68 BCSA-JSCMC p18Column flange bending[KN]84.68 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*36.21[mm] + 1.25*80[mm] = 244.84[mm]BCSA-JSCMC Table 2.4Leff = min(ex, LeffPatternII/2) + pn = min(50[mm], 244.84[mm]/2) + 190[mm] = 240[mm]BCSA-JSCMC Table 2.6Mp = (Leff*t2*py)/4 = (240[mm]*11.6[mm]2*0.2532[KN/mm2])/4 = 2.044235[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 6*197.68[KN] = 1186.08[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*2.044235[KN*m]/36.21[mm] = 225.82[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*2.044235[KN*m] + 45.2625[mm]*1186.08[KN])/(36.21[mm] + 45.2625[mm]) = 709.12[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(225.82[KN], 709.12[KN], 1186.08[KN]) = 225.82[KN]BCSA-JSCMC p. 18Column flange tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24End plate bending[KN]360.88 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*34.45[mm] + 1.25*55[mm] = 206.55[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4Leff = min(LeffPatternII, LeffPatternI) = min(206.55[mm], 216.46[mm]) = 206.55[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (206.55[mm]*20[mm]2*0.265[KN/mm2])/4 = 5.473575[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*5.473575[KN*m]/34.45[mm] = 635.54[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*5.473575[KN*m] + 43.0625[mm]*395.36[KN])/(34.45[mm] + 43.0625[mm]) = 360.88[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(635.54[KN], 360.88[KN], 395.36[KN]) = 360.88[KN]BCSA-JSCMC p. 18Beam web tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24Triangular limit[KN]N/A Final force at the bolt row 4[KN]84.68 BCSA-JSCMC p18Column flange bending[KN]84.68 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*36.21[mm] + 1.25*80[mm] = 244.84[mm]BCSA-JSCMC Table 2.4Leff = min(ex, LeffPatternII/2) + pn = min(50[mm], 244.84[mm]/2) + 280[mm] = 330[mm]BCSA-JSCMC Table 2.6Mp = (Leff*t2*py)/4 = (330[mm]*11.6[mm]2*0.2532[KN/mm2])/4 = 2.810824[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 8*197.68[KN] = 1581.44[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*2.810824[KN*m]/36.21[mm] = 310.5[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*2.810824[KN*m] + 45.2625[mm]*1581.44[KN])/(36.21[mm] + 45.2625[mm]) = 947.58[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(310.5[KN], 947.58[KN], 1581.44[KN]) = 310.5[KN]BCSA-JSCMC p. 18Column flange tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24End plate bending[KN]360.88 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*34.45[mm] + 1.25*55[mm] = 206.55[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4Leff = min(LeffPatternII, LeffPatternI) = min(206.55[mm], 216.46[mm]) = 206.55[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (206.55[mm]*20[mm]2*0.265[KN/mm2])/4 = 5.473575[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*5.473575[KN*m]/34.45[mm] = 635.54[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*5.473575[KN*m] + 43.0625[mm]*395.36[KN])/(34.45[mm] + 43.0625[mm]) = 360.88[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(635.54[KN], 360.88[KN], 395.36[KN]) = 360.88[KN]BCSA-JSCMC p. 18Beam web tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24Triangular limit[KN]N/A Positive moment capacity[KN*m]60.840LC-10BCSA-JSCMC p30Mc = S(Fri x hi ) = 60.839215[KN*m]BCSA-JSCMC p30Final force at the bolt row 1[KN]214.07 BCSA-JSCMC p18Column flange bending[KN]214.07 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*36.21[mm] + 1.25*80[mm] = 244.84[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*36.21[mm] = 227.51[mm]BCSA-JSCMC Table 2.4Leff = min(LeffPatternII, LeffPatternI) = min(244.84[mm], 227.51[mm]) = 227.51[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (227.51[mm]*11.6[mm]2*0.2532[KN/mm2])/4 = 1.937885[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*1.937885[KN*m]/36.21[mm] = 214.07[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*1.937885[KN*m] + 45.2625[mm]*395.36[KN])/(36.21[mm] + 45.2625[mm]) = 267.22[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(214.07[KN], 267.22[KN], 395.36[KN]) = 214.07[KN]BCSA-JSCMC p. 18Column flange tension[KN]327.6 BCSA-JSCMC p24Lt1 = g*(3)1/2 = 90[mm]*(3)1/2 = 155.88[mm]BCSA-JSCMC p24Lt = Lt1 + Lt2 = 155.88[mm] + 0[mm] = 155.88[mm]BCSA-JSCMC p24Pt = Lt*tw*py = 155.88[mm]*8.3[mm]*0.2532[KN/mm2] = 327.6[KN]BCSA-JSCMC p24End plate bending[KN]364.26 BCSA-JSCMC p18LeffPatternII = 4*m + 1.25*e = 4*34.45[mm] + 1.25*55[mm] = 206.55[mm]BCSA-JSCMC Table 2.4LeffPatternIII = a*m1 = 6.283185*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4LeffPatternI = 2*Pi*m = 2*Pi*34.45[mm] = 216.46[mm]BCSA-JSCMC Table 2.4Leff = min(max((LeffPatternII + LeffPatternIII)/2, LeffPatternII), LeffPatternI) =min(max((206.55[mm] + 216.46[mm])/2, 206.55[mm]), 216.46[mm]) = 211.5[mm]BCSA-JSCMC Table 2.5Mp = (Leff*t2*py)/4 = (211.5[mm]*20[mm]2*0.265[KN/mm2])/4 = 5.604826[KN*m]BCSA-JSCMC p18Pt = pt*At = 0.56[KN/mm2]*353[mm2] = 197.68[KN]BCSA-JSCMC Table 2.1PrMode3 = n*Pt = 2*197.68[KN] = 395.36[KN]BCSA-JSCMC Eq. 2.3PrMode1 = 4*Mp/m = 4*5.604826[KN*m]/34.45[mm] = 650.78[KN]BCSA-JSCMC p18PrMode2 = (2*Mp + ne*SP1t)/(m + ne) = (2*5.604826[KN*m] + 43.0625[mm]*395.36[KN])/(34.45[mm] + 43.0625[mm]) = 364.26[KN]BCSA-JSCMC p18Pr = min(PrMode1, PrMode2, PrMode3) = min(650.78[KN], 364.26[KN], 395.36[KN]) = 364.26[KN]BCSA-JSCMC p. 18Beam web tension[KN]N/A Triangular limit[KN]N/A Horizontal shear zoneColumn web panel shear[KN]441.33221.63LC-10.5Cl. 4.2.3Pv = 0.6*pyc*tc*Dc = 0.6*0.2532[KN/mm2]*8.3[mm]*350[mm] = 441.33[KN]Cl. 4.2.3Compression zoneBeam flange compression[KN]1027.99221.63LC-10.22BCSA-JSCMC (2.9) p28Pcfb = 1.4*pyb*Tb*Bb = 1.4*0.2532[KN/mm2]*11.6[mm]*250[mm] = 1027.99[KN]BCSA-JSCMC (2.9) p28Column web crushing[KN]333.31221.63LC-10.66Cl. 4.5.2.1IsColumnEnd Truenbw = min(5, 2 + 0.6 + be/(Tc + rc)) = min(5, 2 + 0.6 + 328.4[mm]/(11.6[mm] + 5.8[mm])) = 5Cl. 4.5.2.1b1+n2 = Tb + 2*swf + 2*tp + nbw*(Tc + rc) = 11.6[mm] + 2*10[mm] + 2*20[mm] + 5*(11.6[mm] + 5.8[mm]) = 158.6[mm]Cl. 4.5.2.1Pc = (b1+n2)*tc*pyc = (158.6[mm])*8.3[mm]*0.2532[KN/mm2] = 333.31[KN]Cl. 4.5.2.1Compression buckling of the web[KN]322.37221.63LC-10.69Cl. 4.5.2.1,Cl. 4.5.3.1IsColumnEnd Truenbw = min(5, 2 + 0.6 + be/(Tc + rc)) = min(5, 2 + 0.6 + 328.4[mm]/(11.6[mm] + 5.8[mm])) = 5Cl. 4.5.2.1b1+n2 = Tb + 2*swf + 2*tp + nbw*(Tc + rc) = 11.6[mm] + 2*10[mm] + 2*20[mm] + 5*(11.6[mm] + 5.8[mm]) = 158.6[mm]Cl. 4.5.2.1Pc = (b1+n2)*tc*pyc = (158.6[mm])*8.3[mm]*0.2532[KN/mm2] = 333.31[KN]Cl. 4.5.2.1IsColumnEnd Truenbw = min(5, 2 + 0.6 + be/(Tc + rc)) = min(5, 2 + 0.6 + 328.4[mm]/(11.6[mm] + 5.8[mm])) = 5Cl. 4.5.2.1b1+n2 = Tb + 2*swf + 2*tp + nbw*(Tc + rc) = 11.6[mm] + 2*10[mm] + 2*20[mm] + 5*(11.6[mm] + 5.8[mm]) = 158.6[mm]Cl. 4.5.2.1e = (275*[N/mm2]/py)1/2 = (275*[N/mm2]/0.2532[KN/mm2])1/2 = 1.04216Cl. 1.4aebw