Page 9 - Constructor 50 mm Racking

Software calculated detail design check for each individual Projects

ABC Company CR18 Quick Check
unity checks: ( top 4 values of all calculated load cases )
maximum beam stress M z,Sd M z,Rd M y,Sd M y,Rd M Sd
member no. load case [kNm] [kNm] [kNm] [kNm] M Rd
B01/02 23 [/ full load] & [horizontal placem. load beam] 0.208 2.979 2.904 5.504 0.598
B01/02 23 [/ pattern load 1] & [horizontal placem. load beam] 0.208 2.979 2.899 5.504 0.597
B05/07 158 \ full load 0.000 0.000 3.271 5.504 0.594
B01/07 38 I pattern load 1 0.000 0.000 3.270 5.504 0.594
maximum beam-end-connector moments (M Sd0¦M Sd1) M Rd_HL (M Sd0¦M Sd1) 50 mm Pitch Pallet Racking
member no. load case [kNm] [kNm] M Rd_HL
H02/03 57 / pattern load 2 1.786 2.070 0.863
H01/02 24 / pattern load 1 1.772 2.070 0.856
H04/02 114 / pattern load 2 1.772 2.070 0.856
H01/02 24 / pattern load 2 1.766 2.070 0.853
maximum usage upright
member no. load case Term1 Term2 Term3  Term 1...3
S02/01 41 / pattern load 2 0.612 0.365 0.000 0.978
S01/01 11 [ I pattern load 1 ] & [ / pattern load 1 CA] 0.699 0.256 0.020 0.976
S02/01 41 / pattern load 1 0.663 0.304 0.000 0.966
S02/01 41 [ I pattern load 1 ] & [ / pattern load 1 CA] 0.699 0.243 0.020 0.962

maximum base moments M Sd_F M Rd_F M Sd_F
member no. load case [kNm] [kNm] M Rd_F
S01/01 11 / pattern load 2 0.584 1.555 0.376
S01/01 11 / pattern load 1 0.581 1.555 0.373
S01/01 11 / pattern load 1 + placem. load top beam 0.562 1.631 0.344
S01/01 11 / full load 0.489 1.500 0.326
maximum frame bracing stress
member no. load case analysis factor
D00/01 2 / full load + accidental load CA compression stress 0.241
D00/01 2 / full load + placem. load 1st diagonal CA compression stress 0.163
D00/01 2 / pattern load 1 + placem. load 1st diagonal CA compression stress 0.160
D00/01 2 / full load + placem. load CA compression stress 0.144
stability unity check number of floor fixings / F t,Sd F p,Rd F t,Sd
load case baseplate [kN] [kN] F p,Rd
unloaded + placem. load top CA 1 2.070 3.500 0.591
maximum pressure baseplate A bas f j N Sd_F N Rd_F N Sd _F N Sd_F
member no. load case [cm²] [kN/cm²] [kN] [kN] f  A bas max N Rd_F
j
S-B/01 18 / full load CA 41.65 3.333 103.70 105.00 0.988
S04/01 101 \ full load 41.65 3.333 98.13 105.00 0.935
S01/01 11 / full load 41.65 3.333 98.13 105.00 0.935
S04/01 101 / pattern load 2 41.65 3.333 98.09 105.00 0.934

serviceability: ( top 2 values of load case: user load )
maximum deflection of beams f max f zul f max
member no. load case [mm] [mm] f zul
B01/07 38 / serviceability load 9.556 13.000 0.735
B05/07 158 / serviceability load 9.539 13.000 0.734
maximum down-aisle sway v x_St v x_zul v x_St
www.genexwholesale.com.au
member no. load case [mm] [mm] v x_zul
S00/08 9 / serviceability load 15.893 50.000 0.318
S01/08 18 / serviceability load 14.801 50.000 0.296
maximum cross-aisle sway v z_St v z_zul v z_St
member no. load case [mm] [mm] v z_zul
S-A/08 51 / user load CA 4.547 50.000 0.091
S-B/08 52 / user load CA 4.541 50.000 0.091
rptQuickCheck Calculation: 6/23/2021 1:05:40 PM -36-