1605 EDGEMOOR LN 2025-04-25 - Laserfiche WebLink

' Project Title: Engineer: Project ID: SDA#9684A-6' DECK Project Descr: Wood Column Project File:9684A.ec6 LIC#:KW-06014008,Build:20.22.12.28 Structural Design Associates (c)ENERCALC INC 1983-2022 DESCRIPTION: DECK POST- MIDDLE Code References Calculations per NDS 2018, IBC 2018, CBC 2019,ASCE 7-16 Load Combinations Used : IBC 2018 General Information Analysis Method Allowable Stress Design Wood Section Name 6x8 End Fixities Top Free,Bottom Fixed Wood Grading/Manuf. Graded Lumber Overall Column Height 18 ft Wood Member Type Sawn Exact Width 5.50 in Allow Stress Modification Factors Wood Species Hem-Fir Exact Depth Wood Grade No.2 7.50 in Cf or Cv for Bending 1.0 Fb+ 575.0 psi Fv 140.0 psi Area 41.250 inA2 Cf or Cv for Compressioi 1.0 lx 193.359 in^4 Cf or Cv for Tension 1.0 Fb- 575.0 psi Ft 375.0 psi ly :Wet Use Factor 1.0 Fc-Prll 575.0 psi Density 26.840 pcf y 103.984 inA4 Incising Factors: Ct:Temperature Fact 1.0 Fc-Perp 405.0 psi for Bending 0.80 Cfu:Flat Use Factor 1.0 E:Modulus of Elasticity.. . x-x Bending y-y Bending Axial for Elastic Modulus 0.95 Kf:Built-up columns 1.0 Basic 1,100.0 1,100.0 1,100.0 ksi Use Cr:Repetitive? No Minimum 400.0 400.0 Brace condition for deflection(buckling)along columns: X-X(width)axis: Unbraced Length for buckling ABOUT Y-Y Axis=18 ft,I. Y-Y(depth)axis: Unbraced Length for buckling ABOUT X-X Axis=18 ft,I Applied Loads Service loads entered. Load Factors will be applied for calculations. Column self weight included : 138.394 Ibs*Dead Load Factor AXIAL LOADS . . . Axial Load at 18.0 ft,Xecc=0.750 in, D=0.560, L= 1.960, S =0.820 k Axial Load at 18.0 ft, D= 0.560, L = 1.960, S=0.820 k DESIGN SUMMARY Bending&Shear Check Results PASS Max.Axial+Bending Stress Ratio = 0.7316: 1 Maximum SERVICE Lateral Load Reactions. Load Combination +D+0.750L+0.750S Top along Y-Y 0.0 k Bottom along Y-Y 0.0 k Governing NDS Forumla Comp+Myy,NDS Eq.3.9-3 Top along X-X 0.0 k Bottom along X-X 0.0 k Location of max.above base 0.0 ft Maximum SERVICE Load Lateral Deflections... At maximum location values are. Along Y-Y 0.0 in at 0.0 ft above base Applied Axial 5.428 k for load combination: n/a Applied Mx 0.0 k-ft Applied My -0.1653 k-ft Along X-X 0.4230 in at 18.0 ft above base Fc:Allowable 191.461 psi for load combination:+D+0.750L+0.750S Other Factors used to calculate allowable stresses... PASS Maximum Shear Stress Ratio= 0.0: 1 Bending Compression Tension Load Combination +0.4491 D Location of max.above base 18.0 ft Applied Design Shear 0.0 psi Allowable Shear 179.20 psi Load Combination Results Maximum Axial+Bendina Stress Ratios Maximum Shear Ratios Load Combination C D C p Stress Ratio Status Location Stress Ratio Status Location D Only 0.900 0.444 0.1660 PASS 0.0 ft 0.0 PASS 18.0 ft +D+L 1.000 0.407 0.7130 PASS 0.0 ft 0.0 PASS 18.0 ft +D+S 1.150 0.362 0.3670 PASS 0.0 ft 0.0 PASS 18.0 ft +D+0.750L 1.250 0.337 0.5259 PASS 0.0 ft 0.0 PASS 18.0 ft +D+0.750L+0.750S 1.150 0.362 0.7316 PASS 0.0ft 0.0 PASS 18.0ft +1.151D 1.600 0.270 0.1769 PASS 0.0 ft 0.0 PASS 18.0 ft +1.113D+0.750L+0.750S 1.600 0.270 0.6803 PASS 0.0 ft 0.0 PASS 18.0 ft +0.60D 1.600 0.270 0.09220 PASS 0.0 ft 0.0 PASS 18.0 ft +0.4491D 1.600 0.270 0.06901 PASS 0.0 ft 0.0 PASS 18.0 ft