Creep Factor, Bd = 0.00Section Stiffness, EI For Pcr = 0.00E+00 kg-cm^2Euler Buckling Load, Pcr = 0.000 tonBuckling Failure = Pcr < Pu

Basic Section Properties:

Total Width = 45.00 cmTotal Height = 45.00 cmCenter, Xo = 0.00 cmCenter, Yo = 0.00 cm

X-bar (Right) = 22.50 cmX-bar (Left) = 22.50 cmY-bar (Top) = 22.50 cmY-bar (Bot) = 22.50 cm

Transformed Properties:Base Material = fc' = 250

kg/cm^2Area, A = 2,025.0 cm^2Inertia, I33 = 3.42E+05 cm^4Inertia, I22 = 3.42E+05 cm^4Inertia, I32 = 0.00E+00 cm^4

Radius, r3 = 12.99 cmRadius, r2 = 12.99 cm

Additional Section Properties:

Transformed Properties:Base Material = fc' = 250

kg/cm^2Modulus, S3(Top) = 1.52E+04 cm^3Modulus, S3(Bot) = 1.52E+04 cm^3Modulus, S2(Left) = 1.52E+04 cm^3Modulus, S2(Right) = 1.52E+04 cm^3

Plastic Modulus, Z3 = 2.68E+04 cm^3Plastic Modulus, Z2 = 2.68E+04 cm^3Torsional, J = 5.93E+05 cm^4Shear Area, A3 = 1,718.9 cm^2Shear Area, A2 = 1,718.9 cm^2

Principal Angle = 0.00E+00 DegInertia, I33' = 3.42E+05 cm^4Inertia, I22' = 3.42E+05 cm^4

Framing Along-X

Total C/C Length, Lc = 6.500 mUnsupported Length, Lu = 6.000 mFraming Type = 1Framing Case = 0K Factor, Braced = 1.00Kl/r, Braced = 46.19K Factor, Unbraced = 1.00Kl/r, Unbraced = 46.19

Framing Along-Y

Total C/C Length, Lc = 6.500 mUnsupported Length, Lu = 6.000 mFraming Type = 1

Framing Case = 0K Factor, Braced = 1.00Kl/r, Braced = 46.19K Factor, Unbraced = 1.00Kl/r, Unbraced = 46.19

Final Design Loads

Sr.No CombinationLoad Pu Mux-Bot Muy-Bot Mux-Top

Muy-Top

ton ton-m ton-m ton-m ton-m

1U=1.4CM+1.7CV+ 65.00 10.00 10.00 10.00 10.001.7H+1.4(SX+0.3SZ)

Result Summary

Sr.No Combination Pu (ton)Cap. Ratio-Bot

Cap. Ratio-Top Remarks

1U=1.4CM+1.7CV+ 65.00 0.648 0.648 Capacity OK1.7H+1.4(SX+0.3SZ)

Moment Magnification Calculations

Load-Moment Interaction

Load-Moment Interaction

Moment-Moment Interaction

Moment-Curvature Curve (Angle = 0

Load Point Location: Loading-1 (Bot)

Load Point Location: Loading-1 (Bot)

Neutral Axis Location: Loading-1 (Bot)

Elastic Stresses: Loading-1 (Bot)

Cracked Stresses: Loading-1 (Bot)

Rebar Stresses: Loading-1 (Bot)