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16x20 Biaxial Column, 10-#8

Biaxial bending for a 16x20 / 10-#8 column per ACI 318-19: demand-plane cut through the 3D P-Mx-My interaction surface and D/C.


16 × 20 in 10-#8 f′c 4,000 psi fy 60 ksi Biaxial Full inputs

Biaxial bending (P-Mx-My): demand-plane angle λ = 31.0 deg

PASS

Both axial and moment D/C ratios ≤ 1.00.

Demand-plane summary

λ (demand-plane angle)
31.0 deg
Mx,design
50.0 kip-ft
My,design
30.0 kip-ft

P-M interaction diagram

P-M interaction diagram showing demand point against the φ-reduced capacity envelope

Demand (Pu, Mu) tested against the φ-reduced capacity envelope. Operating point (φPn, φMn) shown on the boundary. φ is computed per anchor from εt (§21.2.2); your operating point lies in the compression-controlled region; how the φ transition works.

3D interaction surface

P-Mx-My capacity envelope (φ-reduced) at 10° cuts. Drag to rotate, scroll to zoom, right-drag to pan. demand point (Pu, Mux, Muy). operating point (φPn, φMnx, φMny).

Interaction Diagram Points (9 anchors, demand-plane cut at λ = 31.0 deg)
Anchor Description c (in) εt φ φPn (kip) φMλ (kip-ft)
1 Pure compression cap N/A N/A 0.65 798.27 0.00
2 Cap intersection 22.98 -0.00009 0.65 798.20 107.27
3 Arc strain (zero) (εt = 0) 22.26 0.00000 0.65 773.86 118.46
4 Arc strain (positive half yield) (εt = +εty/2) 16.44 0.00103 0.65 502.69 192.90
5 Compression-controlled limit (εt = εty) 13.09 0.00207 0.65 276.24 211.61
6 Transition lower (εt = εty + 0.0015) 10.14 0.00357 0.78 92.28 228.79
7 Tension-controlled limit (εt = εty + 0.003) 8.94 0.00446 0.85 0.05 225.41
8 Tension-controlled deep (εt = εty + 0.008) 8.94 0.00446 0.85 0.05 225.41
9 Pure bending 8.94 0.00446 0.85 0.00 225.41
Strength-reduced interaction curve ACI 318-19 §22.4.2 · §21.2.2
Quantity Value
Pu (factored axial demand, kip) 200.00
φPn (axial capacity at operating point, kip) 584.56
Mu (resultant in the demand plane, Mλ, design moment, kip-ft) 58.31

No transverse load between supports. Cm from end-moment ratio per ACI 318-19 §6.6.4.5.3(a).

φMλ (moment capacity, kip-ft) 170.43
c (neutral axis depth, in) N/A
εt (extreme tension strain) N/A
φ (strength reduction factor) N/A
φ regime (§21.2.2) Compression-controlled φ = 0.65 throughout (εt ≤ εty = 0.00207)
D/C axial 0.34
D/C moment 0.34
Slenderness (about X)
kl/r about X 20.00

Nonsway frames only (ACI 318-19 §6.6.4.3).

kl/r limit 28.00
Slenderness (about Y)
kl/r about Y 25.00

Nonsway frames only (ACI 318-19 §6.6.4.3).

kl/r limit 28.00
Tie spacing limit (§25.7.2.1) 16.00 in (governed by 16·d_bar)
Bar clear spacing (§25.2.3) 4.08 in ≥ 1.50 in
Input summary (values as entered)
Section geometry
Section 16 × 20 in (rectangular)
Ag (gross area) * 320.0 in²
Ast (total steel area) * 7.90 in²
ρ (reinforcement ratio) * 0.0247 (2.47%)
Materials
f′c 4,000 psi
fy (longitudinal) 60 ksi (Grade 60)
Concrete Normal weight
Reinforcement
Longitudinal bars 10-#8
Per-face distribution 1 per b-face, 2 per h-face (+ 4 corners)
Clear cover 1.5 in
Transverse #3 ties @ 16 in
Loads
Pu 200 kip
M2x (larger end moment, about X) 50 kip-ft
M1x (smaller end moment, about X) 25 kip-ft
Curvature about X Single
M2y (larger end moment, about Y) 30 kip-ft
M1y (smaller end moment, about Y) 15 kip-ft
Curvature about Y Single
Bending Biaxial (P-Mx-My)
Transverse load between supports No
Slenderness parameters
Lu,x (unsupported length, about X) 120 in (10.00 ft)
kx (effective length factor, about X) 1
Lu,y (unsupported length, about Y) 120 in (10.00 ft)
ky (effective length factor, about Y) 1
* Derived from entered dimensions and reinforcement; not directly entered.

Assumptions and limits

  • Tie arrangement and crossties (§25.7.2.3) are not checked.

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Verdict method 8 · build 40c109d · generated 2026-10-23 00:15 UTC