AISC 360 — Combined Forces (Chapter H)

Beam-column interaction per AISC 360-16: H1 equations, P-delta, Direct Analysis Method, B1-B2

Most columns in real structures are not loaded in pure compression — they experience simultaneous axial force and bending moments due to frame action, eccentric connections, or lateral loads. Chapter H of AISC 360-16 provides the interaction equations that combine the axial and flexural checks from Chapters E and F into a single utilization ratio. These equations, known informally as the "H1 equations," are the most frequently evaluated check in structural steel design.

1. The H1 Interaction Equations

For doubly symmetric and singly symmetric members subjected to flexure and compression:

H1-1a: When Pr/Pc0.2P_r/P_c \geq 0.2

PrPc+89(MrxMcx+MryMcy)1.0\frac{P_r}{P_c} + \frac{8}{9}\left(\frac{M_{rx}}{M_{cx}} + \frac{M_{ry}}{M_{cy}}\right) \leq 1.0

H1-1b: When Pr/Pc<0.2P_r/P_c < 0.2

Pr2Pc+(MrxMcx+MryMcy)1.0\frac{P_r}{2 P_c} + \left(\frac{M_{rx}}{M_{cx}} + \frac{M_{ry}}{M_{cy}}\right) \leq 1.0

where:

  • PrP_r = required axial strength (factored for LRFD, unfactored for ASD)
  • PcP_c = available axial strength = ϕcPn\phi_c P_n (LRFD) or Pn/ΩcP_n/\Omega_c (ASD)
  • Mrx,MryM_{rx}, M_{ry} = required flexural strength about x and y axes, including second-order effects
  • Mcx,McyM_{cx}, M_{cy} = available flexural strength about x and y axes
The two-equation format avoids an excessively conservative interaction for members with low axial ratios. Equation H1-1b is more lenient on axial force (Pr/2Pc instead of Pr/Pc) but stricter on bending (full addition instead of 8/9 factor). The transition at Pr/Pc = 0.2 ensures continuity.
[DIAGRAM: Interaction diagram showing the bilinear curve. X-axis: Mr/Mc (from 0 to 1), Y-axis: Pr/Pc (from 0 to 1). Two lines: H1-1a from (0, 1.0) to (9/8, 0) and H1-1b from (0, 0.5) to (1.0, 0), meeting at the knee at Mr/Mc ≈ 0.44 and Pr/Pc = 0.2.]

2. Second-Order Analysis Requirements

The MrxM_{rx} and MryM_{ry} in the H1 equations must include second-order effects — the additional moments caused by the axial force acting through the deflected shape. There are two components:

EffectSymbolDescription
P-δ (member effect)PδP \cdot \deltaAxial force × member deflection between ends. Amplifies moments in individual members. Always present.
P-Δ (frame effect)PΔP \cdot \DeltaAxial force × story drift (sway). Amplifies lateral moments. Only in unbraced/sway frames.

2.1. Direct Analysis Method (Chapter C)

The DAM is the preferred method for stability analysis. It directly models the second-order effects in the structural analysis and permits K=1.0K = 1.0 for all members. Requirements:

1. Notional loads: Ni=0.002YiN_i = 0.002 \, Y_i at each level

2. Reduced stiffness: EI=0.8τbEIEI^* = 0.8 \tau_b EI, EA=0.8EAEA^* = 0.8 EA

3. Second-order analysis: P-Δ and P-δ captured automatically

4. Column strength: Use K=1.0K = 1.0 for all compression members

2.2. Approximate B1-B2 Method (Appendix 8)

When rigorous second-order analysis is not available, the B1-B2 method approximates second-order moments from first-order analysis results:

Mr=B1Mnt+B2MltM_r = B_1 M_{nt} + B_2 M_{lt}

where MntM_{nt} = moment from no-translation (gravity) analysis, MltM_{lt} = moment from lateral translation (sway) analysis.

B1 — P-δ amplifier

B1=Cm1αPr/Pe11.0B_1 = \frac{C_m}{1 - \alpha P_r / P_{e1}} \geq 1.0

where Cm=0.60.4(M1/M2)C_m = 0.6 - 0.4(M_1/M_2) for members without transverse loads between supports (M1/M2M_1/M_2 is positive for single curvature), and Pe1=π2EI/(KL)2P_{e1} = \pi^2 EI / (KL)^2with K=1.0K = 1.0 in the DAM. The factor α=1.0\alpha = 1.0 for LRFD and α=1.6\alpha = 1.6 for ASD.

B2 — P-Δ amplifier

B2=11αPr/Pe2B_2 = \frac{1}{1 - \alpha \sum P_r / \sum P_{e2}}

where Pr\sum P_r is the total required vertical load in the story and Pe2\sum P_{e2} is the total story elastic buckling load. When B2>1.5B_2 > 1.5, a rigorous second-order analysis is required — the B1-B2 approximation becomes inaccurate for high amplification.

α = 1.6 for ASD: This is a key difference between LRFD and ASD in second-order analysis. Since ASD uses unfactored loads, multiplying by α = 1.6 brings the loads to an equivalent factored level for the P-Δ check. Forgetting to use α = 1.6 in ASD underestimates the second-order effects and can lead to unconservative designs.

3. Other Sections in Chapter H

H2: Unsymmetric and Other Members

For members not covered by H1 (unsymmetric shapes, biaxial bending with tension):

faFa+fbxFbx+fbyFby1.0\frac{f_a}{F_a} + \frac{f_{bx}}{F_{bx}} + \frac{f_{by}}{F_{by}} \leq 1.0

This stress-based interaction is more general but less refined than the H1 approach.

H3: Members Under Torsion

Section H3 provides interaction equations for members subjected to combined axial force, flexure, and torsion. For round and rectangular HSS:

(PrPc+MrMc)2+(VrVc+TrTc)21.0\left(\frac{P_r}{P_c} + \frac{M_r}{M_c}\right)^2 + \left(\frac{V_r}{V_c} + \frac{T_r}{T_c}\right)^2 \leq 1.0

For open sections (W, C, L), torsion produces warping normal stresses that are added directly to the flexural stresses before checking H1. This typically requires specialized software.

Solved Example — W12×65 Beam-Column

Given: W12×65 (W310×97), A992 (Fy=50F_y = 50 ksi), in a braced frame. Unbraced length: KLx=24KL_x = 24 ft, KLy=12KL_y = 12 ft (braced at midheight for weak axis). Factored forces (LRFD): Pu=267P_u = 267 kips, Mux=147M_{ux} = 147 ft·kips, Muy=24M_{uy} = 24 ft·kips. Members with no transverse loads between supports (Cm applies).

Properties: Ag=19.1A_g = 19.1 in², rx=5.28r_x = 5.28 in, ry=3.02r_y = 3.02 in, Zx=96.8Z_x = 96.8 in³, Zy=44.1Z_y = 44.1 in³, Sx=87.9S_x = 87.9 in³, ry=3.02r_y = 3.02 in, rts=3.40r_{ts} = 3.40 in, J=2.18J = 2.18 in&sup4;, ho=11.9h_o = 11.9 in.

Step 1 — Available Compressive Strength (Pc)

KLrx=24×125.28=54.5\frac{KL}{r_x} = \frac{24 \times 12}{5.28} = 54.5
KLry=12×123.02=47.7\frac{KL}{r_y} = \frac{12 \times 12}{3.02} = 47.7

Strong axis governs (54.5). Transition: 113.4 → inelastic.

Fe=π2×29,00054.52=96.3 ksiF_e = \frac{\pi^2 \times 29{,}000}{54.5^2} = 96.3 \text{ ksi}
Fcr=0.65850/96.3×50=0.6580.519×50=0.799×50=40.0 ksiF_{cr} = 0.658^{50/96.3} \times 50 = 0.658^{0.519} \times 50 = 0.799 \times 50 = 40.0 \text{ ksi}
Pc=ϕcPn=0.90×40.0×19.1=688 kipsP_c = \phi_c P_n = 0.90 \times 40.0 \times 19.1 = 688 \text{ kips}

Step 2 — Available Flexural Strength (Mcx, Mcy)

Strong axis (x):

Mp=50×96.8=4,840 in⋅kips=403.3 ft⋅kipsM_p = 50 \times 96.8 = 4{,}840 \text{ in·kips} = 403.3 \text{ ft·kips}
Lp=1.76×3.02×24.08=128 in=10.7 ftL_p = 1.76 \times 3.02 \times 24.08 = 128 \text{ in} = 10.7 \text{ ft}

With Lb=12L_b = 12 ft for strong axis (assuming lateral bracing at ends only for a 24 ft column with midheight bracing for weak axis), we need to check LTB. Since Lb=24L_b = 24 ft > Lp=10.7L_p = 10.7 ft, LTB applies. For a column with end moments (no transverse loads), Cb=1.0C_b = 1.0 (conservative).

Lr35.3L_r \approx 35.3 ft (from AISC tables). Since Lp<Lb=24<LrL_p < L_b = 24 < L_r → inelastic LTB:

Mnx=1.0[403.3(403.30.7×50×87.9/12)(2410.735.310.7)]M_{nx} = 1.0\left[403.3 - (403.3 - 0.7 \times 50 \times 87.9/12)\left(\frac{24 - 10.7}{35.3 - 10.7}\right)\right]
=403.3(403.3256.3)×0.541=403.379.4=323.9 ft⋅kips= 403.3 - (403.3 - 256.3) \times 0.541 = 403.3 - 79.4 = 323.9 \text{ ft·kips}
Mcx=ϕbMnx=0.90×323.9=291.5 ft⋅kipsM_{cx} = \phi_b M_{nx} = 0.90 \times 323.9 = 291.5 \text{ ft·kips}

Weak axis (y):

No LTB for minor-axis bending (Section F6). Yielding governs:

Mcy=ϕbFyZy=0.90×50×44.1/12=165.4 ft⋅kipsM_{cy} = \phi_b \cdot F_y \cdot Z_y = 0.90 \times 50 \times 44.1 / 12 = 165.4 \text{ ft·kips}

Step 3 — Check Axial Ratio

PrPc=267688=0.3880.2use H1-1a\frac{P_r}{P_c} = \frac{267}{688} = 0.388 \geq 0.2 \quad \rightarrow \text{use H1-1a}

Step 4 — Interaction Check (H1-1a)

PrPc+89(MrxMcx+MryMcy)=0.388+89(147291.5+24165.4)\frac{P_r}{P_c} + \frac{8}{9}\left(\frac{M_{rx}}{M_{cx}} + \frac{M_{ry}}{M_{cy}}\right) = 0.388 + \frac{8}{9}\left(\frac{147}{291.5} + \frac{24}{165.4}\right)
=0.388+0.889×(0.504+0.145)=0.388+0.889×0.649= 0.388 + 0.889 \times (0.504 + 0.145) = 0.388 + 0.889 \times 0.649
=0.388+0.577=0.9651.0    (96.5%)= 0.388 + 0.577 = 0.965 \leq 1.0 \quad \checkmark \;\; (96.5\%)
Result: The W12×65 passes at 96.5% utilization — very efficient. The strong-axis bending dominates the interaction (Mrx/Mcx = 0.504 contributes 45% of the total utilization). If the weak-axis moment increased to 40 ft·kips, the interaction ratio would be: 0.388 + 0.889 × (0.504 + 0.242) = 1.05 → FAILS. The engineer would then need to add weak-axis bracing, increase the column size, or reduce the moment.
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5. International Comparison — Combined Forces

AspectAISC 360Eurocode 3NBR 8800
Interaction equationsH1-1a/b (simple, bilinear)kij method (Annex A or B) — complexH1-1a/b (= AISC)
Number of equations22 (but with kyy, kyz, kzy, kzz factors)2 (= AISC)
Second-orderDAM or B1-B2GNA or amplification factorsDAM or B1-B2
ComplexityLow — suitable for hand calculationHigh — typically requires softwareLow (= AISC)
The AISC H1 equations are elegant in their simplicity: two equations, clear transition, easily programmable. The Eurocode kij method is more precise (accounting for the shape of the moment diagram along the member length) but requires computing 4 interaction factors, each with its own sub-formula — practically impossible by hand. CalcSteel implements both approaches and typically shows 5–15% higher utilization with EC3 for members governed by LTB.
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