CFST Column Design
Concrete-Filled Steel Tube (CFST) — AISC 360-22 Chapter I — Rect/Sq HSS & Round HSS. Compactness classification, Pno, EIeff, axial & flexural strength, P-M interaction diagram.
Concrete-Filled Steel Tube (CFST) — AISC 360-22 Chapter I — Rect/Sq HSS & Round HSS. Compactness classification, Pno, EIeff, axial & flexural strength, P-M interaction diagram.
A Concrete-Filled Steel Tube (CFST) column consists of a hollow steel section — either rectangular/square HSS or circular HSS — filled with plain or reinforced concrete. The steel tube acts as permanent formwork, provides confinement to the core concrete, and resists tension and bending; the concrete core restrains local buckling of the steel wall and carries axial compression.
CFST columns combine the high tensile strength of steel with the compressive strength of concrete, resulting in column strengths that typically exceed the sum of the individual capacities. They are common in high-rise building cores, bridge piers, and industrial structures.
Chapter I of AISC 360-22 governs the design of composite columns. Three cross-section types are covered:
This calculator covers filled composite members (rectangular and circular HSS).
| As | Area of steel section (in² / mm²) |
| Ac | Net area of concrete core (in² / mm²) |
| Es | Modulus of elasticity of steel — 29,000 ksi / 200,000 MPa |
| Ec | Modulus of elasticity of concrete — wc1.5√f'c (ACI 318) |
| Fy | Yield stress of steel (ksi / MPa) |
| f'c | Specified compressive strength of concrete (ksi / MPa) |
| Pno | Nominal compressive strength without length effects |
| Pn | Nominal compressive strength accounting for buckling |
| EIeff | Effective flexural stiffness for buckling calculation |
| C2 | Concrete contribution factor: 0.85 (rect), 0.95 (round) |
The steel wall must be checked for local buckling. AISC 360-22 Table I1.1a defines three compactness categories based on the wall slenderness ratio λ = b/t (rectangular) or D/t (circular), compared to limiting values λp (compact) and λr (noncompact).
| Category | Limit | Formula |
|---|---|---|
| Compact | b/t ≤ λp | λp = 2.26√(Es/Fy) |
| Noncompact | λp < b/t ≤ λr | λr = 3.00√(Es/Fy) |
| Slender | b/t > λr | — |
| Not Permitted | b/t > 5.00√(Es/Fy) | §I1.4a |
Note: b = clear flat width of the longer wall = B − 2t (or H − 2t, whichever governs).
| Category | Limit | Formula |
|---|---|---|
| Compact | D/t ≤ λp | λp = 0.15 Es/Fy |
| Noncompact | λp < D/t ≤ λr | λr = 0.19 Es/Fy |
| Slender | D/t > λr | — |
| Not Permitted | D/t > 0.31 Es/Fy | §I1.4a |
Members that are slender or not-permitted cannot use the filled composite provisions of Chapter I. Slender sections have reduced strength; not-permitted sections exceed the code's calibrated range entirely.
The nominal compressive strength without length effects Pno depends on the compactness class:
Compact (§I2.2a–b):
C2 = 0.85 for rectangular HSS, 0.95 for circular HSS. The higher C2 for circular sections reflects concrete confinement from hoop action.
Noncompact (§I2.2c, Eq. I2-9b):
Pp = FyAs + C2f'cAc (compact strength); Py = FyAs + 0.70f'cAc
Slender (§I2.2d, Eq. I2-9c):
Fcr is the critical buckling stress of the hollow steel section based on b/t (rect) or D/t (circular) per §I2.2d.
The effective flexural stiffness used for the column buckling calculation:
For filled members (no rebar, Isr = 0): C3 = 0.45 + 3(As/Ag), capped at 0.9. EIeff replaces EI in the classic Euler/AISC flexural buckling equations.
The length-dependent compressive strength Pn follows the same slenderness curves as Chapter E, but uses Pno in place of FyAg and EIeff in place of EI:
Design strength: φcPn with φc = 0.75 (LRFD).
The nominal flexural strength for compact filled composite sections is calculated using the Plastic Stress Distribution Method (PSDM). The full plastic moment Mp is found by sweeping the plastic neutral axis (PNA) from the center to the bottom of the section, integrating the rectangular stress block contributions from steel (±Fy) and concrete (C2f'c compression only). The maximum moment on the P-M envelope typically occurs near the balanced point, not at zero axial force.
Unlike the bilinear H1-1 formula used for pure steel members, compact CFST sections are checked against the full PSDM cross-section interaction envelope. The envelope is derived by sweeping the PNA and recording (P, M) at each position, producing a smooth convex curve with five key characteristic points:
| Point | Axial P | Moment M | Description |
|---|---|---|---|
| A | Pp = FyAs + C2f'cAc | 0 | Pure compression (PNA at bottom) |
| B | 0 | Mp | Pure bending (equal compression/tension areas) |
| C | C2f'cAc | Mp | Balanced point — same M as B but concrete compression only |
| D | PA/2 | Mmax ≈ Mp + extra | Maximum moment point |
| E | 0 | 0 | Origin |
For LRFD design, the PSDM envelope is scaled by resistance factors:
The cap at φcPn is critical: for a slender column with Pn < Pno, the design P-axis is cut at the lower value, creating a flat horizontal portion at the top of the envelope.
The demand/capacity ratio is computed as the radial D/C on the φ-scaled PSDM envelope:
If DCR ≤ 1.0, the member is adequate. This approach is more accurate and less conservative than a bilinear H1-1 formula, especially for points near the pure bending or balanced-point region of the envelope.
For rectangular HSS with both Mux and Muy, each axis is checked independently against its own PSDM envelope (x-axis and y-axis envelopes are different for non-square sections). The governing D/C is the maximum of the two:
For circular HSS, the cross-section is symmetric about all axes, so only one envelope is needed regardless of the Mu direction.
Given: Square HSS 10×10, t = 0.500 in, Fy = 46 ksi, f'c = 5.0 ksi, K = 0.65, L = 14 ft, Pu = 600 kips, Mux = 100 kip-ft, Muy = 0.
| As = 4×(10−t)×t = 4×9.5×0.5 | = 19.0 in² |
| Ac = (10−2×0.5)² = 9.0² | = 81.0 in² |
| Ag = 10² | = 100.0 in² |
| ρ = As/Ag | = 19% ✓ (≥1%) |
| λ = b/t = (10−2×0.5)/0.5 | = 18.0 |
| λp = 2.26√(29000/46) | = 56.7 |
| λ < λp → Compact | ✓ |
| C2 (rectangular) | = 0.85 |
| FyAs = 46 × 19.0 | = 874 kips |
| C2f'cAc = 0.85 × 5.0 × 81.0 | = 344 kips |
| Pno | = 1218 kips |
| Is (HSS 10×10×½) | ≈ 170 in⁴ (4 plates about centroid) |
| Ic = 9⁴/12 = 6561/12 | ≈ 547 in⁴ |
| Ec = 33×wc1.5√f'c ≈ 33×1451.5×√5 | ≈ 4074 ksi |
| C3 = 0.45 + 3×(19/100) = 0.45+0.57 | = 0.90 (capped) |
| EIeff = 29000×170 + 0.90×4074×547 | ≈ 6,930,000 kip·in² |
| KL = 0.65 × 14 × 12 = 109.2 in | |
| Pe = π²×EIeff/(KL)² | ≈ 5,715 kips |
| Pno/Pe = 1218/5715 | = 0.213 < 2.25 → inelastic |
| Pn = 1218 × 0.6580.213 | ≈ 1104 kips |
| φcPn = 0.75 × 1104 | = 828 kips |
The plastic moment Mp is found by PSDM with the PNA at mid-height (equal areas). For a 10×10×½ square HSS filled with f'c = 5 ksi, Mp ≈ 525 kip·ft. The PSDM envelope is swept numerically and the φ-scaled envelope is formed with φc = 0.75 (P-axis, capped at 828 kips) and φb = 0.90 (M-axis).
| Pu = 600 kips, Mux = 100 kip-ft = 1200 kip-in | |
| Ray direction: (M, P) = (1200, 600) | |
| Intersection with φ-PSDM envelope | ≈ (Mcap, Pcap) |
| DCR = |demand| / |intersection| | ≈ 0.83 (OK ✓) |
Note: exact values depend on the full swept PSDM curve — use the calculator above to obtain the precise DCR.