Radius of Gyration (r) — Definition, Formula & Column Buckling
The radius of gyration (r) is a geometric property defined as the square root of the ratio of moment of inertia to cross-sectional area:
r = sqrt(I / A)
Physically, r represents the distance from the centroidal axis at which the entire area A could be concentrated (as a thin ring) and still produce the same moment of inertia I. It is a measure of how efficiently a cross-section distributes its material relative to its centroid — the larger r is for a given area, the more buckling-resistant the section.
The radius of gyration is the single most important parameter governing column compressive strength, as it appears in the slenderness ratio KL/r that controls elastic and inelastic buckling behavior across all major design codes.
Physical Interpretation
PRELIMINARY — NOT FOR CONSTRUCTION. All content is for educational and reference use only. Must be independently verified by a licensed Professional Engineer (PE) or Structural Engineer (SE) before use in any project.
Consider two sections with the same cross-sectional area A = 10 in^2:
| Section | Ix (in^4) | rx (in) | Comment |
|---|---|---|---|
| Solid square 3.16" x 3.16" | 8.33 | 0.913 | Material concentrated near centroid |
| W10x33 (approximate) | 170 | 4.12 | Material distributed in flanges |
Both sections have the same area and weight. But the W-shape has a radius of gyration 4.5x larger, resulting in a slenderness ratio 4.5x smaller and dramatically higher column capacity. This illustrates why structural steel shapes (I-beams, HSS tubes) are far more efficient for columns than solid sections of equivalent weight.
Formulas for Common Shapes
Rectangle
I = b * d^3 / 12
A = b * d
r = sqrt(I/A) = sqrt(b * d^3 / (12 * b * d)) = d / sqrt(12) = 0.289 * d
Circle
I = pi * D^4 / 64
A = pi * D^2 / 4
r = sqrt(I/A) = sqrt((pi*D^4/64) / (pi*D^2/4)) = D / 4
Thin-Walled Tube (HSS Round)
I = pi * R^3 * t (approximate, R = mean radius)
A = 2 * pi * R * t
r = sqrt(I/A) = sqrt(pi * R^3 * t / (2 * pi * R * t)) = R / sqrt(2) âÃÂà0.707 * R
I-Shape (W, UB, UC)
rx = sqrt(Ix / A) (strong-axis radius of gyration)
ry = sqrt(Iy / A) (weak-axis radius of gyration)
For standard rolled shapes, rx and ry are tabulated in the AISC Manual. Weak-axis (ry) typically governs column design because it produces the larger slenderness ratio.
Radius of Gyration — Common W-Shapes (AISC)
| Section | A (in^2) | Ix (in^4) | Iy (in^4) | rx (in) | ry (in) | rx/ry | Weight (plf) |
|---|---|---|---|---|---|---|---|
| W8x10 | 2.94 | 30.8 | 2.08 | 3.24 | 0.841 | 3.85 | 10 |
| W8x31 | 9.13 | 110 | 37.1 | 3.47 | 2.02 | 1.72 | 31 |
| W10x26 | 7.63 | 144 | 19.0 | 4.35 | 1.58 | 2.75 | 26 |
| W10x49 | 14.4 | 272 | 93.4 | 4.35 | 2.55 | 1.71 | 49 |
| W12x26 | 7.65 | 204 | 17.3 | 5.17 | 1.51 | 3.42 | 26 |
| W12x50 | 14.7 | 394 | 56.3 | 5.18 | 1.96 | 2.64 | 50 |
| W14x22 | 6.49 | 199 | 7.00 | 5.54 | 1.04 | 5.33 | 22 |
| W14x48 | 14.1 | 485 | 51.4 | 5.87 | 1.91 | 3.07 | 48 |
| W14x90 | 26.5 | 999 | 362 | 6.14 | 3.70 | 1.66 | 90 |
| W18x55 | 16.2 | 890 | 44.9 | 7.41 | 1.67 | 4.44 | 55 |
| W21x44 | 13.0 | 843 | 20.7 | 8.06 | 1.26 | 6.40 | 44 |
| W24x55 | 16.2 | 1350 | 29.1 | 9.13 | 1.34 | 6.81 | 55 |
| W30x99 | 29.1 | 3990 | 128 | 11.7 | 2.10 | 5.57 | 99 |
Key observation: rx/ry ratios of 1.7 to 6.8 show how dramatically W-shapes differ between strong and weak axes. For unbraced columns, the weak axis (ry) nearly always controls. A column 20 ft tall with KL = 20 ft has:
- KL/rx = 240/11.7 = 20.5 (W30x99, strong axis)
- KL/ry = 240/2.10 = 114 (W30x99, weak axis)
The weak-axis slenderness ratio is 5.6x larger and will produce a substantially lower buckling capacity.
Role in Column Buckling — Slenderness Ratio
The slenderness ratio KL/r is the universal parameter governing column compressive strength. All major design codes base their column strength curves on KL/r (or the equivalent non-dimensional slenderness).
AISC 360 Chapter E — Column Strength
Elastic buckling stress (Euler):
Fe = pi^2 * E / (KL/r)^2
Critical stress Fcr:
When KL/r <= 4.71*sqrt(E/Fy) = 113 (Fy = 50 ksi):
Fcr = (0.658^(Fy/Fe)) * Fy (inelastic buckling)
When KL/r > 113:
Fcr = 0.877 * Fe (elastic buckling)
AS 4100 Section 6 — Column Strength
The modified slenderness lambda_n is:
lambda_n = (KL/r) * sqrt(kf) * sqrt(Fy/250)
The member slenderness reduction factor alpha_c depends on lambda_n and the section constant alpha_b.
EN 1993-1-1 Clause 6.3.1
Non-dimensional slenderness:
lambda_bar = sqrt(A*fy / Ncr)
Ncr = pi^2 * E * I / (KL)^2
lambda_bar = (KL/r) / (pi * sqrt(E/fy))
The reduction factor chi is determined from the appropriate buckling curve (a0, a, b, c, d).
Effect of r on Column Capacity — W12x50 Example
A 15-ft tall W12x50 column (Fy = 50 ksi):
| Axis | r (in) | KL/r | Fcr (ksi) | phiPn (kips) |
|---|---|---|---|---|
| Strong (x) | 5.18 | 34.7 | 45.6 | 605 |
| Weak (y) | 1.96 | 91.8 | 30.1 | 399 |
If the column is unbraced in the weak direction, capacity drops 34% to 399 kips. Providing weak-axis bracing at mid-height (Ky*Ly = 7.5 ft, KL/ry = 45.9) restores capacity to 610 kips.
Design Implications
1. Weak-Axis Governs for Unbraced Columns
Unless bracing is provided in both directions, ry (weak axis) will produce the controlling slenderness ratio. A column that is equally unbraced in both directions will buckle about the weak axis.
2. rx/ry Ratio Guides Bracing Requirements
Sections with high rx/ry ratios (like W21x44 at 6.40) require weak-axis bracing at much closer intervals than strong-axis bracing. If the column height is H:
- Strong-axis unbraced length: Kx * Lx = H (braced at top and bottom)
- Weak-axis unbraced length: Ky _ Ly <= H _ (ry/rx) to make slenderness ratios equal
3. HSS Sections Are Balanced
Square HSS sections have rx = ry, making them equally efficient in both directions. This simplifies bracing requirements and makes them attractive for free-standing columns.
4. Built-Up Sections Can Optimize r
Lacing, batten plates, or perforated cover plates can increase the radius of gyration of built-up columns while adding minimal weight.
Frequently Asked Questions
What is radius of gyration? Radius of gyration r = sqrt(I/A) measures how a cross-section's area is distributed relative to its centroid. A larger r means material is farther from the center, providing greater buckling resistance for the same cross-sectional area.
How does radius of gyration affect column design? r appears in the slenderness ratio KL/r, which controls buckling capacity. For a column of given length, doubling r halves the slenderness ratio and dramatically increases compressive strength. The weak-axis r (ry) typically governs design for unbraced W-shape columns.
What is a good radius of gyration for a column? For a 12-ft column, a minimum ry of 1.5-2.0 in (KL/ry ~ 72-96) is typical for W-shapes, yielding reasonable efficiency. For taller columns, select sections with larger ry or provide intermediate bracing. W14 sections offer the best rx/ry balance; W8 and W10 sections are more square-shaped with better weak-axis properties.
How do I calculate radius of gyration? For standard rolled sections, use tabulated r values from the AISC Manual Table 1-1 (rx and ry columns). For custom shapes, compute I (moment of inertia) and A (area), then r = sqrt(I/A). The calculation accounts for the entire cross-section including fillets.
Related Terms and Pages
- Effective Length Factor — K Factor Guide
- Compact Section — Definition & Limits
- Plastic Modulus — Definition & Formula
- Lateral Torsional Buckling — LTB Explained
- Column Capacity Calculator — Free Online Tool
- Column Design Guide — AISC 360
- Column Buckling Equations
- Section Properties Database
Educational reference only. Radius of gyration values should be taken from the governing design standard (AISC Manual Table 1-1) for final design. All column designs must be independently verified by a licensed Professional Engineer.
Disclaimer: This content is for educational purposes only. Results must be verified by a licensed professional engineer. Steel Calculator provides preliminary design tools — NOT a substitute for professional engineering judgment.