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

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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) ≈ 0.707 * 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:

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:

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


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.