Bracing Connection Calculator (Gusset Plate)

Design a bracing connection - a brace member bolted to a gusset plate welded to the main member - to Eurocode 3 (EN 1993-1-8) with SCI P358. The calculator verifies the gusset plate in tension (gross-section yield and net-section rupture), the Whitmore effective-width section, the brace-to-gusset bolt group (shear and bearing) and the gusset-to-member fillet weld (two runs at their connection angles), each with its utilisation and a clear PASS/FAIL on an interactive 3D model.

Free online calculator with step-by-step working and one-click Excel (.xlsx) and PDF export.

Using this bracing connection calculator

What it checks

A bracing connection transfers axial force from a brace member into a gusset plate and then into the frame. This calculator verifies the gusset plate in gross-section yielding and net-section rupture, the bolt group in shear and bearing, block tearing and tear-out, the weld to the supporting members, and the Whitmore section - the effective width of gusset that actually carries the brace force.

Bracing is an axial connection, so unlike a beam shear connection there is no eccentricity moment to resolve, but there are more ways for the plate to fail: a gusset can rupture on the net section, tear out a block of material around the bolt group, or buckle over the Whitmore width if the brace is in compression.

Net section, not gross section, governs

Running the tool on its defaults - a 120 by 400 by 10 mm S275 gusset with three M24 grade 8.8 bolts carrying 80 kN - gives:

Gusset, net-section rupture
291.0 kN, utilisation 0.275 - GOVERNS
Gusset, gross-section yielding
330.0 kN, utilisation 0.242
Bolt group
406.7 kN, utilisation 0.197
Weld
438.5 kN, utilisation 0.183
Whitmore section
582.1 kN, utilisation 0.137

Net-section rupture governs even though its resistance in kN is not the lowest number in a naive reading - the gross section yields at 330 kN and the net section ruptures at 291 kN, so the net section is the real limit. That is the usual outcome for a bolted gusset: drilling holes removes material exactly where the force is highest.

The consequence is that gusset design is driven by hole layout, not plate size. Staggering the bolts, or spreading them over more rows so the net width at any one section is larger, buys more capacity than making the plate wider or thicker.

The Whitmore section

The Whitmore section is the effective width of gusset that actually resists the brace force - conventionally taken by spreading 30 degrees each side from the first row of bolts to the last. Material outside that spread contributes little, so a very wide gusset does not help beyond the Whitmore width.

It matters most for a brace in compression, where the gusset can buckle over that effective width as a short column. With a tension brace the Whitmore check is usually comfortable - 582 kN against 291 kN net section in the example above - but a compression brace with a long unsupported gusset can make it the governing mode.

Formula reference

Gross-section yielding
Npl,Rd=AfyγM0N_{pl,Rd} = \dfrac{A\,f_y}{\gamma_{M0}}
Net-section rupture
Nu,Rd=0.9AnetfuγM2N_{u,Rd} = \dfrac{0.9\,A_{net}\,f_u}{\gamma_{M2}}
Block tearing
Veff,Rd=fuAntγM2+fyAnv3γM0V_{eff,Rd} = \dfrac{f_u A_{nt}}{\gamma_{M2}} + \dfrac{f_y A_{nv}}{\sqrt3\,\gamma_{M0}}
Bolt shear
Fv,Rd=αvfubAsγM2F_{v,Rd} = \dfrac{\alpha_v f_{ub} A_s}{\gamma_{M2}}
Bearing
Fb,Rd=k1αbfudtγM2F_{b,Rd} = \dfrac{k_1 \alpha_b f_u d t}{\gamma_{M2}}
Whitmore effective width
bw=b+2Ltan30b_w = b + 2\,L\tan 30^\circ
Design weld strength
fvw,d=fuβwγM2f_{vw,d} = \dfrac{f_u}{\beta_w\,\gamma_{M2}}

Assumptions and limits

The brace force is assumed concentric with the bolt group, so no eccentricity moment is applied to the gusset. Where the brace centreline does not pass through the working point of the frame, the resulting moment is a real effect this tool does not model, and it can be significant on a shallow-angle brace.

Gusset buckling under a compression brace is addressed only through the Whitmore section check. A long, thin or unsupported gusset edge may need a proper stability check, and free-edge stiffening is a detailing decision the tool does not make.

The tool checks the gusset and its fasteners, not the brace member itself, not the beam or column it frames into, and not the frame action. Static persistent design situation; fatigue, fire and seismic detailing - including the capacity-design requirements that govern a seismic brace - are outside the scope.

FAQ

Because the two use different strengths and different partial factors: gross-section yielding uses f_y with gamma_M0, net-section rupture uses 0.9 A_net f_u with gamma_M2. In the example the net section comes out at 291 kN against 330 kN gross, so the holes control.

Improve the hole layout before the plate size. Staggering the bolts or adding a row so the net width at any one cross-section is larger addresses the governing mode directly. Making the plate thicker helps both modes but is less efficient.

It defines the width of gusset that actually carries the brace force, spreading 30 degrees each side from the first bolt row. Plate outside that width contributes little, and for a compression brace the gusset can buckle over it.

Partly. The Whitmore check addresses gusset stability over the effective width, but a long or unstiffened free edge may need a separate buckling assessment that this tool does not perform.

No. The model assumes the brace force is concentric with the bolt group. If your geometry forces the brace centreline away from the working point, the resulting moment on the gusset and on the frame is real and must be assessed separately.

Not on its own. Seismic bracing is governed by capacity design - the connection must be stronger than the yielding brace and must accommodate its inelastic rotation - which is a different design basis from the static checks here.

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