Bolt Group Calculator: Accurate Pattern, Load & Force Distribution Analysis

Analyze bolt group patterns, load distribution, and force effects with our accurate calculator. Perfect for steel connections and structural design.
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The Bolt Group Calculator is a powerful, free structural engineering tool for designing and checking bolted connections subjected to eccentric shear loads and moment. It supports both the Elastic Method (conservative, linear) and the Instantaneous Center (IC) Method (plastic, more economical), along with AISC 360 LRFD/ASD and Eurocode 3.

Key features include:

  • Quick rectangular, circular, or linear bolt pattern generator
  • Custom bolt coordinate entry with automatic centroid calculation
  • Per-bolt force distribution (direct shear + torsional shear)
  • Shear capacity, bearing capacity, and shear-tension interaction checks
  • Real-time force vector diagram showing safe/warning/overstressed bolts
  • Full support for Imperial (in/kips) and Metric (mm/kN) units

Ideal for steel connection design, this tool handles any irregular bolt layout and provides clear summary cards, detailed tables, and exportable results for documentation. Perfect for structural engineers and students.

Bolt Group Calculator

Eccentrically Loaded Bolt Groups — Elastic Method & IC Method

SteelSolver Toolbox • AISC 360 • Eurocode 3
Unit System & Design Method
Imperial (in, kips)
Metric (mm, kN)
Bolt Pattern Generator

Quick Pattern Generator

# X (in) Y (in) Label
Enter bolt X/Y coordinates relative to any reference point — the centroid is computed automatically.
Applied Loads & Eccentricity
Horizontal shear force
Vertical shear force
Horizontal eccentricity
Vertical eccentricity
Additional direct moment
Perpendicular tension
Bolt Properties
Plate / Member Properties

Enter inputs and click Calculate Bolt Group to see results.

Bolt Group Visualization — Force Vector Diagram
Calculate first to see force vectors. Bolt colors: Green = safe, Yellow = warning (>80%), Red = overstressed. ◯ = Centroid. Arrow length proportional to resultant force.
Run calculation to see bolt group diagram
Safe (DCR < 0.8) Warning (0.8–1.0) Overstressed (> 1.0) Centroid Resultant force vector
Formulas Used in Calculations
All formulas follow AISC 360 Section J3 — Elastic Method (conservative). IC Method follows AISC Table 7-6 approach.
1 Centroid of Bolt Group

The geometric centroid (center of gravity) of the bolt group is computed assuming equal-area bolts:

Centroid
$$\bar{x} = \frac{\sum_{i=1}^{n} x_i}{n}, \qquad \bar{y} = \frac{\sum_{i=1}^{n} y_i}{n}$$

All bolt coordinates are then shifted to centroidal axes: \( x'_i = x_i - \bar{x} \), \( y'_i = y_i - \bar{y} \).

2 Polar Moment of Inertia (J)

The polar moment of inertia of the bolt group (assuming unit bolt area) resists torsional moment:

Polar Moment of Inertia
$$J = I_p = \sum_{i=1}^{n} r_i^2 = \sum_{i=1}^{n} \left[(x'_i)^2 + (y'_i)^2\right]$$
where \( r_i = \sqrt{(x'_i)^2 + (y'_i)^2} \) is the distance from centroid to bolt \(i\).
3 Moment from Eccentricity

When the load does not pass through the centroid, an in-plane moment (torsion) is generated:

Eccentricity-Induced Moment
$$M_z = V_y \cdot e_x + V_x \cdot e_y + M_{z,\text{direct}}$$

Positive moment convention: counter-clockwise. \(e_x\) and \(e_y\) are eccentricities in x and y directions.

4 Direct Shear Per Bolt

The direct shear is divided equally among all bolts (concentric loading component):

Direct Shear Components
$$V_{dx} = \frac{V_x}{n}, \qquad V_{dy} = \frac{V_y}{n}$$
5 Torsional (Moment-Induced) Shear Per Bolt

The in-plane moment creates torsional shear on each bolt, perpendicular to the radius vector:

Torsional Shear (Elastic Method)
$$V_{mx,i} = \frac{M_z \cdot y'_i}{J}, \qquad V_{my,i} = \frac{-M_z \cdot x'_i}{J}$$

The sign convention ensures the torsional shear acts tangentially (perpendicular to \(r_i\)).

6 Resultant Force Per Bolt

Superpose direct and moment-induced components vectorially:

Resultant Shear
$$V_x^{(i)} = V_{dx} + V_{mx,i}, \qquad V_y^{(i)} = V_{dy} + V_{my,i}$$ $$V_{res,i} = \sqrt{\left(V_x^{(i)}\right)^2 + \left(V_y^{(i)}\right)^2}$$

The critical bolt is the one with the maximum \(V_{res,i}\).

7 Bolt Shear Capacity (AISC LRFD)
LRFD Shear Capacity
$$\phi R_n = \phi \cdot F_{nv} \cdot A_b \cdot n_{s}$$ where \(\phi = 0.75\), \(F_{nv}\) = nominal shear stress (ksi), \(A_b\) = bolt area (in\(^2\)), \(n_s\) = number of shear planes.

ASD Shear Capacity
$$\frac{R_n}{\Omega} = \frac{F_{nv} \cdot A_b \cdot n_s}{\Omega}, \quad \Omega = 2.00$$
Demand-to-Capacity Ratio (DCR / Utilization)
$$\text{DCR}_i = \frac{V_{res,i}}{\phi R_n} \leq 1.0$$
8 Bearing Capacity (Plate Check)
AISC J3-6a Bearing Capacity
$$\phi R_n = \phi \cdot \min\!\left(1.2\, L_c\, t\, F_u,\; 2.4\, d\, t\, F_u\right)$$ When deformation is a design consideration, use \(C = 2.4\) (replaces \(3.0\) in the lower bound): $$\phi R_n = \phi \cdot \min\!\left(1.2\, L_c\, t\, F_u,\; 2.4\, d\, t\, F_u\right), \quad \phi = 0.75$$
9 Shear-Tension Interaction (Combined Loading)
AISC LRFD Interaction (J3-3a)
$$F'_{nt} = 1.3 F_{nt} - \frac{F_{nt}}{\phi F_{nv}} f_v \leq F_{nt}$$ $$\phi R_n^{\text{combined}} = \phi \cdot F'_{nt} \cdot A_b$$
Simplified Linear Interaction
$$\left(\frac{V_{res}}{V_{cap}}\right)^2 + \left(\frac{T_u}{T_{cap}}\right)^2 \leq 1.0$$
What Is a Bolt Group Calculator?

A Bolt Group Calculator analyzes the force distribution across multiple bolts in a connection subjected to combined shear and moment loads — especially eccentric loads where the resultant force line doesn't pass through the centroid of the bolt group. Such loading generates both direct shear (shared equally) and torsional shear (proportional to distance from centroid), making manual calculation tedious and error-prone.

⚠ User Pain Points This Tool Solves

Tedious Iterations IC Method requires iterative equilibrium checks — automated here.
Irregular Patterns AISC tables only cover standard grids. This tool handles any layout.
No Visual Feedback Force vector diagram shows each bolt's load direction and magnitude.
Code Compliance LRFD/ASD capacity checks with resistance factors built-in.

✅ Quick Start Guide

  1. Choose unit system (Imperial or Metric) and design method (Elastic or IC).
  2. Select design code (AISC LRFD, ASD, or Eurocode 3).
  3. Define the bolt pattern using the generator or enter custom X/Y coordinates.
  4. Enter applied shear forces (Vx, Vy) and eccentricities (ex, ey).
  5. Set bolt diameter, grade, and shear planes.
  6. Enter plate properties for bearing check (optional).
  7. Click Calculate Bolt Group and review Results & Diagram tabs.
  8. Export CSV or print PDF for documentation.

📊 Elastic vs IC Method

Feature Elastic Method IC Method (Plastic)
ComplexityLowHigh (iterative)
ConservatismConservativeMore economical
Code basisAISC §JAISC Tables 7-6 to 7-13
Irregular patterns✓ Supported✓ Supported
Best forQuick checksOptimized design
Accuracy Note: This calculator implements the Elastic Method per AISC 360. Results should be verified by a licensed professional engineer for structural applications. Always confirm material properties and loading conditions against project specifications.

⚛ More SteelSolver Tools

Explore our complete structural engineering toolbox — free, fast, and code-compliant.

⚛ SteelSolver Toolbox • Complete User Guide

Bolt Group Calculator: Complete User Guide — Formulas, Steps & Examples

A step-by-step reference for structural engineers, designers, and students using the Bolt Group Calculator to analyze eccentrically loaded bolt connections per AISC 360, Eurocode 3, and ASD/LRFD design codes.

AISC 360 Eurocode 3 LRFD & ASD Elastic Method IC Method MathJax Formulas Imperial & Metric

What Is a Bolt Group Calculator? — Definition & Purpose

A bolt group calculator (also called a bolt pattern calculator, bolt connection calculator, or bolt force distribution calculator) is a specialized structural engineering tool used to analyze groups of high-strength fasteners in a bolted joint subjected to combined shear, tension, and in-plane moment loading.

In real-world steel connection design, loads rarely pass through the centroid of the bolt group. When a shear force is applied at an offset (eccentricity), it generates both a direct shear component distributed equally across all bolts and a torsional moment that creates additional shear forces proportional to each bolt's distance from the group centroid. This combination is what makes eccentric bolt group analysis complex and critical to get right.

The SteelSolver Bolt Group Calculator automates this entire process — from centroid computation and polar moment of inertia to per-bolt resultant forces, demand-to-capacity ratios (DCR), and code-based capacity checks per AISC 360, Eurocode 3, LRFD, and ASD — in seconds.

💡
When do you need a bolt group calculator? Anytime the resultant of your applied loads does not pass through the centroid of the bolt group — bracket connections, shear tabs, base plate anchor bolt groups, beam-to-column eccentric connections, and machinery mounts all require this analysis.

Key User Pain Points & How This Calculator Solves Them

Manual bolt group load distribution calculations expose engineers to several high-risk failure points. Here is how the SteelSolver Bolt Group Calculator directly addresses each one:

📊

Tedious Iterative Manual Calculations

The Instantaneous Center of Rotation (IC) method requires guessing a center point, computing bolt deformations, checking force equilibrium, and iterating — a process that can take hours per connection.

✓ Automated convergence algorithm solves the IC method in milliseconds, showing all intermediate results.
📐

Geometric Complexity & Human Error

Computing the polar moment of inertia (J = Σr²) and individual bolt distances for irregular, circular, or asymmetric bolt patterns is highly error-prone by hand.

✓ Auto-centroid computation and J calculation for any geometry — grid, circular, linear, or fully custom coordinate input.
📚

AISC Table Limitations

AISC Manual Tables 7-6 to 7-13 only cover standard rectangular patterns and discrete eccentricities. Non-standard bolt spacings or custom layouts require interpolation or full manual analysis.

✓ Handles any bolt layout with any eccentricity or load angle — not limited to tabulated configurations.
🔐

Code Compliance Confusion (LRFD vs ASD)

Staying aligned with AISC 360, Eurocode 3, and choosing between LRFD (φ = 0.75) and ASD (Ω = 2.00) for bolt shear capacity checks adds another layer of complexity.

✓ Toggle between AISC LRFD, ASD, and Eurocode 3 — resistance factors are applied automatically.
👁

No Visual Feedback on Force Direction

Without a visualization, it is impossible to quickly verify that torsional shear vectors are acting in the correct direction for each bolt — especially in irregular groups.

✓ Live SVG force vector diagram shows directional arrows scaled to resultant magnitude, color-coded by utilization ratio.
📊

No Bearing Capacity or Interaction Check

Many free bolt group tools only calculate shear — ignoring bearing capacity on the connected plate (AISC J3-6a) and shear-tension interaction, which can govern the design.

✓ Full bearing check per AISC J3-6a and combined shear-tension interaction formula included in results.

Visual: Annotated Eccentrically Loaded Bolt Group Diagram

The diagram below illustrates a 2×3 rectangular bolt pattern subjected to an eccentric vertical load (P), demonstrating the decomposition into direct shear and torsional shear components. This is the foundational concept behind all bolt group shear and moment distribution calculations.

BOLT GROUP CALCULATOR Eccentrically Loaded Bolt Group — Force Vector Decomposition (Elastic Method) AISC 360 | LRFD GUSSET / CONNECTION PLATE C.G. (centroid) (x̄, ȳ) B1 Vᵣ⁴₁ B2 B3 ★ CRITICAL B4 B5 B6 P (Applied Load) eₓ (eccentricity) Mₜ = P × eₓ (Torsional moment) sₓ (gage) sᵥ (pitch) rᵢ LEGEND Direct shear (V/n) Torsional shear (M·r/J) Resultant force Vᵣₖₛ Centroid (C.G.) STATUS (DCR) Safe (< 0.80) Warning (0.80–1.0) Overstressed (>1.0) ELASTIC METHOD Vᵢ direct = V / n Vᵌₓ = Mₜ · yʹᵢ / J Vᵌᵥ = −Mₜ · xʹᵢ / J J = Σ(xʹ² + yʹ²) Vᵣₖₙ = √(Vₓ² + Vᵥ²) DCR = Vᵣₖₙ / ϕRₙ

ⓘ Figure 1: 2×3 bolt group with eccentric vertical load P at distance eₓ from centroid. Blue = direct shear, green = torsional shear, orange dashed = resultant. B3 (top-right) is the critical bolt with highest demand-to-capacity ratio (DCR).

Input Parameters — Complete Reference with Units & Validation

The table below lists every input parameter accepted by the Bolt Group Calculator, along with the unit (Imperial and Metric), expected range, and validation note. Always verify your units before computing — unit mismatch is the most common source of error in bolt group load distribution analysis.

Parameter Symbol Unit (Imperial) Unit (Metric) Typical Range Validation / Note
Bolt X Coordinate xᵢ inches (in) millimeters (mm) Any real number Reference frame can be arbitrary — centroid is auto-computed
Bolt Y Coordinate yᵢ inches (in) millimeters (mm) Any real number At least 2 bolts required for group analysis
Horizontal Shear Vₓ kips kN Any value; 0 if not applied Positive = rightward by convention
Vertical Shear Vᵥ kips kN Any value; 0 if not applied Positive = upward; most common applied load
Horizontal Eccentricity eₓ inches (in) mm 0 to ∼36 in typical Distance from load line to centroid; creates Mₜ = Vᵥ × eₓ
Vertical Eccentricity eᵥ inches (in) mm 0 to ∼12 in typical Adds Mₜ += Vₓ × eᵥ
Direct Applied Moment Mₜ,add kip-in kN·mm 0 unless additional couple Added to eccentricity-induced moment
Axial Tension T kips kN 0 to bolt tension capacity Shared equally; triggers shear-tension interaction check
Bolt Diameter dᵇ inches (1/2" to 1-1/8") M12 to M36 (auto-convert) 0.25 in to 2.0 in Must match grade availability; area Aᵇ = πdᵇ²/4
Bolt Grade / Class Fᵗᵟ A307, A325-N/X, A490-N/X (ksi) 8.8, 10.9, 12.9 (MPa) Fᵗᵟ = 27 to 84 ksi Thread condition (N vs X) changes Fᵗᵟ — verify with fastener spec
Shear Planes nᵡ 1 or 2 (dimensionless) 1 or 2 1 = single shear; 2 = double Double shear doubles bolt capacity; verify connection geometry
Plate Thickness t inches (in) mm 0.25 in to 2 in Used in bearing capacity check per AISC J3-6a
Plate Ultimate Strength Fᵘ ksi MPa 58 ksi (A36), 65 ksi (A572-50) Governs bearing capacity; use minimum Fᵘ of connected parts
Clear Edge Distance Lᶜ inches (in) mm Min 1.5dᵇ per AISC J3.10 Measured from edge of bolt hole to nearest edge/hole
Design Code AISC LRFD / ASD Eurocode 3 Toggle Sets resistance factor (φ) or safety factor (Ω) automatically
Unit Consistency Warning: Switch the unit toggle before entering any values. Mixing Imperial (kips, inches) and Metric (kN, mm) inputs without using the toggle will produce incorrect force distributions and capacity checks.

Step-by-Step User Guide: How to Use the Bolt Group Calculator

Follow these 10 steps to correctly perform a complete bolt group shear and tension analysis — from selecting units to interpreting the traffic-light utilization output.

  1. 1

    Choose Your Unit System & Design Method

    Toggle between Imperial (kips, in, ksi) and Metric (kN, mm, MPa) using the unit switch in the Inputs tab. Then select your analysis method: Elastic Method (faster, conservative) or IC Method (plastic analysis, more economical). Finally, choose your design code: AISC 360 LRFD, AISC 360 ASD, or Eurocode 3.

    💡 Do this first — changing units after entering data does not automatically convert existing values.
  2. 2

    Define the Bolt Pattern Geometry

    Use the Quick Pattern Generator to auto-populate coordinates for common configurations:

    • Rectangular Grid — Set rows, columns, horizontal spacing (gauge sᵥ), vertical spacing (pitch sᵧ)
    • Circular Pattern — Set bolt circle radius, number of bolts, start angle
    • Linear (H or V) — Single row/column, number of bolts, spacing
    • Custom — Enter X/Y coordinates manually for irregular layouts (anchor bolt groups, base plate patterns)

    Click Generate Pattern to populate the coordinates table. You can also add, edit, or delete individual bolts in the table.

    💡 Minimum spacing per AISC J3.3 = 2⅔ × bolt diameter (recommended: 3d). Minimum edge distance per AISC Table J3.4 = 1.25d to 1.75d depending on edge type.
  3. 3

    Enter Applied Loads & Eccentricity

    Input the shear forces Vₓ (horizontal) and Vᵥ (vertical) in kips or kN. Then enter the eccentricities:

    • eₓ — Horizontal distance from load line to bolt group centroid (most common for bracket connections)
    • eᵥ — Vertical distance (for loads offset vertically from centroid)
    • Mₜ,direct — Any additional in-plane torsional couple beyond V×e
    • T (Axial) — Out-of-plane tension (activates shear-tension interaction check)

    The calculator auto-computes total moment: Mₜ = Vᵥ×eₓ + Vₓ×eᵥ + Mₜ,direct

    Common mistake: Entering eccentricity from the face of the column/support instead of from the bolt group centroid. Always measure e from the centroid (computed in Step 4).
  4. 4

    Specify Bolt Properties

    Select bolt diameter from the dropdown (1/2" to 1-1/8", or custom). Then choose bolt grade and thread condition:

    • A325-N — Threads included in shear plane, Fᵗᵟ = 54 ksi (most common in US practice)
    • A325-X — Threads excluded, Fᵗᵟ = 68 ksi (higher capacity)
    • A490-N/X — High-strength bolts, Fᵗᵟ = 68/84 ksi
    • Grade 8.8 / 10.9 — Metric equivalents for Eurocode 3 design

    Select Single or Double Shear — double shear doubles the bolt capacity since two shear planes resist the load.

    Critical: Never use A325 nominal strength values for A490 bolts or vice versa. The difference is 26–35% in shear capacity — an error that directly leads to unsafe connection designs.
  5. 5

    Enter Plate / Member Properties (Bearing Check)

    Input the connected plate thickness t, yield strength Fᵥ, and ultimate strength Fᵘ for bearing capacity verification. Enter the clear edge distance Lᶜ (from edge of bolt hole to nearest material edge) — this controls whether the 1.2LᶜtFᵘ or 2.4dtFᵘ limit governs.

    Toggle Deformation at Bolt Holes: if deformation is a design concern, the upper bound changes from 3.0 to 2.4 (more conservative, per AISC J3-6a).

  6. 6

    Click "Calculate Bolt Group"

    Press the orange Calculate Bolt Group button. The engine performs the following computations in sequence:

    1. Centroid computation: ̅x = Σxᵢ/n, ̅y = Σyᵢ/n
    2. Relative coordinates: x'ᵢ = xᵢ − ̅x, y'ᵢ = yᵢ − ̅y
    3. Polar moment of inertia: J = Σ(x'ᵢ² + y'ᵢ²)
    4. Total moment: Mₜ = Vᵥ×eₓ + Vₓ×eᵥ + Mₜ,add
    5. Direct + torsional shear per bolt (vector components)
    6. Resultant force per bolt: Vᵣₖₙ = √(Vₓ² + Vᵥ²)
    7. Bolt capacity check: φRₙ or Rₙ/Ω
    8. Bearing capacity: φmin(1.2LᶜtFᵘ, 2.4dtFᵘ)
    9. DCR per bolt; critical bolt identification
    10. Shear-tension interaction (if axial load > 0)

    The calculator auto-switches to the Results tab on completion.

  7. 7

    Review the Summary Cards & Traffic Light Status

    The Results tab shows summary cards for: n bolts, centroid coordinates, J (in⁴ or mm⁴), total moment Mₜ, maximum resultant Vᵣₖₙ, bolt capacity, and max DCR. The traffic light indicator gives instant pass/fail feedback:

    DCR < 0.80 — Safe, adequate reserve capacity
    DCR 0.80–1.00 — Warning, close to limit; verify loads
    DCR > 1.00 — FAIL: redesign required
  8. 8

    Inspect the Per-Bolt Force Distribution Table

    The detailed table shows for each bolt: X/Y coordinates, distance from centroid (rᵢ), direct shear components (Vᵈₓ, Vᵈᵥ), torsional shear components (Vᵋₓ, Vᵋᵥ), resultant Vᵣₖₙ, bolt capacity, and DCR with color-coded status (OK / WARN / FAIL). The critical bolt (marked ★) is the one with the highest DCR — it governs the connection design.

  9. 9

    View the Bolt Group Force Vector Diagram

    Switch to the Diagram tab to see the live SVG visualization. Each bolt displays:

    • Color-coded circle (green/yellow/red based on DCR)
    • Orange dashed arrow = resultant force vector (arrow length proportional to Vᵣₖₙ)
    • DCR value beneath each bolt
    • Centroid marker (orange crosshairs)
    • Scale bar for spatial reference

    Use this diagram to verify that force vectors are in the expected directions for your loading case.

  10. 10

    Export Results & Print PDF Report

    Use the Export CSV button to download a full tabular result (bolt forces, DCRs, capacities, summary statistics) for Excel documentation. Use Print / PDF for a formatted calculation report suitable for project file submission. The Formulas tab provides all step-by-step equations with LaTeX formatting for inclusion in engineering reports.

    Documentation tip: Print the Formulas tab alongside your Results for a complete, auditable calculation set per AISC 360 / IBC requirements.

All Formulas Used in Bolt Group Calculations — With Full Derivation

Every result produced by this calculator is derived from first principles of structural mechanics, force equilibrium, and deformation compatibility as specified in AISC 360. The following nine formula sets are applied sequentially by the calculation engine.

Formula 1 — Centroid of Bolt Group (Center of Gravity)

The first step in any bolt group analysis is locating the geometric centroid — the point through which a concentric shear load would produce zero rotation. For a group of n bolts with equal cross-sectional area Aᵇ:

Centroid Coordinates
$$\bar{x} = \frac{\displaystyle\sum_{i=1}^{n} x_i}{n}, \qquad \bar{y} = \frac{\displaystyle\sum_{i=1}^{n} y_i}{n}$$

For unequal bolt areas (mixed diameters), weight by area: \(\bar{x} = \sum A_i x_i / \sum A_i\). The centroidal coordinates are then used to transform all bolt positions into the centroidal reference frame:

Centroidal Coordinates per Bolt
$$x'_i = x_i - \bar{x}, \qquad y'_i = y_i - \bar{y}$$

Units: xᵢ, yᵢ in inches (in) or mm. The centroid result is shown in the Summary Cards as "Centroid X" and "Centroid Y".

Formula 2 — Polar Moment of Inertia (J or Iᵣ)

The polar moment of inertia of the bolt group characterizes its resistance to torsional (in-plane) moment. It is the key geometric property that governs how torsional shear is distributed — bolts farther from the centroid carry proportionally higher torsional loads.

Polar Moment of Inertia (unit bolt area)
$$J = I_p = \sum_{i=1}^{n} r_i^2 = \sum_{i=1}^{n} \left[(x'_i)^2 + (y'_i)^2\right]$$

Where \( r_i = \sqrt{(x'_i)^2 + (y'_i)^2} \) is the radial distance from the bolt group centroid to bolt i. If actual bolt area Aᵇ is incorporated: \( J = A_b \cdot \sum r_i^2 \).

Units: in⁴ (Imperial) or mm⁴ (Metric). Displayed in Summary Cards as "J (Polar I)".

Formula 3 — Eccentric Moment (In-Plane Torsion)

When a shear force is applied at an offset (eccentricity) from the bolt group centroid, it generates an in-plane torsional moment Mₜ. This moment is the source of the additional torsional shear forces acting on each bolt:

Total In-Plane Moment
$$M_z = V_y \cdot e_x + V_x \cdot e_y + M_{z,\text{direct}}$$

Where eₓ = horizontal eccentricity (perpendicular to Vᵥ), eᵥ = vertical eccentricity (perpendicular to Vₓ), and Mₜ,direct = any additional applied couple. Sign convention: counter-clockwise positive.

Units: kip-in (Imperial) or kN·mm (Metric). This is the fundamental quantity that separates eccentric bolt group analysis from simple concentric shear.

Formula 4 — Direct Shear per Bolt (Concentric Component)

The direct (concentric) shear component is shared equally among all n bolts in the group. It acts in the same direction as the applied force on every bolt:

Direct Shear Components
$$V_{dx} = \frac{V_x}{n}, \qquad V_{dy} = \frac{V_y}{n}$$

This is the simplest component — applicable even for concentric connections where the load passes through the centroid and Mₜ = 0. For a concentric connection, Vᵈₓ and Vᵈᵥ are the only shear components.

Units: kips (Imperial) or kN (Metric) per bolt.

Formula 5 — Torsional (Moment-Induced) Shear per Bolt

This is the most critical formula in eccentric bolt group analysis. The torsional shear acts tangentially (perpendicular to the radius vector from centroid to bolt), with magnitude proportional to the bolt's distance from the centroid — the farther the bolt, the greater its torsional load:

Torsional Shear Components (Elastic Method)
$$V_{mx,i} = \frac{M_z \cdot y'_i}{J}$$ $$V_{my,i} = \frac{-M_z \cdot x'_i}{J}$$

The negative sign on Vᵋᵥ ensures the shear force acts perpendicular to the radius vector rᵢ in the correct rotational direction. This formula is derived from the analogy between bolt group torsion and torsional stress in a shaft: \(\tau = T \cdot r / J\).

Units: kips or kN per bolt. These components are listed as "Vᵋₓ" and "Vᵋᵥ" in the per-bolt results table.

Formula 6 — Resultant Force per Bolt (Vector Superposition)

The total shear force on each bolt is obtained by vector superposition of the direct and torsional components. The resultant governs the design check:

Total Components and Resultant
$$V_{x}^{(i)} = V_{dx} + V_{mx,i}$$ $$V_{y}^{(i)} = V_{dy} + V_{my,i}$$ $$V_{\text{res},i} = \sqrt{\left[V_{x}^{(i)}\right]^2 + \left[V_{y}^{(i)}\right]^2}$$

The critical bolt is the bolt with the maximum Vᵣₖₙ,ᵢ — this governs the connection capacity. The direction of the resultant force vector (\(\theta = \arctan(V_y/V_x)\)) is shown visually in the diagram.

Force Direction Angle
$$\theta_i = \arctan\!\left(\frac{V_y^{(i)}}{V_x^{(i)}}\right)$$
Formula 7 — Bolt Shear Capacity (AISC 360 LRFD & ASD)

The nominal bolt shear capacity per AISC 360 Section J3.6 is based on the nominal shear stress Fᵗᵟ and the nominal bolt area Aᵇ. The design capacity depends on the design method:

AISC LRFD Shear Capacity (φ = 0.75)
$$\phi R_n = \phi \cdot F_{nv} \cdot A_b \cdot n_s$$
AISC ASD Shear Capacity (Ω = 2.00)
$$\frac{R_n}{\Omega} = \frac{F_{nv} \cdot A_b \cdot n_s}{\Omega}$$
Eurocode 3 Shear Resistance (γM2 = 1.25)
$$F_{v,Rd} = \frac{0.6 \cdot F_{ub} \cdot A_s}{\gamma_{M2}}$$

Where: Fᵗᵟ = nominal shear stress (ksi), Aᵇ = bolt nominal area = πd²/4 (in²), nᵡ = number of shear planes (1 or 2).

Demand-to-Capacity Ratio (DCR / Utilization)
$$\text{DCR}_i = \frac{V_{\text{res},i}}{\phi R_n} \leq 1.0 \quad \text{(LRFD)}$$ $$\text{DCR}_i = \frac{V_{\text{res},i}}{R_n / \Omega} \leq 1.0 \quad \text{(ASD)}$$

A DCR of 1.0 means the bolt is exactly at its design capacity. Values > 1.0 indicate overstress and require redesign (more bolts, larger diameter, or higher grade).

Formula 8 — Bearing Capacity of Connected Plate (AISC J3-6a)

Bolt shear alone does not govern every connection — sometimes bearing failure of the connected plate at the bolt hole controls the design. AISC 360 Section J3.6a gives the nominal bearing strength:

AISC J3-6a Bearing Capacity
$$\phi R_n = \phi \cdot \min\!\left(1.2\,L_c\,t\,F_u,\;\; C_{\text{max}}\,d\,t\,F_u\right)$$

Where: Lᶜ = net clear distance (in) from hole edge to next hole or plate edge, t = plate thickness (in), Fᵘ = ultimate tensile strength of plate (ksi), d = bolt diameter (in). The constant Cᵖᵃₓ depends on whether deformation at bolt holes is a design consideration:

Deformation ConditionCᵖᵃₓφ (LRFD)Ω (ASD)
Deformation IS a design consideration2.40.752.00
Deformation is NOT a design consideration3.00.752.00

The governing capacity is the lesser of the bolt shear capacity and bearing capacity. Select the appropriate deformation toggle in the Plate Properties section.

Formula 9 — Shear-Tension Interaction (Combined Loading Check)

When bolts carry both shear and tension simultaneously (e.g., beam-to-column moment connections, anchor bolt groups resisting overturning), a shear-tension interaction check is required per AISC 360 Section J3.7:

AISC LRFD Modified Tensile Stress (J3-3a)
$$F'_{nt} = 1.3 F_{nt} - \frac{F_{nt}}{\phi F_{nv}} \cdot f_v \leq F_{nt}$$
Combined Tensile Capacity
$$\phi R_n^{\text{combined}} = \phi \cdot F'_{nt} \cdot A_b$$

Where fᵟ = required shear stress on the bolt = Vᵣₖₙ/Aᵇ (ksi), Fᵗᵟ = nominal shear stress, Fᵗᵗ = nominal tensile stress. The simplified elliptical interaction formula is:

Simplified Elliptical Interaction
$$\left(\frac{V_{\text{res}}}{V_{\text{cap}}}\right)^2 + \left(\frac{T_u}{T_{\text{cap}}}\right)^2 \leq 1.0$$

This check is automatically activated in the calculator when axial tension T > 0. The interaction ratio is displayed in the Shear-Tension Interaction card in the Results tab.

Quick Reference: All Bolt Group Formulas at a Glance

# Quantity Formula Units
1 Centroid \(\bar{x} = \Sigma x_i/n\), \(\bar{y} = \Sigma y_i/n\) in / mm
2 Polar Moment \(J = \Sigma[(x'_i)^2 + (y'_i)^2]\) in⁴ / mm⁴
3 Total Moment \(M_z = V_y e_x + V_x e_y + M_{z,\text{add}}\) kip-in / kN·mm
4 Direct Shear \(V_{dx} = V_x/n\), \(V_{dy} = V_y/n\) kips / kN
5 Torsional Shear \(V_{mx} = M_z y'/J\), \(V_{my} = -M_z x'/J\) kips / kN
6 Resultant \(V_{\text{res}} = \sqrt{V_x^2 + V_y^2}\) kips / kN
7 LRFD Shear Cap. \(\phi R_n = 0.75 \cdot F_{nv} \cdot A_b \cdot n_s\) kips / kN
8 Bearing Cap. \(\phi R_n = 0.75 \min(1.2L_c tF_u, 2.4dtF_u)\) kips / kN
9 DCR \(\text{DCR} = V_{\text{res}} / \phi R_n \leq 1.0\) dimensionless
10 Interaction \((V/V_c)^2 + (T/T_c)^2 \leq 1.0\) dimensionless

Elastic Method vs. IC Method — When to Use Which in Bolt Group Analysis

The two available analysis methods represent fundamentally different assumptions about bolt behavior. Choosing the right one can mean the difference between an over-conservative design that wastes material and an efficient, code-compliant connection.

■ Elastic Method (Linear)
  • Assumes linear force distribution (proportional to distance from centroid)
  • Simple, fast, closed-form solution
  • Conservative — underestimates group capacity
  • Suitable for quick checks, preliminary design
  • Used in AISC 360 Appendix and most hand-calc textbooks
  • Best for: symmetric patterns, small eccentricities, simple connections
  • Formula: Vᵋ = M·r/J (linear)
■ IC Method — Instantaneous Center of Rotation (Plastic)
  • Accounts for bolt deformation — non-linear plastic behavior
  • Finds the center of rotation (IC) iteratively for equilibrium
  • More economical — higher group capacity than elastic
  • Basis for AISC Manual Tables 7-6 through 7-13
  • Required for optimized design of heavily loaded connections
  • Best for: large eccentricities, irregular patterns, optimized connections
  • Output: C coefficient × single bolt capacity = group capacity
💡
SEO Engineers Note: When searching "bolt group elastic vs IC method" — the key takeaway is: use Elastic for simplicity and conservative design, use IC for economy and code-table validation. For connections where adding another bolt is expensive (e.g., deep connection plates), the IC method often justifies the extra computation effort by showing the elastic method over-designs by 20–40%.

Understanding Your Results — All Output Parameters Explained

Output Parameter Symbol Unit Interpretation
Centroid X, Y ̅x, ̅y in / mm Geometric center of bolt group; eccentricity must be measured from this point
Polar Moment of Inertia J in⁴ / mm⁴ Larger J = more resistance to torsion; increasing bolt spacing increases J
Total Moment Mₜ Mₜ kip-in / kN·mm Torsional moment driving force redistribution; = V×e + Mᵈᵄᵃ
Direct Shear Vᵈₓ, Vᵈᵥ Vᵈₓ, Vᵈᵥ kips / kN Uniform shear on every bolt = V/n; same for all bolts in the group
Torsional Shear Vᵋₓ, Vᵋᵥ Vᵋₓ, Vᵋᵥ kips / kN Moment-induced shear component; varies by bolt position; zero at centroid
Resultant Force Vᵣₖₙ Vᵣₖₙ kips / kN Total shear force on bolt; governs bolt capacity check; largest = critical bolt
Distance from Centroid rᵢ in / mm Radial distance; proportional to torsional shear received by bolt
Bolt Shear Capacity φRₙ or Rₙ/Ω kips / kN Design strength of single bolt in shear; same for all bolts of same grade/diameter
Bearing Capacity φRₙ (bearing) kips / kN Plate bearing limit at each bolt hole; may govern over bolt shear for thin plates
DCR (Utilization Ratio) DCR dimensionless <1.0 = acceptable; =1.0 = exactly at limit; >1.0 = FAIL; target DCR < 0.90
Critical Bolt (★) Bolt with highest DCR; governs the connection design; shown on diagram
Interaction Ratio IR dimensionless Combined shear-tension check; must be ≤ 1.0; only shown when axial T > 0
Traffic Light Status Green = safe, Yellow = warning, Red = fail; based on max DCR across all bolts

Common Mistakes & Microcopy — What to Avoid in Bolt Group Analysis

These are the most frequently encountered errors in bolt group load distribution calculations — both in manual work and when using online tools. Each is paired with the correct approach.

  • Measuring eccentricity from the support face instead of from the bolt group centroid
    Measure e from the centroid of the bolt pattern (auto-computed). Using the wrong reference point overestimates or underestimates Mₜ and changes every bolt force.
  • Mixing units — entering forces in kN but lengths in inches without toggling the unit switch
    Always toggle the unit system first, then enter all inputs. The moment Mₜ = V×e must have consistent units (kip-in or kN·mm) for correct J-based torsional shear.
  • Using A325-N strength for A325-X bolts or confusing thread conditions
    A325-N (threads in shear plane) Fᵗᵟ = 54 ksi; A325-X (threads excluded) Fᵗᵟ = 68 ksi — a 26% difference. Always verify the thread condition from the fastener specification.
  • Forgetting to check bearing capacity — only verifying bolt shear, ignoring the connected plate
    Bearing capacity per AISC J3-6a often governs for thin plates. The governing capacity = min(bolt shear, bearing) — always fill in plate thickness and Fᵘ for a complete check.
  • Using single shear capacity for a double-shear connection (e.g., bolt through web between two clip angles)
    Double shear provides two shear planes — set nᵡ = 2 to correctly double the bolt capacity. Common in web connections, seated connections, and bolted splice plates.
  • Applying Elastic Method capacity limits to IC Method results, or vice versa
    Select the method consistently. The IC method output is a C coefficient × single-bolt capacity — do not apply φRₙ directly to IC Method C values without understanding the scaling.

🔎 Accuracy Note & Engineering Disclaimer

The SteelSolver Bolt Group Calculator implements the Elastic Method per AISC 360 using rigorously validated formulas. The calculated results are accurate to the precision of the inputs provided.

Important limitations to be aware of:

  • This calculator performs the Elastic Method — it is conservative relative to the IC Method. For heavily loaded connections, the IC method may demonstrate that fewer bolts are required.
  • Results do not account for block shear failure (AISC J4.3), weld-bolt combinations, or prying action in tension-loaded bolts.
  • Bolt spacing, edge distance, and end distance minimum requirements per AISC J3 must be verified independently.
  • Results produced by this calculator are for reference and educational purposes only. All final structural connection designs must be reviewed, verified, and stamped by a licensed professional engineer (PE) in accordance with the applicable building code (IBC, ASCE 7, local amendments).
  • Always cross-check critical connections against hand calculations or AISC Manual tables.

Frequently Asked Questions — Bolt Group Calculator FAQ

  • A bolt group calculator (also called a bolt pattern force distribution calculator or bolt connection calculator) is used whenever multiple fasteners in a structural steel connection are subjected to an eccentric load — meaning the load does not pass through the centroid of the bolt group. This produces both direct shear (shared equally) and torsional shear (proportional to distance from centroid). Common applications include bracket connections, shear tabs with eccentric loads, beam-to-column connections, base plate anchor bolt groups, and machinery mounts. If your load passes through the bolt group centroid, simple V/n calculations are sufficient and the full bolt group analysis is not needed.
  • The critical bolt is the bolt with the highest resultant shear force Vᵣₖₙ — and therefore the highest demand-to-capacity ratio (DCR). In eccentric bolt groups, the critical bolt is typically the one where the direct shear and torsional shear vectors are most nearly aligned (adding constructively), AND is farthest from the centroid (receiving the largest torsional component). Geometrically, this is often the bolt in the corner of the pattern that is farthest from the centroid in the direction that opposes the load eccentricity. The calculator marks it with ★ in the results table and uses the most intense color in the diagram.
  • LRFD (Load and Resistance Factor Design) applies a resistance factor φ = 0.75 to the nominal bolt strength: design capacity = φRₙ. Load demands are factored up (1.2D + 1.6L, etc.) before comparison. ASD (Allowable Strength Design) divides the nominal strength by a safety factor Ω = 2.00: allowable capacity = Rₙ/Ω. Service (unfactored) loads are compared to this allowable. Both methods are accepted by AISC 360 — they are calibrated to give equivalent designs for typical load ratios. Select the method that matches how your applied loads are specified.
  • For anchor bolt group design in base plates, use the Custom coordinate entry to input anchor bolt positions (typically symmetric about two axes). Apply vertical axial load (column load P) as axial tension/compression, horizontal base shear as Vₓ or Vᵥ, and column base moment as Mₜ. Enable the axial tension input to activate the shear-tension interaction check — base plate anchor bolts under seismic or wind loading frequently experience combined shear and tension. Note that anchor bolts in concrete also require separate pullout and concrete breakout checks per ACI 318 Appendix D, which are outside the scope of this steel bolt group calculator.
  • A325 (now superseded by ASTM F3125 Grade A325) is a medium-strength structural bolt, Fᵘ = 120 ksi. A490 (Fᵘ = 150 ksi) is a high-strength bolt. The suffix indicates thread condition: -N means threads are included in the shear plane (lower Fᵗᵟ since threads reduce effective area), while -X means threads are excluded (full shank in shear, higher Fᵗᵟ). In metric, Grade 8.8 ≈ A325 and Grade 10.9 ≈ A490. Always confirm thread condition from project drawings or specifications before entering into the calculator.
  • Increasing bolt spacing increases the polar moment of inertia J = Σr². Since torsional shear on each bolt = Mₜ·rᵢ/J, a larger J reduces the torsional component on the critical bolt — even though r also increases. The net effect is beneficial because J grows as the square of the distances, while the r in the numerator grows linearly. However, code-specified maximum spacing (usually 24t or 12 in per AISC J3.5) and practical gusset plate dimensions impose an upper limit. Edge distance constraints also prevent bolt spacing from being increased indefinitely.
  • Yes — use the Circular Pattern generator in the Bolt Pattern section. Enter the bolt circle radius, number of bolts (n), and starting angle. The calculator automatically generates the X/Y coordinates using: xᵢ = R·cos(θᵢ), yᵢ = R·sin(θᵢ) where θᵢ = start angle + i×360/n. For circular patterns under in-plane moment (flange bolt groups resisting pipe overturning moment), all bolts are equidistant from the centroid (rᵢ = R for all bolts), so the torsional shear is equal in magnitude on every bolt, but varies in direction. The resultant force varies based on how the direct shear components add to the tangential torsional components.
  • The bolt group calculator requires a minimum of 2 bolts. With only 1 bolt, there is no "group" — the single bolt carries all load components directly and no torsional distribution occurs. Practically, AISC good practice recommends a minimum of 2 bolts per connection to guard against failure from eccentricities, misalignment, and dynamic loads not captured in static analysis. For bolted moment connections (requiring moment capacity), a minimum of 4 bolts arranged in a pattern with significant J is typically required. AISC J1.8 requires at least 2 bolts for slip-critical connections.