Bolt Shear Strength Calculator | Single & Double Shear (AISC, Eurocode, ISO)

Bolt Shear Strength Calculator – determine bolt shear capacity, shear stress, safety factor & pass/fail status for single & double shear configuration
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This powerful Bolt Shear Strength Calculator helps engineers and designers quickly determine the shear capacity and safety of bolts in single shear, double shear, or multi-plane configurations.

It supports major international standards including AISC 360 (LRFD & ASD), Eurocode 3, and ISO 898, with full metric (mm/kN/MPa) and imperial (in/kip/ksi) support.

Enter bolt diameter, grade, thread position, applied load, and number of bolts to instantly get shear area, allowable stress, utilization ratio, achieved safety factor, and clear Pass/Fail status. Advanced features include combined shear+tension interaction, bearing/tearout checks, and temperature derating.

Perfect for structural steel connections, machinery, and safety-critical bolted joints.

🔧

Bolt Shear Strength Calculator

Determine shear capacity, safety factor, and pass/fail status for single & double shear configurations. Supports AISC, Eurocode, ISO standards — metric and imperial.

✓ Single & Double Shear ✓ AISC / Eurocode / ISO ✓ Metric & Imperial ✓ Pass / Fail Status
⚙ Unit System: All fields update automatically
This tool calculates shear failure of bolt bodies — not torque, preload, or clamping force. For axial loads, use our Torque→Clamping Force Calculator.
🔢 Bolt Geometry
mm
Shear Configuration
Shear Configuration Diagram
📈 Material & Bolt Grade
MPa
MPa
Applied Load
kN
kN
👀 Design Code & Safety Factor
🔎 Bearing & Tearout Check (Optional)
Enable bearing / tearout check on connected plate
🌡 Temperature Derating (Optional)
Enable temperature correction factor
🔁 Reverse Calculator — Find Required Bolt Size
Enter the required shear capacity and the tool suggests the minimum bolt diameter for your selected grade and configuration.
kN
📚 All formulas displayed below are used in the calculator. Variables are defined in each block. Rendered with MathJax LaTeX.
🔢 Shear Area Formulas
1. Gross Shank Area (threads excluded from shear plane)
\[ A_{shank} = \frac{\pi}{4} \cdot d^2 \]
Where \(d\) = nominal bolt diameter. Use when the shear plane passes through the unthreaded shank.
2. Tensile Stress Area (threads in shear plane)
\[ A_t = \frac{\pi}{4} \left( d - 0.9382 \cdot P \right)^2 \]
Where \(P\) = thread pitch. Approximately 75–80% of the gross area. Conservative (weaker) assumption.
Shear Strength & Stress
3. Allowable Shear Stress (Von Mises criterion for ductile metals)
\[ \tau_{allow} = \frac{0.577 \cdot F_u}{SF} \]
Shear strength ≈ 57.7% of tensile strength (von Mises). Divide by safety factor for allowable.
4. AISC 360 Nominal Shear Strength
\[ R_n = F_{nv} \cdot A_b \cdot n_{planes} \] \[ F_{nv} = 0.450 \cdot F_u \; \text{(threads in shear plane)} \] \[ F_{nv} = 0.563 \cdot F_u \; \text{(threads excluded)} \]
Per AISC 360-22 Table J3.2. Design strength: \(\phi R_n\) with \(\phi = 0.75\) (LRFD) or \(R_n / \Omega\) with \(\Omega = 2.00\) (ASD).
5. Eurocode 3 Shear Resistance
\[ F_{v,Rd} = \frac{\alpha_v \cdot f_{ub} \cdot A}{\gamma_{M2}} \]
Where \(\alpha_v = 0.6\) (threads in shear); \(\gamma_{M2} = 1.25\); \(f_{ub}\) = ultimate bolt tensile strength.
6. Actual Shear Stress
\[ \tau_{actual} = \frac{F_{applied}}{A_{shear} \cdot n_{planes} \cdot n_{bolts}} \]
Applied shear force divided by total effective shear area. Must be ≤ \(\tau_{allow}\).
7. Total Shear Capacity
\[ F_{allow}^{total} = \tau_{allow} \cdot A_{shear} \cdot n_{planes} \cdot n_{bolts} \]
Scales capacity with number of bolts and shear planes.
Combined Loading & Bearing
8. Combined Shear + Tension Interaction (AISC J3.10)
\[ \left(\frac{f_v}{F_{nv}}\right)^2 + \left(\frac{f_t}{F_{nt}}\right)^2 \leq 1.0 \]
Where \(f_v, f_t\) = actual shear/tension stresses; \(F_{nv}, F_{nt}\) = nominal allowable values.
9. Bearing Capacity on Plate
\[ R_n^{bearing} = 2.4 \cdot F_u \cdot d \cdot t \] \[ R_n^{tearout} = 1.2 \cdot L_c \cdot t \cdot F_u \]
Per AISC 360. \(t\) = plate thickness; \(L_c\) = clear edge distance; governing is the lesser value.
10. Safety Factor / Utilization
\[ SF_{achieved} = \frac{F_{allow}^{total}}{F_{applied}} \] \[ \text{Utilization} = \frac{F_{applied}}{F_{allow}^{total}} \times 100\% \]
Utilization < 80%: safe; 80–100%: near limit; > 100%: FAIL.
📈 Material property reference table. Click any row to auto-fill bolt grade properties in the calculator.
🔢 ISO 898-1 Metric Bolt Grades
ClassFu (MPa)Fy (MPa)Shear Str. (MPa)Typical Use
🔢 ASTM / SAE Imperial Bolt Grades
GradeFu (ksi)Fy (ksi)Shear Str. (ksi)Typical Use
📄 Export & Copy Results

Run the calculator first, then copy or print your full report.

✓ Copied to clipboard!
🔎 How to Use This Calculator
1
Select unit system (Metric or Imperial) at the top. All labels update automatically.
2
Enter bolt diameter and select whether threads pass through the shear plane (conservative) or the shank does (optimistic).
3
Choose Single or Double Shear configuration — double shear approximately doubles the capacity.
4
Select bolt grade / standard. Fu and Fy auto-fill. You can override with custom values.
5
Enter applied shear force and design code. Click Calculate to see results.
6
Check Utilization Ratio: green (<80%), yellow (80–100%), red (>100% = FAIL).

Accuracy Note: This tool uses standard engineering formulas (AISC 360, Eurocode 3 EN 1993-1-8, ISO 898-1) and is intended for preliminary design and educational purposes. Always verify critical connections with a licensed structural or mechanical engineer. Results depend on input accuracy, material certifications, and installation quality. This calculator does not replace professional engineering judgment.

🔗 Related Engineering Calculators

This calculator addresses transverse shear failure only. For other failure modes, use the appropriate tool:

🔢 Engineering Calculator Guide

Bolt Shear Strength Calculator:
Complete User Guide & Formula Reference

A step-by-step guide to calculating bolt shear capacity, shear stress, and safety factor for structural and mechanical fastener connections. Covers single shear, double shear, AISC 360, Eurocode 3, ISO 898, metric and imperial units.

✓ Bolt Shear Capacity ✓ Single & Double Shear ✓ AISC / Eurocode / ISO ✓ Metric & Imperial ✓ Safety Factor ✓ Pass / Fail Status
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What Is a Bolt Shear Strength Calculator? Understanding shear failure — separate from torque, preload, and clamping force

⚠ Critical Distinction: Shear Failure vs. Torque & Preload

A Bolt Shear Strength Calculator is a precision engineering tool that solves one specific problem: "Will this bolt snap sideways under a lateral (transverse) load?" This is entirely separate from torque, clamping force, or preload calculations, which deal with the bolt’s axial tension. Shear strength is a distinct material property — it describes resistance to forces acting perpendicular to the bolt axis, not along it. Engineers who confuse the two risk catastrophic structural failure.

🔢 What Bolt Shear Strength Calculates

  • The maximum transverse load a bolt can resist before shearing (cutting) through its cross-section
  • Shear stress (\(\tau\)) acting across the bolt’s cross-sectional area
  • Allowable shear capacity with code-based safety factors (AISC, Eurocode 3, ISO 898)
  • Utilization ratio: how close the bolt is to its failure limit
  • Pass/Fail status for design compliance

❌ What This Calculator Does NOT Calculate

  • Torque (rotational force applied during installation)
  • Preload / clamping force (axial tension created by tightening)
  • Thread stripping (internal thread shear — separate calculation)
  • Fatigue life under cyclic loads (use a dedicated S-N tool)
  • Bolt bending (use a pin/beam bending calculator)
💡 Quick rule: If the force tries to pull the bolt out → use a tensile/clamping tool. If it tries to slide or cut the bolt sideways → use this shear calculator.

📈 Where Bolt Shear Strength Matters Most

🏢 Structural Engineering

Steel beam-to-column connections, bracket plates, gusset plates, shear tab connections, and moment frames where lateral loads act perpendicular to the bolt axis.

⚙ Mechanical Engineering

Flange couplings, clevis pins, hinge bolts, machinery guards, and automotive chassis connections where transverse forces dominate.

✈ Aerospace & Industrial

Anchor bolt design, pressure vessel flanges, lug plates, and structural assemblies where shear is the governing failure mode under service loads.

Key User Pain Points & How This Calculator Solves Them Why manual bolt shear calculations fail — and what the tool fixes

Thread Ambiguity: Shank vs. Threaded Area

Engineers are unsure whether the shear plane passes through the smooth shank (stronger) or the threaded portion (weaker), leading to either over-design or dangerous under-estimation of bolt shear capacity.

✓ Solution: Explicit shank vs. thread toggle with automatic area calculation for each case

Single vs. Double Shear Confusion

Doubling shear planes nearly doubles bolt shear capacity, but many engineers apply single-shear formulas to double-shear connections, severely underestimating the bolt’s load-bearing capacity.

✓ Solution: One-click shear configuration selector with SVG diagram showing exact cut planes

Unit Conversion Errors

Mixing metric (mm, MPa, kN) and imperial (in, ksi, kip) units is one of the most common and costly engineering mistakes in fastener shear strength calculations.

✓ Solution: One-click unit system toggle — all labels, inputs, and outputs convert simultaneously

No Quick Bolt Grade Reference

Looking up Fu (ultimate tensile strength) and Fy (yield strength) for ASTM A325, ISO 10.9, or SAE Grade 8 from separate tables slows down the design process and introduces transcription errors.

✓ Solution: Built-in grade library with auto-fill for ISO 898, ASTM A325/A490, SAE Grade 2/5/8, Stainless

No Clear Pass/Fail with Safety Margin

Raw calculations produce a number, but engineers need to know the utilization ratio and whether the connection is 5% or 50% over capacity — with the code-based safety factor already applied.

✓ Solution: Color-coded utilization bar (green/amber/red) + achieved safety factor display

Code Compliance Uncertainty

Different projects require different standards: AISC 360 (LRFD or ASD), Eurocode 3 (EN 1993-1-8), ISO 898, or ASME — each with different reduction factors and shear stress coefficients.

✓ Solution: Design code selector with pre-loaded \(\phi\), \(\Omega\), and \(\gamma_{M2}\) factors per standard
📈

Bolt Shear Failure: Visual Explanation Single shear, double shear, and shear plane diagrams

SINGLE SHEAR 2 plates — 1 shear plane Shear Plane F R Plate A Plate B Capacity = τₐₗₗₒₗₓ × A × 1 plane DOUBLE SHEAR 3 plates — 2 shear planes (~2x capacity) Plane 1 Plane 2 F R Plate 1 Web Plate 2 Capacity = τₐₗₗₒₗₓ × A × 2 planes = ~2x Single Shear SHEAR STRESS Cross-section view — \(\tau = F / A\) Gross Area A πd²/4 Threaded Area At d (nominal diameter) Orange = shear area used Shear force (F) Shear plane Threaded area At Gross shank area A R = Reaction force Single shear: 1 plane | Double shear: 2 planes
Fig. 1 — Bolt shear force configurations: single shear (left), double shear (centre), and bolt cross-section shear stress distribution (right). Double shear provides approximately twice the shear resistance of a single-shear connection.
Utilization Ratio — Pass / Fail Status Guide SAFE (< 80%) WARN FAIL 0% 25% 50% 75% 80% 100% 100%+ Example: 67% ✓ Safe Utilization (%) = Applied Shear Force ÷ Total Shear Capacity × 100. Design target: below 80% for adequate margin.
Fig. 2 — Utilization ratio gauge. The calculator color-codes results: green (<80% = safe), amber (80–100% = near limit, review design), red (>100% = bolt failure).
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Step-by-Step User Guide: How to Use the Bolt Shear Strength Calculator From inputs to results — with validation tips and common mistakes

1

Select Your Unit System (Metric or Imperial)

Click Metric (mm / kN / MPa) or Imperial (in / kip / ksi) at the top of the calculator. All input labels, result units, and bolt grade values update automatically — you never need to convert manually.

  • Metric: diameter in mm, force in kN, stress in MPa (N/mm²)
  • Imperial: diameter in inches, force in kip (1 kip = 1000 lbf), stress in ksi (kip/in²)
  • All internal calculations use metric (SI) internally and convert for display
Common Mistake: Do not mix units. If your plate thickness is in millimetres, make sure the force is in kN, not lbf. The unit toggle prevents this error entirely.
2

Enter the Bolt Nominal Diameter

Type the nominal (outer) bolt diameter or click a quick-fill size pill (M6, M8, M10, M12… or 1/4", 3/8", 1/2"…). The nominal diameter is the declared thread size, not the thread root or pitch diameter.

  • Metric example: M12 bolt → enter 12 mm
  • Imperial example: 1/2" bolt → enter 0.5 in
  • The calculator uses nominal diameter to compute both shank gross area and tensile stress area automatically
Do not enter the thread root diameter. Enter the nominal (declared) size. The calculator internally derives the correct reduced area for threaded sections using the standard pitch formula.
3

Choose Thread Position in the Shear Plane

This is one of the most important inputs. Select from the dropdown:

  • Threads in shear plane (conservative): The cut passes through the threaded portion of the bolt. Use the reduced tensile stress area \(A_t\). This gives a lower (safer) capacity estimate. Required by AISC for most structural connections unless otherwise verified.
  • Shank in shear plane (optimistic): The cut passes through the smooth unthreaded shank. Use the gross shank area \(A_{shank} = \pi d^2 / 4\). This gives ~20–25% higher capacity. Only valid when you can confirm the shear plane avoids threads (e.g., by using a shoulder bolt or specifying exact grip length).
💡 Design tip: When in doubt, always select Threads in shear plane. This is the conservative, code-compliant default for structural fastener design per AISC 360 and Eurocode 3.
4

Select Shear Configuration (Single / Double / Multi-Plane)

Click one of the three configuration cards. The SVG diagram updates automatically to show the joint geometry:

  • Single shear: Two plates, one shear plane (lap joint, bracket connection). Most common in simple connections.
  • Double shear: Three plates, two shear planes (clevis joint, gusset plate, pin connections). Approximately doubles the bolt shear capacity.
  • Multi-plane: Enter a custom number of shear planes for complex assemblies. Capacity scales linearly with the number of planes.
Common Mistake: Applying a double-shear formula to a single-shear connection cuts the apparent safety factor in half — dangerously non-conservative. Always verify the plate configuration before selecting.
5

Select Bolt Grade & Material Standard

Use the Standard dropdown to pick your bolt system, then select the specific grade. Ultimate tensile strength (Fu) and yield strength (Fy) auto-fill:

  • ISO 898-1 Metric: Class 4.6, 5.8, 8.8, 10.9, 12.9 — most common in Europe and Asia
  • ASTM: A307, A325, A490 — North American structural steel standard
  • SAE J429: Grade 2, 5, 8 — general-purpose North American machine bolts
  • Stainless: A2-70, A4-80 — marine and corrosive environments
  • Custom: Enter Fu and Fy directly in MPa or ksi for non-standard materials
Pro tip: For ASTM A325 bolts, Fu = 830 MPa (120 ksi) and Fy = 635 MPa (92 ksi). For ISO 10.9, Fu = 1040 MPa and Fy = 940 MPa. These are pre-loaded in the grade library.
6

Enter Applied Shear Force & Simultaneous Tension

Enter the total applied shear force on the bolt group. The calculator divides this by the number of bolts to check each bolt individually.

  • If only shear is present, leave the Simultaneous Tension field as 0
  • If the bolt is also under axial tension (e.g., prying action, external tension), enter that value to trigger the combined shear + tension interaction check (AISC J3.10)
  • Force direction must be perpendicular to the bolt axis (transverse / lateral)
Do not use this for axial preload or torque. If the force is along the bolt axis (tightening or external tension only), use the Torque → Clamping Force calculator instead.
7

Choose Design Code & Safety Factor

Select the applicable structural standard. The safety factor auto-fills:

  • AISC 360 — LRFD: \(\phi = 0.75\) resistance factor (load and resistance factor design)
  • AISC 360 — ASD: \(\Omega = 2.00\) safety factor (allowable strength design)
  • Eurocode 3 (EN 1993-1-8): Partial factor \(\gamma_{M2} = 1.25\)
  • ISO 898: Safety factor 1.5 — fastener-specific standard
  • ASME B&PV: Safety factor 3.0 — pressure vessel / conservative
  • Custom: Enter any value from 1.0 to 10.0
8

Click “Calculate Shear Capacity” & Read Results

The results panel appears instantly below the inputs. Check these key outputs:

  • Actual Shear Stress vs. Allowable Shear Stress — actual must be lower
  • Total Shear Capacity vs. Applied Force — capacity must exceed applied
  • Utilization Ratio (%) — target below 80% for adequate margin
  • Safety Factor achieved — must equal or exceed your design code requirement
  • Pass / Fail Status — green = safe, amber = near limit, red = failure
  • Step-by-step working — scroll down to verify every calculation stage
Design action if FAIL: Increase bolt diameter, upgrade to a higher grade (e.g., 8.8 → 10.9), add more bolts, or switch from single to double shear. The Reverse Calculator (Advanced tab) can suggest the minimum required diameter automatically.
🔢

All Formulas Used in Bolt Shear Strength Calculations Full derivations with variable definitions, units, and code references

All equations below are typeset in LaTeX via MathJax. Every formula shown here is directly used in the calculator’s calculation engine. Variables are defined in full beneath each equation.
Formula 1 — Shear Area (Gross Shank)

Gross Cross-Sectional Area — Threads Excluded from Shear Plane

\[ A_{shank} = \frac{\pi}{4} \cdot d^2 \]
\(A_{shank}\) = Gross shank area (mm² or in²) — full circular cross-section area
\(d\) = Nominal bolt diameter (mm or in) — the declared outer diameter
Use when: The shear plane passes through the unthreaded shank portion. Gives the largest (most optimistic) shear area.
Formula 2 — Shear Area (Threaded)

Tensile Stress Area — Threads Included in Shear Plane

\[ A_t = \frac{\pi}{4} \left( d - 0.9382 \cdot P \right)^2 \]
\(A_t\) = Tensile stress area (mm²) — effective area through threaded cross-section
\(d\) = Nominal bolt diameter (mm)
\(P\) = Thread pitch (mm) — distance between thread peaks. For M12: P = 1.75 mm; for M10: P = 1.5 mm
0.9382 = Standard constant for unified/metric thread profile geometry (ISO 68-1)
Use when: The shear plane cuts through the threaded section. This is the conservative, code-preferred value (~75–80% of gross area).
Formula 3 — Allowable Shear Stress (Von Mises)

Allowable Shear Stress — Von Mises Yield Criterion for Ductile Metals

\[ \tau_{allow} = \frac{0.577 \cdot F_u}{SF} \]
\(\tau_{allow}\) = Allowable shear stress (MPa or ksi)
0.577 = Von Mises constant (= \(1/\sqrt{3}\)) — relates shear strength to tensile strength for ductile metals
\(F_u\) = Ultimate tensile strength (MPa or ksi) — from material grade (e.g., 830 MPa for A325)
\(SF\) = Safety factor (dimensionless) — AISC ASD: 2.0; ISO 898: 1.5; ASME: 3.0
Note: Some codes use 0.6 instead of 0.577 as a simplified approximation (within ~4% of the Von Mises value).
Formula 4 — AISC 360 Nominal Shear Strength

Nominal Shear Resistance — AISC 360-22 Table J3.2

\[ R_n = F_{nv} \cdot A_b \cdot n_{planes} \] \[ F_{nv} = \begin{cases} 0.450 \cdot F_u & \text{threads in shear plane (N)} \\ 0.563 \cdot F_u & \text{threads excluded (X)} \end{cases} \]
\(R_n\) = Nominal shear strength (kN or kip)
\(F_{nv}\) = Nominal shear stress of fastener (MPa or ksi)
\(A_b\) = Nominal unthreaded body (bolt) cross-sectional area (mm² or in²)
\(n_{planes}\) = Number of shear planes (1 = single, 2 = double)
LRFD design strength: \(\phi R_n\) with \(\phi = 0.75\)
ASD allowable strength: \(R_n / \Omega\) with \(\Omega = 2.00\)
Formula 5 — Eurocode 3 Shear Resistance

Design Shear Resistance per Bolt — EN 1993-1-8 §3.6.1

\[ F_{v,Rd} = \frac{\alpha_v \cdot f_{ub} \cdot A}{\gamma_{M2}} \]
\(F_{v,Rd}\) = Design shear resistance per bolt per shear plane (kN)
\(\alpha_v\) = Shear coefficient: 0.6 for threads in shear plane (classes 4.6, 5.6, 8.8); 0.5 for some classes at threads
\(f_{ub}\) = Ultimate tensile strength of bolt material (MPa) — same as Fu
\(A\) = \(A_t\) (tensile stress area) if threads in shear plane; \(A_{shank}\) if shank in shear plane
\(\gamma_{M2}\) = Partial safety factor = 1.25 for bolts in shear
Formula 6 — Actual Shear Stress

Applied Shear Stress in the Bolt Cross-Section

\[ \tau_{actual} = \frac{F_{applied}}{A_{shear} \cdot n_{planes} \cdot n_{bolts}} \]
\(\tau_{actual}\) = Actual shear stress in bolt (MPa or ksi)
\(F_{applied}\) = Total applied shear force on the connection (kN or kip)
\(A_{shear}\) = Effective shear area per bolt (\(A_t\) or \(A_{shank}\)) (mm² or in²)
\(n_{planes}\) = Number of shear planes per bolt
\(n_{bolts}\) = Total number of bolts in the connection
Check: \(\tau_{actual} \leq \tau_{allow}\) for a safe connection
Formula 7 — Total Shear Capacity

Total Allowable Shear Force on Bolt Group

\[ F_{allow}^{total} = \tau_{allow} \cdot A_{shear} \cdot n_{planes} \cdot n_{bolts} \]
\(F_{allow}^{total}\) = Total allowable shear force for the entire connection (kN or kip)
All other variables as defined above.
Note: This assumes equal load distribution among all bolts. For eccentric bolt groups, the most-loaded bolt governs (use the Advanced / Reverse Calculator feature).
Formula 8 — Safety Factor & Utilization

Achieved Safety Factor and Utilization Ratio

\[ SF_{achieved} = \frac{F_{allow}^{total}}{F_{applied}} \qquad \text{Utilization (\%)} = \frac{F_{applied}}{F_{allow}^{total}} \times 100 \]
\(SF_{achieved}\) = Achieved safety factor (dimensionless) — must be ≥ required SF
Utilization (%) = Percentage of capacity used:
  • < 80% → SAFE with adequate margin
  • 80–100% → NEAR LIMIT — review design
  • > 100% → FAIL — bolt will shear
Formula 9 — Combined Shear + Tension Interaction

AISC 360 J3.10 — Bolt Under Simultaneous Shear and Tension

\[ \left(\frac{f_v}{F_{nv}}\right)^2 + \left(\frac{f_t}{F_{nt}}\right)^2 \leq 1.0 \]
\(f_v\) = Actual applied shear stress (MPa or ksi)
\(F_{nv}\) = Nominal allowable shear stress (MPa or ksi) = 0.45 Fu or 0.563 Fu
\(f_t\) = Actual applied tensile stress (MPa or ksi)
\(F_{nt}\) = Nominal allowable tensile stress = 0.75 Fu
Triggered: Only when a simultaneous tension load is entered. Interaction ratio ≤ 1.0 = safe.
Formula 10 — Bearing & Tearout Capacity (Advanced)

Plate Bearing Strength and Edge Tearout — AISC 360 J3.6

\[ R_n^{bearing} = 2.4 \cdot F_{u,plate} \cdot d \cdot t \] \[ R_n^{tearout} = 1.2 \cdot L_c \cdot t \cdot F_{u,plate} \]
\(R_n^{bearing}\) = Nominal bearing strength of plate (kN or kip)
\(R_n^{tearout}\) = Nominal tearout (edge shear) capacity (kN or kip)
\(F_{u,plate}\) = Ultimate tensile strength of the connected plate (MPa or ksi)
\(d\) = Bolt nominal diameter (mm or in)
\(t\) = Thickness of the connected plate (mm or in)
\(L_c\) = Clear edge distance (centre of bolt to plate edge) (mm or in)
Governing: Use the lesser of \(R_n^{bearing}\) and \(R_n^{tearout}\). If this is less than the bolt shear capacity, the plate governs failure.
🔢 Accuracy Note: These formulas are derived from AISC 360-22, Eurocode 3 EN 1993-1-8:2005, ISO 898-1:2013, and ASME B&PV Code Section II Part D. The calculator implements them faithfully for standard connections. Results are for preliminary design guidance. Critical structural connections must be verified and stamped by a licensed professional engineer. Bolt material properties vary by manufacturer lot; always obtain certified mill test reports for safety-critical applications.

Input Validation & Common Calculation Mistakes Microcopy guide — what to check before trusting your results

❌ Common Mistakes to Avoid

Using tensile strength as shear strength: Shear strength ≠ tensile strength. Bolt shear capacity is approximately 57.7% (Von Mises) to 60% of ultimate tensile strength. Using Fu directly leads to dangerous over-estimation.
Ignoring thread engagement: Thread engagement length affects thread stripping, not bolt shear body failure. For this calculator, thread position at the shear plane matters, not thread engagement length.
Assuming all bolts share load equally: This is only valid for concentric loading. Eccentric loads (where the resultant passes outside the bolt group centroid) cause unequal distribution. Use the Advanced tab for eccentric analysis.
Forgetting combined loading: If your bolt carries both shear and axial tension simultaneously (e.g., hanger connections), always run the combined interaction check (Formula 9). Ignoring tension can cause failure even when shear alone is within limits.
Neglecting bearing/tearout: A bolt may be safe in shear but still cause plate failure. Always check plate bearing and edge tearout for thin or low-strength plates (Advanced tab).

✓ Input Validation Checklist

  • ☑ Diameter > 0 (enter nominal bolt size, not root diameter)
  • ☑ Ultimate tensile strength Fu > 0 (check grade table if unsure)
  • ☑ Applied force > 0 (total force on the entire bolt group)
  • ☑ Safety factor ≥ 1.0 (SF < 1.0 is physically meaningless)
  • ☑ Number of bolts ≥ 1 (integer value only)
  • ☑ Unit system matches your input values (metric or imperial)
  • ☑ Shear plane position reflects actual joint geometry
  • ☑ Design code matches project specification (AISC, EC3, or ISO)
  • ☑ Bearing check inputs filled if plate failure is a concern
💡 The calculator shows a step-by-step working panel after each calculation. Always verify each step against your own hand calculation before using results for design decisions.
📈

Bolt Grade Reference Chart: Fu, Fy & Shear Strength ISO 898-1 metric grades, ASTM, and SAE imperial grades with shear capacity values

Table 1 — ISO 898-1 Metric Bolt Property Classes — Fu, Fy, and Approximate Shear Strength
Class Ultimate Fu (MPa) Yield Fy (MPa) Shear Str. ≈ 0.577×Fu (MPa) Shear (SF=2.0) (MPa) Typical Applications
4.6400240231115Non-critical general fasteners, wood connections
5.8500400289144General purpose machine bolts, lightly loaded joints
8.8830660479240High-strength structural bolts, most common for steel construction
10.91040940600300Very high strength, automotive, heavy machinery
12.912201100704352Ultra-high strength, safety-critical assemblies, aerospace-adjacent
Table 2 — ASTM / SAE Imperial Bolt Grades — Fu, Fy, and Approximate Shear Strength
Grade Fu (ksi) Fy (ksi) Shear ≈ 0.577×Fu (ksi) AISC Fnv (ksi)* Typical Applications
ASTM A307603534.627.0Light structural connections, anchor bolts
ASTM A3251209269.254.0 / 67.5Structural steel connections, most common US standard
ASTM A49015013086.667.5 / 84.4High-strength structural connections, seismic zones
SAE Grade 51209269.2Automotive and general mechanical fastener applications
SAE Grade 815013086.6High-strength automotive, heavy-duty machinery
A2-70 (304 SS)101.565.358.6Food processing, marine, corrosive environments
A4-80 (316 SS)11692.866.9Offshore, chemical, high-corrosion environments

*AISC Fnv: threads-in-shear / threads-excluded values per AISC 360-22 Table J3.2. Shear strength shown is ultimate; divide by safety factor for allowable design value.

Table 3 — Shear Configuration Comparison — Effect on Bolt Shear Capacity
Configuration Shear Planes Capacity vs. Single Shear Typical Joint Type Area Used
Single shear, threaded1Baseline (1.0×)Lap joint, bracket plate\(A_t\) (tensile stress area)
Single shear, shank1~1.25× baselineShoulder bolt connection\(A_{shank}\) (gross area)
Double shear, threaded2~2.0× baselineClevis, gusset plate\(A_t \times 2\)
Double shear, shank2~2.5× baselinePin joint, clevis + shoulder\(A_{shank} \times 2\)
Multi-plane (n planes)n~n × baselineComplex multi-plate assemblies\(A_{eff} \times n\)
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Worked Example: M12 Grade 8.8 Bolt in Single Shear Complete step-by-step shear strength calculation with all formulas applied

🔢 Problem Statement

An M12 Grade 8.8 bolt connects two steel plates in single shear. Threads pass through the shear plane. The connection carries an applied shear force of F = 20 kN. Using AISC ASD (Ω = 2.0), determine: (a) the allowable shear capacity, (b) actual shear stress, and (c) pass/fail status.

🔢 Given Data

Bolt Geometry Diameter d = 12 mm
Thread pitch P = 1.75 mm
Shear planes = 1 (single)
No. bolts = 1
Material (ISO 8.8) Fu = 830 MPa
Fy = 660 MPa
Threads in shear plane
Load & Code F applied = 20 kN
Code: AISC ASD
Safety factor SF = 2.0

🔢 Step 1: Calculate Tensile Stress Area (Formula 2)

\[ A_t = \frac{\pi}{4}(d - 0.9382 \cdot P)^2 = \frac{\pi}{4}(12 - 0.9382 \times 1.75)^2 = \frac{\pi}{4}(10.358)^2 \approx 84.3 \text{ mm}^2 \]

Compare with gross shank area: Ashank = π/4 × 12² = 113.1 mm². The threaded area (84.3 mm²) is 74.5% of gross, confirming the ~25% reduction for threads in the shear plane.

🔢 Step 2: Calculate Allowable Shear Stress (Formula 3)

\[ \tau_{allow} = \frac{0.577 \times 830}{2.0} = \frac{479.0}{2.0} = 239.5 \text{ MPa} \]

🔢 Step 3: Calculate Shear Capacity (Formula 7)

\[ F_{allow} = \tau_{allow} \times A_t \times n_{planes} \times n_{bolts} = 239.5 \times 84.3 \times 1 \times 1 = 20{,}190 \text{ N} = \mathbf{20.19 \text{ kN}} \]

🔢 Step 4: Actual Shear Stress (Formula 6)

\[ \tau_{actual} = \frac{20{,}000}{84.3 \times 1 \times 1} = 237.3 \text{ MPa} \]

🔢 Step 5: Utilization & Safety Factor (Formula 8)

\[ \text{Utilization} = \frac{20.0}{20.19} \times 100 = \mathbf{99.1\%} \qquad SF_{achieved} = \frac{20.19}{20.0} = \mathbf{1.01} \]
Result: NEAR LIMIT (99.1% utilization). The bolt just barely passes, but the safety factor of only 1.01 is dangerously close to 1.0. Recommended actions: (1) Upgrade to M14 or M16, or (2) use two M12 bolts, or (3) verify if double-shear configuration is possible to halve the demand per plane.

Frequently Asked Questions — Bolt Shear Strength Calculator How to calculate bolt shear strength, force vs tensile force comparison, and more

Bolt shear strength is the maximum lateral (sideways) force a bolt can resist before fracturing across its cross-section — as if the bolt is being cut like a pair of scissors. Tensile strength (Fu) is the maximum axial (along the bolt axis) pulling force it can resist before breaking.

These are distinct mechanical properties. Shear strength is approximately 0.577 to 0.60 times the ultimate tensile strength for ductile steel bolts (Von Mises criterion). For example, a bolt with Fu = 830 MPa has a shear strength of approximately 479–498 MPa.

This calculator addresses shear failure only. It is not a torque calculator, clamping force calculator, or preload tool — those all deal with axial tension.

The fundamental approach for calculating bolt shear strength by hand:

  • Step 1: Find the shear area. If threads are in the shear plane: \(A_t = \frac{\pi}{4}(d - 0.9382P)^2\). If shank: \(A = \frac{\pi d^2}{4}\)
  • Step 2: Find allowable shear stress: \(\tau_{allow} = \frac{0.577 \times F_u}{SF}\) where SF is your safety factor
  • Step 3: Allowable capacity = \(\tau_{allow} \times A \times n_{planes} \times n_{bolts}\)
  • Step 4: Compare with applied force. If capacity > applied → safe

The calculator automates all four steps and handles unit conversions, grade lookups, and code factors automatically.

Single shear occurs when two plates overlap and a bolt connects them — there is one cut plane. The full applied force is resisted at one cross-section of the bolt.

Double shear occurs in a three-plate (clevis-type) connection where the middle plate is sandwiched between two outer plates. The bolt has two cut planes, so the applied force is split between two cross-sections. This approximately doubles the shear capacity for the same bolt size and grade.

For example: an M16 Grade 8.8 bolt might carry 30 kN in single shear but 60 kN in double shear. Always confirm which configuration your joint uses before selecting single or double in the calculator.

It depends on where the shear plane intersects the bolt:

  • Use tensile stress area (\(A_t\)) — conservative: When threads pass through the shear plane. Required by AISC 360 for standard connections unless otherwise verified. About 75–80% of gross area.
  • Use gross shank area (\(A_{shank}\)) — optimistic: Only when the shear plane is verified to pass through the unthreaded shank. Applicable for shoulder bolts or when grip length is specifically controlled.

When in doubt, always use the threaded (tensile stress) area. This is the default in the calculator and the most structurally conservative assumption.

ASTM A325 bolts have an ultimate tensile strength Fu = 120 ksi (830 MPa). The shear strength is:

  • Ultimate shear strength: ≈ 0.577 × 120 = 69.2 ksi (477 MPa)
  • AISC 360 Nominal Fnv: 54 ksi (372 MPa) with threads in shear plane; 67.5 ksi (465 MPa) with threads excluded
  • LRFD design shear (\(\phi R_n\)): Use \(\phi = 0.75\) applied to \(R_n = F_{nv} \cdot A_b\)

Use the Grade dropdown in the calculator to auto-fill A325 values and get the full capacity for your specific diameter, configuration, and code.

Safety factor depends on the applicable design standard and application:

  • AISC 360 LRFD: Use resistance factor \(\phi = 0.75\) (equivalent SF ≈ 2.0 for typical load combos)
  • AISC 360 ASD: Safety factor \(\Omega = 2.00\)
  • Eurocode 3: Partial factor \(\gamma_{M2} = 1.25\)
  • ISO 898 / machine design: SF = 1.5 to 3.0 depending on consequence of failure
  • ASME pressure vessel: SF = 3.0 (conservative, safety-critical)

Higher safety factors are used for shock loads, fatigue-prone applications, or connections where failure could cause injury. The calculator lets you set a custom factor if your project specification requires one.

Shear force acts perpendicular (transverse) to the bolt axis — it tries to cut the bolt sideways. A bolt in shear acts like a pin resisting two plates from sliding apart.

Tensile force (preload) acts along the bolt axis — it stretches the bolt and creates clamping force between plates. Torque is the rotational force applied to generate this preload.

These are completely different structural problems. This calculator handles shear only. For preload and torque calculations, use a separate Torque → Clamping Force Calculator. If both forces act simultaneously, run the combined shear + tension interaction check (Formula 9 in this guide).

The utilization ratio is the ratio of the applied shear force to the total allowable shear capacity, expressed as a percentage:

\(\text{Utilization} = \frac{F_{applied}}{F_{allow}^{total}} \times 100\%\)

  • Below 80%: Safe with adequate margin (green)
  • 80–100%: Near limit — the bolt is close to its capacity. Review the design (amber)
  • Above 100%: Failure — the applied load exceeds allowable capacity (red)

A utilization of 60–75% is typical for well-designed connections that leave margin for load uncertainty and fatigue.

Bearing failure occurs when the bolt crushes or elongates the hole in the connected plate, rather than the bolt body shearing. This happens when the plate material is weaker or thinner than the bolt itself.

Bearing capacity (AISC): \(R_n = 2.4 \cdot F_{u,plate} \cdot d \cdot t\). If this value is less than the bolt shear capacity, bearing governs the design.

When to check: Always check bearing when using thin plates (<10 mm), low-grade plate material (e.g., A36 at 400 MPa), or high-strength bolts (A490, 10.9) in thin connections. Use the Advanced → Bearing Check tab in the calculator.

Yes — the formula reference in this guide (Formulas 1–10) can be directly replicated in Microsoft Excel or Google Sheets. The key Excel formulas are:

  • Shank area: =PI()/4*d^2
  • Tensile stress area: =PI()/4*(d-0.9382*P)^2
  • Allowable shear stress: =0.577*Fu/SF
  • Shear capacity: =tau_allow*A*n_planes*n_bolts
  • Utilization: =F_applied/F_capacity*100

Use the Export / Copy tab in the calculator to copy a fully formatted plain-text report of any calculation to paste into your Excel workbook or engineering log.

🔢 Accuracy & Disclaimer: This Bolt Shear Strength Calculator implements industry-standard formulas from AISC 360-22, Eurocode 3 EN 1993-1-8:2005, ISO 898-1:2013, and ASME B&PV Code. Results are provided for preliminary design and educational purposes only. They do not constitute professional engineering advice. All safety-critical fastener connections must be reviewed, verified, and signed off by a licensed structural or mechanical engineer holding appropriate jurisdiction-specific credentials. Bolt material properties (Fu, Fy) must be sourced from certified mill test reports for production designs. The calculator assumes concentric loading; eccentric bolt groups require additional analysis. Consult the applicable building code for your jurisdiction before finalizing any structural connection design.

🔗 Related Engineering Calculators

This guide covers transverse shear failure of bolt bodies. For other fastener failure modes and mechanical property calculations, use the appropriate companion tool: