Stress Area Formula (ASME B1.1 / ISO 724):Select screw size to see computed Aₜ Inch: Aₜ = π/4 × [D − 0.9743/n]² | Metric: Aₜ = π/4 × [(d₂+d₃)/2]² | These formulas are used by MMPDS Ch.8 to compute tensile allowable loads.
Industry default: 65–75% of Proof Stress (IFI-100, MIL-HDBK-60). This matches published torque tables. Using yield strength as the basis produces significantly higher torques — only appropriate when maximum preload is required. Never exceed 90% yield. Note: Proof Stress ≈ 85–92% of Yield for most steel fasteners.
Joint & Friction Parameters
Active K Factor
0.20
Nut Factor
Prevailing / Running Torque
Prevailing torque is the drag torque to spin a locking fastener before seating — per ASME B18.16.6 & IFI-100 it must be added to seating torque. It does not contribute to clamp load. Sources: nylon-insert (Nyloc), all-metal distorted thread, serrated flange nuts.
Min – Max (from size table)
— select screw size —
Clamped Materials
⚙ Bearing Stress Check Active — A soft material is detected under the screw head. The calculator will compare preload vs. bearing capacity and automatically limit torque if the soft material governs.
Pan head ≈ 2× nominal dia. Washer OD per ASME B18.22.1
From material database
Calculated Bearing Area (A_bear = π/4 × (D_head² − D_hole²))
— enter head OD to compute —
Calculated Results
Seating Torque (Ts)
—
in·lbf
T = K·d·P
Prevailing Torque (Tp)
—
in·lbf
per ASME B18.16.6
▶ Applied Torque (Tapplied)
—
in·lbf
Ts + Tp
Applied Torque
—
ft·lbf
÷ 12 (or N·m)
Preload Force
—
lbf
P = σ_pre × A
Preload Stress
—
psi
% × Ref Strength
% of Yield
—
% Fty
σ_pre / Fty
% of UTS
—
% Ftu
σ_pre / Ftu
Prevailing Torque Breakdown
Preload Utilization vs. Yield Strength0%
0%25%50%75%100%
Drawing Note Generator
Select a note format. The generated note reflects the applied torque (seating + prevailing). Copy directly onto your engineering drawing or traveler.
— calculate first to generate note —
✓ Copied to clipboard
All Format Variants
Fastener Lookup Table
Stress areas per ASME B1.1 (UNC/UNF) and ISO 724 / ISO 898-1 for metric. Root diameters and stress areas are computed from thread geometry.
Size
Designation
Nom. Dia
TPI / Pitch
Root Dia
Stress Area
Prevailing Torque Range
Standard
⚠ Engineering Disclaimer: This tool provides torque estimates based on standard fastener preload equations. Results are for reference only. Always consult a licensed structural or mechanical engineer for safety-critical applications. Fastener performance is affected by surface finish, lubrication, temperature, fatigue, and installation method. Reference: ASME B1.1, MIL-HDBK-60, NASA-STD-5020, Shigley's Mechanical Engineering Design.
This calculator uses the industry-standard preload equation T = K × d × P, where T is the tightening torque, K is the nut factor (friction coefficient), d is the nominal bolt diameter, and P is the preload force. This formula is defined in MIL-HDBK-60, Shigley's Mechanical Engineering Design, and Bickford's Introduction to the Design and Behavior of Bolted Joints.
Preload force is computed as P = σpreload × At, where the tensile stress area At is calculated directly from thread geometry using the ASME B1.1-2019 formula for inch fasteners [At = π/4 × (D − 0.9743/n)²] and the ISO 724 formula for metric fasteners.
Bearing Stress & Soft Materials
When fastening into soft materials — FR4 PCB, ABS plastic, polycarbonate, PEEK, or carbon fiber — the fastener head crushes the material before the bolt reaches its yield strength. This calculator performs a bearing stress check: Abearing = π/4 × (D²head − D²nominal), and limits torque to prevent exceeding the material's allowable bearing stress.
Bearing strength values are sourced from IPC-2221B for FR4, MIL-HDBK-17 for composites, and published material datasheets for plastics including ABS (45 MPa), polycarbonate (60 MPa), Nylon 6/6 (70 MPa), and PEEK (150 MPa).
MMPDS & MIL-HDBK-5 Material Data
Fastener material allowables are sourced from MMPDS (Metallic Materials Properties Development and Standardization), the FAA-managed successor to MIL-HDBK-5J. MMPDS provides statistically based A-basis and B-basis Ftu and Fty allowables for aerospace fastener materials including titanium 6Al-4V (AMS 4928), A-286 CRES (AMS 5737), Inconel 718 (AMS 5662), 4340 alloy steel, and H-11 tool steel.
Commercial fastener grades use SAE J429 (Grade 2, 5, 8), ASTM A307, ASTM A574 (socket head cap screws), and ISO 3506-1 (A2-70, A4-70, A2-80 stainless steel fasteners).
Prevailing Torque for Locking Fasteners
Locking fasteners — Nyloc (nylon insert), all-metal distorted thread (Stover, Flexloc), and serrated flange nuts — require additional torque to overcome the locking drag before the fastener seats. This prevailing torque must be added to the seating torque to get the total applied torque on the wrench.
Prevailing torque ranges are sourced from ASME B18.16.6 and IFI-100 for inch fasteners, and ISO 2320 / DIN 267-24 for metric. Critically, prevailing torque does NOT contribute to clamp load — it is friction only.
This free torque calculator is an online bolt torque calculator and free engineering torque tool for mechanical engineers, aerospace engineers, electronics engineers, and IoT hardware designers.
It functions as a free fastener preload calculator, online screw torque calculator, bearing stress calculator for plastic joints, and engineering drawing note generator — all in one free tool, no login or registration required.
Find torque values for Grade 5 bolts, Grade 8 bolts, stainless steel screws, titanium aerospace fasteners, metric bolts M2 through M36, and more.