TorqueCalc

Free online bolt & screw torque calculator — ASME B1.1 · ISO 724 · MIL-HDBK-5 · MMPDS

Torque from Preload Equation:
T = K × d × P
Where: K = Nut Factor (~0.20 dry steel)
       d = Nominal Screw Diameter
       P = Preload Force (lbf or N)
       P = σpreload × Astress
Ref: Shigley's MED, MIL-HDBK-60, Bickford
Unit System
Fastener Parameters
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
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.
References