Bolt Torque, Preload and Clamp Force Calculator

Estimate per-bolt clamp force from tightening torque or find a preliminary torque from a target preload for supported inch fasteners.

What do you want to calculate?

Advanced options use 1 bolt by default when the bolt count is blank.

Advanced options
Documented test values
Joint total
Result display
Estimated clamp force per bolt

Torque-derived force is a planning estimate because friction can change the actual preload.

Estimated proof-load use

Estimated total joint clamp force

This assumes equal preload in every bolt. Bolt count does not change the per-bolt result.

Estimated proof load per bolt

This is a simplified reference estimate, not a formal compliance check.

Nut factor K used

K represents combined thread and bearing friction in the short-form equation.

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How to use our Bolt Torque, Preload and Clamp Force Calculator

  1. Choose whether you know the tightening torque or the target preload per bolt.
  2. Select the full Bolt thread size from the drawing, package, or thread gauge, then choose the closest Assembly condition estimate.
  3. Select Fastener grade for strength check if you know the head marking; otherwise choose the option to skip the check.
  4. Enter Tightening torque with lb-ft or lb-in, or enter Target preload per bolt in lbf, then select Calculate.
  5. Check that the Nut factor K used matches the actual coating and lubricant. Treat Estimated proof-load use above 100 percent as an overload indication, not an approval.
Example inputs for Bolt Torque, Preload and Clamp Force Calculator
Example inputs for Bolt Torque, Preload and Clamp Force Calculator

Definitions

Preload or clamp force: The compressive force a tightened bolt is estimated to create in one joint.

Tightening torque: The twisting input used to tighten the bolt, entered here in lb-ft or lb-in.

Nut factor K: A unit-free friction estimate that combines friction in the threads and under the nut or bolt head. A smaller K produces more estimated preload from the same torque.

Nominal diameter D: The stated bolt diameter in inches, such as 0.500 inch for a 1/2-inch bolt.

Tensile stress area: The effective threaded cross-sectional area used to estimate proof load. Thread pitch changes this area.

Proof load: Tensile stress area multiplied by proof strength. The supported thread areas and SAE Grade 5 and Grade 8 reference strengths use NASA fastener reference data [1].

Estimated proof-load use: Per-bolt clamp force divided by estimated proof load, shown as a percent.


Common mistakes and quick fixes

Mistake: Entering a torque without noticing that Tightening torque treats a bare number as lb-ft.
Fix: Type the unit when needed, such as "75 lb-ft" or "900 lb-in."

Mistake: Selecting a Bolt thread size by diameter only and missing the thread series.
Fix: Match the full designation, such as 1/2-13 UNC or 1/2-20 UNF, because the strength check uses its thread stress area.

Mistake: Using a dry torque specification after adding oil, coating, or anti-seize.
Fix: Choose the Assembly condition estimate that fits the actual assembly, or enter a documented Tested nut factor K.

Mistake: Entering the combined joint load in Target preload per bolt.
Fix: Enter the force for one bolt only; use Bolts in the joint to calculate Estimated total joint clamp force.

Mistake: Treating Estimated proof-load use as a certified pass or installation instruction.
Fix: Use the Fastener grade for strength check or Documented proof strength (psi) only as a simplified planning check, and follow the applicable procedure for the joint.


Limitations & Key Assumptions / Boundary Conditions

  • This is a short-form torque-tension estimate for supported UNC and UNF inch fastener designations only. It is not a bolt installation specification.
  • The calculation assumes K fits the actual fastener, coating, lubricant, bearing surface, and joint setup. Friction changes can cause actual preload to differ substantially from the estimate.
  • The proof-load calculation is a simplified room-temperature reference check using the selected SAE grade or a documented proof strength. It does not certify compliance, fatigue life, yield, or joint safety.
  • Total joint clamp force assumes equal preload in every bolt. It does not model joint stiffness, load distribution, embedment, relaxation, bolt stretch, or external loading.
  • Do not use a dry or plain torque estimate for lubricated, coated, anti-seize-treated, safety-critical, structural, aerospace, or other controlled assemblies without the applicable tested procedure.
  • A Bolts in the joint value of 0 intentionally makes Estimated total joint clamp force zero while leaving the per-bolt estimate unchanged.

Methodology

Calculation method

The calculator uses the common short-form torque-tension relationship. Torque is converted to lb-in before the preload calculation; 1 lb-ft equals 12 lb-in.

T = K x D x F

T is tightening torque in lb-in, K is the nut factor, D is nominal bolt diameter in inches, and F is per-bolt clamp force in lbf.

F = T / (K x D)

This form is used when estimating clamp force from entered torque.

T = K x D x F

This form is used when estimating required torque from Target preload per bolt. The calculator then divides lb-in by 12 to show lb-ft.

Strength check

For a selected grade or Documented proof strength (psi), the calculator looks up the supported thread tensile stress area and estimates proof load from the reference values in NASA RP-1228. The same source supports the supported Unified thread areas and SAE Grade 5 and Grade 8 proof strengths [1].

Proof load = tensile stress area x proof strength

Estimated proof-load use = per-bolt clamp force / proof load x 100

If no grade and no documented proof strength are supplied, the proof-load results are omitted. Total joint clamp force is per-bolt clamp force times Bolts in the joint.

Worked example

For a 1/2-13 bolt at 75 lb-ft, the torque becomes 900 lb-in. With K = 0.20 and D = 0.500 inch, estimated per-bolt clamp force is 900 / (0.20 x 0.500) = 9,000 lbf. With SAE Grade 8 reference proof strength of 120,000 psi and stress area of 0.1419 square inches, estimated proof load is 17,028 lbf, so estimated proof-load use is about 52.85 percent.

Assumptions and limits

The selected assembly condition supplies K = 0.20 for dry or plain and K = 0.15 for a typical steel-on-steel estimate. A valid Tested nut factor K replaces that estimate. These values are planning inputs, so a documented torque-tension test value is preferable when available. The method does not model separate thread and bearing friction, joint stiffness, relaxation, temperature effects, or load sharing.


Sources