BJSFM Documentation

Complete reference for the Bolted Joint Stress Field Model analysis tool — laminate setup, loading, results interpretation, and theoretical background.

Overview

What is BJSFM?

The Bolted Joint Stress Field Model (BJSFM) is an analytical tool used in aerospace and structural engineering to evaluate stress distributions around bolted joints in composite laminates. It computes the boundary stresses and strains around a loaded fastener hole under combined bearing and bypass loading conditions.

BJSFM uses Classical Lamination Theory (CLT) to characterize the laminate, then applies complex variable stress functions (Lekhnitskii’s anisotropic elasticity solution) to determine the stress field around the hole. The tool supports both single-shear and double-shear joint configurations with optional countersink effects.

Bearing Loads

Cosine-distributed pressure applied to the hole boundary simulating fastener contact.

Bypass Loads

Far-field running loads (Nx, Ny, Nxy) that bypass the fastener and create additional hole-boundary stress.

Margin of Safety

Compares ply-level strains (rotated to each fiber direction) against allowable strain limits.

Shared Laminate Builder

Laminate Properties

Input Allowables Format

Toggle between Strain (με) and Stress (ksi). Values in the stack and limits will convert on-the-fly.

NameET1 (Msi)EC1 (Msi)ET2 (Msi)EC2 (Msi)G12 (Msi)ν12t (in)σ₁t (ksi)σ₁c (ksi)σ₂t (ksi)σ₂c (ksi)σ₁₂s (ksi)r_c Tens (in)r_c Comp (in)K_br TensK_br Comp
Save as Custom Preset

Save the current material properties under a name so you can reuse them without re-entering values.

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