Code tool

Direct Stress and Strain Calculator

Enter axial force F, cross-sectional area A, elastic modulus E, and original length L in consistent N, m², Pa, and m units.

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Uniform axial load, linear elasticity, and small deformation are assumed. E is supplied by you; no material table or allowable stress is embedded.

A QUICK WALKTHROUGH

How to use this tool

  1. Enter finite axial force; area, elastic modulus, and length must be positive.
  2. Review stress, strain, elongation, and axial stiffness.

Formula and source

σ = F/A; ε = σ/E; δ = FL/(AE); k = EA/L. Source: MIT OpenCourseWare, Mechanics and Materials I, Lecture 9: https://ocw.mit.edu/courses/2-001-mechanics-materials-i-fall-2006/dfbefba09e533f1349690e6e410d5524_lec9.pdf

Input limits and scope

Finite F; A>0, E>0, L>0. Inputs use N, m², Pa, m. Outputs are stress (Pa), dimensionless strain, elongation (m), and stiffness (N/m). Uniform axial load, linear elasticity, and small deformation are assumed; the tool does not verify elastic-range behavior or allowable stress.

GOOD TO KNOW

Common questions

Does this check allowable stress?

No. It is not design approval or a safety determination.

Are material defaults included?

No. Enter the elastic modulus for the specific material and conditions.