Engineering lab · Interactive tool

Beam Deflection + Stress Calculator

Screen a solid rectangular beam under a cantilever end load, simply supported center load, or simply supported uniform line load.

Elastic beam screening / rectangular section

Live calculation

01Load case

02Geometry and material

Cantilever · end point loadConceptual beam showing the selected supports and applied loading.LENGTH LAPPLIED LOADIDEALIZED NEUTRAL AXIS
Small-deflection Euler–Bernoulli modelI = b·h³ / 12

Beam results updated. Maximum deflection 0.9662 millimeters. Maximum stress 20 megapascals. Yield factor of safety 13.8.

Maximum deflection0.9662 mmelastic displacement
Maximum stress20 MPaextreme-fiber bending
Maximum moment250 N·mpeak bending moment
Yield factor of safety13.8I = 3.125e+5 mm⁴

Revision 1.3 · Reviewed 24 September 2026 · Jared Maffucci

Model, assumptions, and a reproducible reference case

I = bh³/12; δ = PL³/(3EI); σ = PLh/(2I)

Reference inputs

Cantilever, 100 N end load, length 500 mm, width 20 mm, bending height 10 mm, E = 160 GPa, yield strength 250 MPa.

Expected elastic tip deflection
15.625 mm
Calculated by this tool
15.625 mm

The corresponding bending stress is 150 MPa. This deliberately flexible example checks arithmetic; its 3.125% span deflection triggers review of the small-deflection assumption.

Check the material basis, load cases, and applicable design criteria before using a result. Warning thresholds are prompts for review, not acceptance criteria.

Use first-order response to guide the next model

The calculator applies closed-form Euler–Bernoulli beam equations in an N-mm-MPa unit system. It reports the extreme-fiber bending stress, maximum elastic deflection, maximum moment, and arithmetic yield factor of safety.

A result that appears acceptable is not proof that the real part is acceptable. Connections, cutouts, load introduction, stability, geometry changes, and multidirectional loading often control the design.

Escalate beyond this model when

  • Deflection is not small relative to the span or section depth
  • The section changes, contains openings, or is not rectangular
  • Shear deformation may be important
  • Buckling or lateral-torsional stability can control
  • Loads are dynamic, cyclic, thermal, or multidirectional
  • Supports and joints are not reasonably idealized

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