MECHANICS OF MATERIALS

See how a beam bends.

Deflection, reactions and bending moment for two point-load cases. Add an elastic section modulus to estimate nominal bending stress.

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01 · Your inputs

Small-deflection, linear-elastic beam model. This is a preliminary calculation, not a structural capacity check or design approval.

Zero or positive. Self-weight is excluded.

200 GPa is an illustrative assumption, not a certified material property.

Use the centroidal principal axis for your bending direction. Calculate section properties →

Leave blank to omit stress. Use the same bending axis as I and the smaller elastic Z if the extreme-fiber distances differ. Do not use a plastic section modulus.

Decimal point or comma and scientific notation accepted; no thousands separators. Values update as you type.

02 · Your result

Maximum downward deflection

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Dashed line: undeformed beam. Green curve: calculated shape with exaggerated vertical displacement. Numerical values are listed below.
Magnitudes · display rounded to 8 significant digits

An absent warning is not a pass. Slenderness, material strength and permissible deflection must be assessed separately.

Inputs stay in this tab. Nothing is uploaded or saved automatically.

Understand the calculation

Formulas and units
Simply supported, central P: δmax = PL³ / (48EI), at x = L/2 |M|max = PL/4; Rleft = Rright = P/2 |θ|max = PL² / (16EI), at both supports Cantilever, end P: δmax = PL³ / (3EI), at x = L |M|max = PL, at the fixed end; Rfixed = P |θ|max = PL² / (2EI), at the free end Nominal maximum bending stress: |σ|max = |M|max / Z E (N/mm²) = 1000 × E (GPa) 1 N/mm² = 1 MPa; Z = I/c

All reported deflections, slopes and internal moments are magnitudes. The load and displacement act downward; reactions act upward. The cantilever’s external fixed-support moment is counterclockwise. The simply supported beam has an ideal pin at the left and roller at the right. The cantilever is fully fixed at the left.

The example uses L = 1000 mm, P = 1000 N, E = 200 GPa, I = 1,000,000 mm⁴ and Z = 20,000 mm³. For the simply supported case this gives δ = 0.10416667 mm, maximum moment = 250,000 N·mm and nominal bending stress = 12.5 MPa.

Assumptions and validity
  • Euler–Bernoulli theory: straight, slender, prismatic beam; constant EI; homogeneous linear-elastic material; static transverse loading; small deflections and rotations.
  • Use the centroidal principal bending axis. Shear deformation, self-weight, support flexibility, local contact effects, stress concentrations and torsion are excluded.
  • No buckling, yielding, fatigue, allowable stress, serviceability limit or safety factor is assessed. Section slenderness cannot be checked from I alone.
  • A warning appears when δ/L exceeds 1% or maximum slope exceeds 0.1 rad. These are calculator screening thresholds, not limits prescribed by the references or a design code. Values below these thresholds still require independent model validation.
  • The optional stress is nominal elastic bending stress. Its validity depends on your geometry and material staying within the model assumptions.

Supported numerical bounds: span up to 10⁹ mm, load up to 10¹² N, E up to 10⁶ GPa, and I or Z up to 10¹⁸ in their displayed units. Nonzero inputs must be at least 10⁻¹². Numerical acceptance does not imply physical validity. Display precision is not measurement uncertainty.

Sources and derivation

Support reactions and maximum moments follow static force and moment equilibrium. Alkoc Labs beam calculator v0.5.0. Independently verify inputs and results before consequential engineering use.

Continue your calculation.

Find a section’s I and Z, convert engineering units, or browse all tools →

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