HomeCalculatorsPhysicsStatics & StrengthUniform Load Deflection Calculator
Physics calculator

Uniform Load Deflection Calculator

Midspan deflection of a simply supported span with a uniform load. δ = 5 w L⁴/(384 E I). I is an input. Runs locally.

Instant result
Result
—

Enter values to calculate.

Inputs—
Mode—
Formula—
Trust summary CVP VERIFIED · production STALE · CVP protocol 1.0.0-proposed · Engineering assurance
Input interpretation
Enter values to calculate.
Result
—
Assurance
Engineering
Declared partition coverage
PASS · 2/2 declared partitions (domain, invalid-domain) · Matrix
Known limitations
  • Physics L1 gap capability
  • Core CVP does not include live graph, viewport, or pointer interaction.
Model
Midspan deflection of a simply supported span with a uniform load over the whole span.
Scope
Calculation runs locally in the browser; values are not uploaded.
Verification
Engine tested · Source checked · v1.0.0 · CVP VERIFIED · production STALE · CVP protocol 1.0.0-proposed · Engineering assurance· View Manifest · CVP overview · Specification
Versions
Calculation 1.0.0 · CVP protocol 1.0.0-proposed
CVP identity
0/0 property · digest 6c2d3eb00242
Legacy regression
4/4 tests · Production surface contract 6/6
Trust layers
Verification VERIFIED · Production STALE · overall VERIFIED_STALE
CVP status
STALE · Capability production binding: STALE · Site report: STALE · Evidence changed after the last successful production attestation. Re-attestation required.
Reference
O1 model · O2 expected_values · O2 numerical_behavior
Interfaces
PASS · UI (SSR) / REST / MCP — ui-ssr is query-result HTML, not a live browser session.
Supplemental domain review
Not performed
Named expert review
Not performed
CVP suite
1/1 golden · 2/2 CVP boundary · 2/2 invalid · 1/1 cross-interface · 6/6 CVP contract · Manifest
Sources
  • Hibbeler, Mechanics of Materials — Deflection of beams — simply supported beam with a uniform load
  • Gere and Goodno, Mechanics of Materials — Deflection of beams — simply supported beam with a uniform load
Sources
Evidence
2 legacy golden · 2 legacy boundary · legacy regression suite · 1/1 oracle-backed golden · 2/2 invalid · Artifact integrity PASS
STALE · Build schema 1.0.0 ready · Semantic contract ✓ · Last attestation PASS · current evidence changed · re-attestation required · CVP STALE · attestation STALE — Production CURRENT withheld
Semantic contract
PASS
Full verification

Manifest identity, reference classes, interfaces, suite, and production records.

Formulas

Core equations used by this calculator.

Midspan deflectionδ = 5 w L⁴ / (384 E I)
iI comes from a section page. This page does not rebuild a rectangle, a circle, or a hollow circle. A cantilever and a concentrated load are their own pages.

How to use

1

Enter the load intensity, the span, the modulus, and the area moment

L, E, and I must be positive. w may be negative. Positive w is the positive deflection direction. w, L, E, and I share one unit system, and δ then has the unit of L.

2

Read the midspan deflection

δ = 5 w L⁴/(384 E I). The sign of w is the sign of δ.

Example calculations

Common configurations with formula and result.

ϟ

Span 2

w = 24, L = 2, E = 1, I = 1, in one consistent unit system

δ = 5 × 24 × 2⁴ / (384 × 1 × 1)
δ = 5
ϟ

Same total load as a midspan point load

w L = 48. That point load on the beam-deflection page is δ = 8.

δ_uniform / δ_point = 5/8
δ = 5 here, δ = 8 on the point-load page

Uniform Load Deflection calculator specification

Version 1.0.0 · Engine tested

Calculation status

Review policy · Evidence

Definition
A simply supported span of length L carries a uniform load w over the whole span. The midspan deflection is δ = 5 w L⁴ / (384 E I). E is the elastic modulus. I is the centroidal area moment, typed in.
What it calculates
Midspan deflection of a simply supported span with a uniform load over the whole span.
Inputs
  • w
  • L
  • E
  • I
Outputs
  • delta
  • w
  • L
  • E
  • I
Formula
δ = 5 w L⁴ / (384 E I).
Assumptions
  • Calculation runs locally in the browser; values are not uploaded.
  • Keep units consistent with the labels on each field.
  • I comes from a section page. This page does not rebuild a rectangle, a circle, or a hollow circle. A cantilever and a concentrated load are their own pages.
Units
  • w, L, E, and I set the deflection unit. δ has the unit of length when those four are consistent.
Boundary conditions
  • missing w, L, E, or I → MISSING_REQUIRED_INPUT
  • L ≤ 0, E ≤ 0, or I ≤ 0 → VALUE_MUST_BE_POSITIVE
Example
w=24 L=2 E=1 I=1 → δ=5
Validation cases

3 published on this page · 4/4 tests · Production surface contract 6/6 · View evidence

  • w=24 L=2 E=1 I=1 → δ=5
  • w=-24 L=2 E=1 I=1 → δ=-5
  • L=0 → VALUE_MUST_BE_POSITIVE
Sources
  • Hibbeler, Mechanics of Materials — Deflection of beams — simply supported beam with a uniform load
    Supports: The midspan deflection is 5 w L⁴ / (384 E I) when a uniform load covers a simply supported span.
  • Gere and Goodno, Mechanics of Materials — Deflection of beams — simply supported beam with a uniform load
    Supports: Supports the page formula: δ = 5 w L⁴ / (384 E I)
Calculation version
1.0.0

Background

Interpretation and common distinctions.

Find the midspan deflection of a simply supported span with a uniform load over the whole span.

Supported and not supported

Supported: δ = 5 w L⁴/(384 E I). Positive w is the positive deflection direction. Aliases are intensity, omega, q, span, length, youngs, modulus, Ix, and inertia.

Not supported: a cantilever, a concentrated load, a load that covers only part of the span, a deflection away from midspan, and rebuilding I from a section. /calc/mechanical is not open.

Agent / API notes

Capability id: mechanical.statics.uniform_load_deflection · tool id: uniform-load-deflection · pin 1.0.0.

{ "w": 24, "L": 2, "E": 1, "I": 1 }

Share the link with w, L, E, and I. The result is not written into the link.

Frequently asked questions

Key distinctions behind the calculation.

Where is the deflection reported?

At midspan. A point elsewhere on the span is not this page.

Does this rebuild the area moment?

No. I is an input. A rectangle, a circle, and a hollow circle stay on their section pages.

Is a cantilever or a point load included?

No. A cantilever and a concentrated load are their own pages.