HomeCalculatorsPhysicsStatics & StrengthUniform Load at a Station Calculator
Physics calculator

Uniform Load at a Station Calculator

Deflection at station x on a simply supported uniform load. δ = w x (L³ − 2 L x² + x³) / (24 E I). 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
Deflection at a stated station on a simply supported span with a uniform load.
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 aa8a253223c1
Legacy regression
3/3 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 · 1/1 CVP boundary · 1/1 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 — uniform load
Sources
Evidence
2 legacy golden · 1 legacy boundary · legacy regression suite · 1/1 oracle-backed golden · 1/1 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.

Deflection at xδ = w x (L³ − 2 L x² + x³) / (24 E I)
ix = L/2 is the midspan uniform-load page.

How to use

1

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

x must lie strictly between the supports.

2

Read the deflection at that station

The sign of w is the sign of δ.

Example calculations

Common configurations with formula and result.

ϟ

Midspan

w = 24, x = 1, L = 2, E = 1, I = 1

δ = 5 w L⁴ / (384 E I)
δ = 5
ϟ

Quarter span

w = 24, x = 0.5, L = 2, E = 1, I = 1

δ = 57 w L⁴ / (6144 E I)
δ = 3.5625

Uniform Load at a Station 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. The deflection at station x from the left support is δ = w x (L³ − 2 L x² + x³) / (24 E I).
What it calculates
Deflection at a stated station on a simply supported span with a uniform load.
Inputs
  • w
  • x
  • L
  • E
  • I
Outputs
  • delta
Formula
δ = w x (L³ − 2 L x² + x³) / (24 E I).
Assumptions
  • Calculation runs locally in the browser; values are not uploaded.
  • Keep units consistent with the labels on each field.
  • x = L/2 is the midspan uniform-load page.
Units
  • w, x, L, E, and I set the deflection unit.
Boundary conditions
  • missing w, x, L, E, or I → MISSING_REQUIRED_INPUT
  • L ≤ 0, E ≤ 0, or I ≤ 0 → VALUE_MUST_BE_POSITIVE
  • x ≤ 0 or x ≥ L → INVALID_INPUT
Example
w=24 x=1 L=2 E=1 I=1 → δ=5
Validation cases

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

  • w=24 x=1 L=2 E=1 I=1 → δ=5
  • w=24 x=0.5 L=2 E=1 I=1 → δ=3.5625
  • x=0 → INVALID_INPUT
Sources
  • Hibbeler, Mechanics of Materials — Deflection of beams — simply supported beam with a uniform load
    Supports: The elastic curve is δ = w x (L³ − 2 L x² + x³) / (24 E I).
  • Gere and Goodno, Mechanics of Materials — Deflection of beams — uniform load
    Supports: Supports the page formula. x = L/2 recovers 5 w L⁴ / (384 E I).
Calculation version
1.0.0

Background

Interpretation and common distinctions.

Find the deflection at a stated station on a simply supported span with a uniform load.

Supported and not supported

Supported: δ = w x (L³ − 2 L x² + x³) / (24 E I). x = L/2 is the midspan page.

Not supported: a station at a support, and a cantilever. /calc/mechanical is not open.

Agent / API notes

Capability id: mechanical.statics.uniform_load_at_deflection · tool id: uniform-load-at · pin 1.0.0.

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

Other calculators in this family: Angled Pull Calculator, Angled Pull on an Incline Calculator, Area Moment Calculator, Beam Deflection Calculator, Beam Moment Deflection Calculator, Beam Moment Maximum Deflection Calculator, Bending Stress Calculator, Cantilever Deflection Calculator . Explore all Statics & Strength.

→ Angled Pull Calculator Pull at an angle above the horizontal that puts a block on a level surface at impending slip. The normal is W − P sinα. Runs locally. › → Angled Pull on an Incline Calculator The pull at an angle above the horizontal that puts a block on an incline at impending slip. α = 0 is horizontal. α = θ is parallel to the plane. Runs locally. › → Area Moment Calculator Second moment of composite plane areas about the composite centroid. Supply each part's centroidal Ix and Iy. Runs locally. Not a section modulus and not a beam calculator. › → Beam Deflection Calculator Midspan deflection of a simply supported span with one concentrated load. δ = P L³/(48 E I). I is an input. Runs locally. › → Beam Moment Deflection Calculator Midspan deflection of a simply supported span with one end moment. δ = M L²/(16 E I). I is an input. Runs locally. › → Beam Moment Maximum Deflection Calculator Largest deflection of a simply supported span with one end moment. δ = M L²/(9√3 E I) at x = L/√3. I is an input. Runs locally. › → Bending Stress Calculator Elastic bending stress from a moment and a section modulus. S can also be formed from Ix and c. Runs locally. › → Cantilever Deflection Calculator Free-end deflection of a cantilever with one concentrated load at the tip. δ = P L³/(3 E I). I is an input. Runs locally. ›

Frequently asked questions

Key distinctions behind the calculation.

Is the other quarter the same?

Yes. x and L − x give the same deflection.