Section Modulus Calculator
Elastic section modulus of a composite plane area about its centroid. Sx = Ix/cy and Sy = Iy/cx. Ix and Iy come from the area-moment engine. Runs locally. Not bending stress and not beam deflection.
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
- Elastic section modulus of a composite plane area about its centroidal x and y axes.
- 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 e32986c1101c
- Legacy regression
- 6/6 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
- Supplemental domain review
- Not performed
- Named expert review
- Not performed
- CVP suite
- 1/1 golden · 4/4 CVP boundary · 3/3 invalid · 1/1 cross-interface · 6/6 CVP contract · Manifest
- Sources
- Hibbeler, Engineering Mechanics: Statics
- Gere and Goodno, Mechanics of Materials
- Evidence
- 2 legacy golden · 4 legacy boundary · legacy regression suite · 1/1 oracle-backed golden · 3/3 invalid · Artifact integrity PASS
- Semantic contract
- PASS
Full verification
Formulas
Core equations used by this calculator.
How to use
Enter the parts
Each row is centroidal Ix, Iy, A, x, y. A negative area is a hole.
Enter the fiber distances
cy is the distance from the centroid to the extreme fiber for Sx. cx is the same distance for Sy. Enter one or both.
Read Sx and Sy
A blank distance omits that modulus. Both distances must be positive.
Example calculations
Common configurations with formula and result.
Both axes
Ix = 16, Iy = 4, cy = 2, cx = 1
Sx only
Two unit areas at y = 0 and y = 2, cy = 1
Section Modulus calculator specification
Version 1.0.0 · Engine tested
- Engine tested 6/6 tests · Production surface contract 6/6
- Named expert review Not performed
- Calculation version 1.0.0
- Definition
- Sx = Ix/cy and Sy = Iy/cx. Ix and Iy are the centroidal second moments of the composite area. cx and cy are distances from that centroid to the extreme fiber.
- What it calculates
- Elastic section modulus of a composite plane area about its centroidal x and y axes.
- Inputs
- parts
- cx?
- cy?
- Outputs
- Sx
- Sy
- Ix
- Iy
- x_bar
- y_bar
- area
- Formula
Sx = Ix/cy, Sy = Iy/cx- Assumptions
- Calculation runs locally in the browser; values are not uploaded.
- Keep units consistent with the labels on each field.
- Ix and Iy are shifted to the composite centroid by the area-moment engine. This page does not build a rectangle from b and h, does not return σ = M/S, and does not use the principal axes.
- Units
- Keep second moment and fiber distance in one consistent unit system. S has dimension length³.
- Boundary conditions
- no parts → MISSING_REQUIRED_INPUT
- neither cx nor cy → MISSING_REQUIRED_INPUT
- cx or cy ≤ 0 → VALUE_MUST_BE_POSITIVE
- Ix < 0 when cy is set, or Iy < 0 when cx is set → INVALID_INPUT
- Example
- parts=16,4,4,0,0 cx=1 cy=2 → Sx=8, Sy=4
- Validation cases
3 published on this page · 6/6 tests · Production surface contract 6/6 · View evidence
- parts=16,4,4,0,0 cx=1 cy=2 → Sx=8, Sy=4, Ix=16, Iy=4
- parts=1,0,1,0,0; 1,0,1,0,2 cy=1 → Sx=4, Ix=4
- parts=16,4,4,0,0 cy=0 → VALUE_MUST_BE_POSITIVE
- Sources
- Hibbeler, Engineering Mechanics: Statics — Moments of inertiaSupports: Elastic section modulus S = I/c, with c the distance from the centroid to the extreme fiber
- Gere and Goodno, Mechanics of Materials — Moments of inertiaSupports: Supports the page formula: Sx = Ix / cy
- Hibbeler, Engineering Mechanics: Statics — Moments of inertia
- Calculation version
- 1.0.0
Background
Interpretation and common distinctions.
Find the elastic section modulus of a composite plane area about its centroid.
Supported and not supported
Supported: Sx = Ix/cy and Sy = Iy/cx after the area-moment engine shifts each part to the composite centroid.
Not supported: bending stress, plastic modulus, a rectangle built from b and h, modulus about the principal axes, and beam deflection. /calc/mechanical is not open.
Agent / API notes
Capability id: mechanical.statics.section_modulus · tool id: section-modulus · pin 1.0.0.
{ "parts": "16,4,4,0,0", "cx": 1, "cy": 2 }
Share the link with parts, cx, and cy. The result is not written into the link.
Related tools
Other calculators in this family: Area Moment Calculator, Circular Section Calculator, Hollow Circular Section Calculator, Inclined-Axis Moment Calculator, Plane Centroid Calculator, Principal Moment Calculator, Principal Section Modulus Calculator, Rectangular Section Calculator . Explore all Section Properties.
Frequently asked questions
Key distinctions behind the calculation.
Does this compute bending stress?
No. It returns the elastic section modulus S = I/c. Bending stress σ = M/S, plastic modulus, and material allowables are out of scope.
Does this build a rectangle from width and height?
A solid rectangle from width and height is the rectangular-section page. This page takes centroidal Ix and Iy you already have. For that rectangle, Sx = b h²/6.
Is this the principal-axis modulus?
No. Sx and Sy use Ix and Iy about axes parallel to x and y. Principal-axis modulus is on the principal-section-modulus page.