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Solid mechanics · analytical simulation

Cantilever Beam Mechanics

Inspect how material stiffness, beam dimensions and a free-end point load change deflection, internal forces and elastic bending stress in the public MATLAB example.

Conceptual cantilever beam with a downward free-end load and deflected centreline.
Original conceptual illustration by Ricardo Fitas; not a measured deformation or finite-element result.

Interactive analytical model

Cantilever beam lab

Explore the rectangular Euler–Bernoulli beam encoded in the public MATLAB file. The source preset is 210 GPa, 0.75 m × 20 mm × 15 mm and a 20 N downward free-end load.

Control ranges are browser-demo bounds. The equations assume a prismatic rectangular beam, linear elasticity, small deflection and a point load at the free end; they do not check yielding, shear deformation or buckling.

Second moment I

5.625e-9 m⁴

b h³ / 12

Tip deflection

-2.381 mm

signed downward

Fixed-end moment

-15.000 N·m

source sign convention

Max outer-fibre stress

20.000 MPa

at the fixed support

0.00-1.19-2.380.000.190.380.560.75Beam coordinate x [m]Signed deflection v [mm]
Analytical small-deflection curve. Negative values indicate downward deflection; the vertical plotting scale is fitted to the computed tip value.
Deflection
-0.744 mm
Moment
-7.500 N·m
Shear
20.000 N
Top stress
10.000 MPa
Computed beam response at five equally spaced stations
x [m]v [mm]M [N·m]Q [N]|σ|max [MPa]
0.0000.000-15.00020.00020.000
0.188-0.205-11.25020.00015.000
0.375-0.744-7.50020.00010.000
0.563-1.507-3.75020.0005.000
0.750-2.3810.00020.0000.000

Corrugated Digital Twin · source-bounded paper audit

The published test bench is a different mechanical case

The paper reports a physical corrugated-board test, a digital asset and a regression step. This panel makes that evidence chain inspectable without presenting the live cantilever calculator above as the paper's experiment, dashboard or Digital Twin.

Evidence state

Paper evidence only

No data or asset replay

  1. 1. Physical asset

    Corrugated specimen in a three-point-bending test bench.

  2. 2. Measured response

    Load sensing captures the specimen response and loading-history sensitivity.

  3. 3. Digital asset

    A MATLAB representation and dashboard participate in bidirectional data flow.

  4. 4. Reported estimate

    Linear regression estimates a displacement limit from the measured response.

Comparison between the live analytical cantilever and the published corrugated Digital Twin case
AspectLive beam lab abovePublished Digital Twin case
Mechanical boundaryFixed cantilever with a free-end point load.Physical three-point-bending test bench.
Evidence classExecuted analytical Euler–Bernoulli calculation.Physical test, Digital Twin prototype and regression reported by the paper.
InputsEditable E, L, b, h and load P with explicit SI units.Measured response and a sensor/control protocol; no reusable export is embedded here.
Outputs shown hereDeflection, moment, shear and elastic bending stress.Source evidence only; no sensor replay, MATLAB dashboard or regression result is reproduced.

Rights boundary: All rights reserved; no reuse without permission. No paper figure, measured data or dashboard asset is copied.

Reproduction blocker: The public paper does not grant reuse rights for its assets, and no reusable sensor data, control protocol or source package has been verified.

Decision: Keep the current calculator separate; reproduce the digital-twin case only from an authorized data/protocol export.

Open versioned preprint

Jason E. Djajasaputra and Ricardo Fitas. Authorea preprint v1, posted 11 December 2024. Physical test, digital-twin prototype and regression. This audit records the published case; it does not reproduce or validate its results.

Model, equations and limits

The public source defines a 210 GPa rectangular cantilever, 0.75 m long, 20 mm wide and 15 mm high, with a signed −20 N tip load. This page presents the same case as a positive 20 N downward load and preserves the source sign convention for deflection and moment.

  • I = b h³ / 12 and v(x) = −P x²(3L−x)/(6EI).
  • M(x) = −P(L−x), Q = P and σ = −My/I.
  • The source preset gives −2.381 mm tip deflection and 20.000 MPa maximum outer-fibre stress at the fixed support.
  • Outputs are analytical Euler–Bernoulli calculations, not experimental measurements or a finite-element validation.