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Sandbox Physics

M066 · A driven bending plate

Chladni Plate Resonance

Move a point driver over a three-dimensional thin plate. Tune a resonance, split a degenerate pair by stretching the rectangle, and suppress a mode by driving on its node.

Interactive modelChladni Plate Resonance
Selected natural frequency0 Hz0\,\mathrm{Hz}
Selected / fundamental frequency00
Gold-point displacement0 μm0\,\mathrm{\mu m}
Gold-point RMS displacement0 μm0\,\mathrm{\mu m}
Actual height magnification00
Displayed mechanical energy0 μJ0\,\mathrm{\mu J}
Mean input power0 μW0\,\mathrm{\mu W}

Physics tutorial

Bending makes a different spectrum

BackgroundA thin solid plate resists curvature. Its bending stiffness, thickness and boundary conditions determine its natural vibrations.

Why it mattersConnect the moving surface, quiet lines and a quantitative frequency account.

Start with the essentials

Focus question
Can a resonant mode stay quiet when its driver sits on a node?
One-sentence intuition
Resonance needs both frequency matching and spatial coupling. A nodal driver has zero coupling to that mode.

Core mathematical model

Specified parameters

E=70 GPa,ν=0.33,ρ=2700 kg/m3,F0=0.2 mNE=70\,\mathrm{GPa},\quad\nu=0.33,\quad\rho=2700\,\mathrm{kg/m^3},\quad F_0=0.2\,\mathrm{mN}

Uniform material parameters are teaching assumptions. The small force keeps this linear plate in its small-deflection range.

Bending equation

D∇4w+ρh w¨=p,D=Eh312(1−ν2)D\nabla^4w+\rho h\,\ddot w=p,\qquad D=\frac{Eh^3}{12(1-\nu^2)}

Kirchhoff–Love theory, uniform thickness and isotropic linear elasticity. The prescribed modal damping is added after projection.

Simply supported rectangle

ϕmn=sin⁡mπxasin⁡nπyb,ωmn=π2Dρh(m2a2+n2b2)\phi_{mn}=\sin\frac{m\pi x}{a}\sin\frac{n\pi y}{b},\quad \omega_{mn}=\pi^2\sqrt{\frac{D}{\rho h}}\left(\frac{m^2}{a^2}+\frac{n^2}{b^2}\right)

Positive integer indices start at one. At the edges displacement and normal bending moment vanish; the slope is not clamped.

Complex modal response

Qmn=F0ϕmn(xd,yd)Mmn(ωmn2−Ω2+2iζωmnΩ),Mmn=ρhab4Q_{mn}=\frac{F_0\phi_{mn}(x_d,y_d)}{M_{mn}(\omega_{mn}^2-\Omega^2+2i\zeta\omega_{mn}\Omega)},\quad M_{mn}=\frac{\rho hab}{4}

The displayed displacement is the real part of the modal sum times the complex driving phase. All retained modes participate.

An independent power account

P‾in=−F0Ω2∑mnϕmn(xd,yd)Im⁡Qmn=∑mnζMmnωmnΩ2∣Qmn∣2\overline P_{\rm in}=-\frac{F_0\Omega}{2}\sum_{mn}\phi_{mn}(x_d,y_d)\operatorname{Im}Q_{mn}=\sum_{mn}\zeta M_{mn}\omega_{mn}\Omega^2|Q_{mn}|^2

In steady state, mean input power equals mean viscous dissipation. This does not assert constant instantaneous energy.

Common difficulties

An amplitude map is not sand

Typical misconceptionEvery pale line predicts a measured sand pattern.

Better mental modelThis map is computed RMS displacement in a linear model. Granular motion, friction, air and real support compliance are outside its scope.

Run the experiment

  1. 01

    Drive on a node

    Compare Four lobes with Drive on a node. Keep the selected frequency unchanged.

    What to observe: The selected mode is suppressed, although other off-resonant modes can still move.
  2. 02

    Split equal frequencies

    Try Degenerate pair, then Break the symmetry. Use Tune to selected mode after changing the aspect ratio.

    What to observe: The two swapped mode indices share a square frequency but separate on a rectangle.
  3. 03

    Separate physics from display

    Double thickness, then vary only the height display gain.

    What to observe: Thickness doubles natural frequency. Display gain leaves the physical trace and power unchanged.

Primary sources: NASA SP-160 · Vibration of PlatesExperimental simply supported plates

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