← Back to demos

Modal Sound Explorer

Interactive modal vibration and sound synthesis. Click an object to strike it and hear its modes.
(Inspired by the Sonic Explorer demo from [van den Doel and Pai 1998])

Object Type
1D wave equation, fixed-fixed boundary conditions
Material Preset
Frequency & Damping
440 Hz
1.0
Low modes decay faster →
2.0e-6
High modes decay faster →
Modes
12
About the physics model

When a solid object is struck, the impact excites vibrational modes, which are standing wave patterns each with its own frequency, spatial shape, and decay rate. The total sound is the superposition of all excited modes, each ringing as a decaying sinusoid [1].

This demo implements four analytical models from classical vibration theory, organized by spatial dimension (1D or 2D) and restoring-force type (tension or bending stiffness):

The key perceptual distinction is between harmonic and inharmonic spectra. When mode frequencies fall in integer ratios (as in the string), the auditory system fuses them into a single pitch. When they do not (as in the beam, membrane, and plate), the result is a more complex, often metallic or percussive timbre without a clearly defined pitch [1, 4, 5].

Strike-position coupling: The excitation amplitude of mode n is proportional to the mode shape evaluated at the strike point, ψn(xs). Striking a nodal line (where ψn = 0) silences that mode entirely [1].

Rayleigh damping models energy dissipation as D = αM + βK. In the modal domain, mode n has decay rate αn = α/2 + β ωn2/2. The α term gives a constant decay rate across all modes (mass-proportional); the β term preferentially damps high-frequency modes (stiffness-proportional). Their balance determines material character: metals have low α and β (long ring), wood has high α (short, warm), rubber has both high (dead thud) [3].

Material presets are perceptually tuned within physically plausible ranges. The implied loss factors (η = 2ξ) at each preset's fundamental frequency fall within values reported in the vibration engineering literature: steel and glass at η ≈ 0.006, aluminum at η ≈ 0.014, ceramic at η ≈ 0.04, wood at η ≈ 0.1, and rubber at η ≈ 1.0 [8, 9]. The fundamental frequencies are free parameters chosen for perceptual clarity; in physical objects they would be determined by geometry, density, and stiffness.

Appendix: Material Preset Values

Each preset sets three Rayleigh damping parameters. The table below shows the preset values and the physical quantities they imply at the fundamental frequency.

Material f1 (Hz) α (1/s) β (s) ξ1 η1 T60 (s)
Steel 440 1.0 2×10−6 0.003 0.006 1.70
Aluminum 520 2.0 4×10−6 0.007 0.014 0.62
Glass 880 0.5 1×10−6 0.003 0.006 0.89
Wood 220 40.0 5×10−5 0.049 0.098 0.20
Ceramic 660 5.0 1×10−5 0.021 0.043 0.16
Rubber 110 200 1×10−3 0.49 0.98 0.04

ξ1 is the damping ratio (fraction of critical damping) at the fundamental: ξ = α/(2ω) + βω/2. η1 = 2ξ is the loss factor, the quantity typically tabulated in materials science handbooks. T60 is the time for the fundamental mode to decay by 60 dB (a factor of 1000 in amplitude): T60 = 6 ln(10)/decay ≈ 13.8/decay.

References

  1. K. van den Doel and D. K. Pai, “The Sounds of Physical Shapes,” Presence, vol. 7, no. 4, pp. 382–395, 1998. doi:10.1162/105474698565794
  2. C. Zheng and D. L. James, “Rigid-Body Fracture Sound with Precomputed Soundbanks,” ACM Trans. Graph. (SIGGRAPH 2010), vol. 29, no. 3, pp. 1–13, 2010. doi:10.1145/1778765.1778806
  3. D. L. James, T. R. Langlois, R. Mehra, and C. Zheng, “Physically Based Sound for Computer Animation and Virtual Environments,” in ACM SIGGRAPH 2016 Courses (SIGGRAPH ’16), Article 22, 2016. doi:10.1145/2897826.2927375 · Project page
  4. T. D. Rossing and N. H. Fletcher, Principles of Vibration and Sound, 2nd ed. Springer, 2004. doi:10.1007/978-1-4757-3822-3
  5. N. H. Fletcher and T. D. Rossing, The Physics of Musical Instruments, 2nd ed. Springer, 1998. Chapters 2–3 (vibrating strings, bars, membranes, plates). doi:10.1007/978-0-387-21603-4
  6. R. D. Blevins, Formulas for Natural Frequency and Mode Shape. Van Nostrand Reinhold, 1979. Table 8-1 (beam eigenvalues). doi:10.1007/978-3-319-05868-1
  7. A. W. Leissa, Vibration of Plates, NASA SP-160, 1969. NASA Technical Reports
  8. L. Cremer, M. Heckl, and B. A. T. Petersson, Structure-Borne Sound: Structural Vibrations and Sound Radiation at Audio Frequencies, 3rd ed. Springer, 2005. doi:10.1007/b137728
  9. A. D. Nashif, D. I. G. Jones, and J. P. Henderson, Vibration Damping. Wiley, 1985. ISBN: 978-0471867722. Publisher page