Resources · Nonlinear acoustics

Nonlinear acoustic plane waves

Wave steepening, shock formation, N-waves and sonic booms.

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At finite amplitude, an acoustic waveform can change shape as it propagates. For a fluid with a positive coefficient of nonlinearity, compressions travel faster than rarefactions. The waveform steepens and energy transfers into higher harmonics. Dissipation competes with this steepening and gives real shock fronts a finite thickness.

Steepening of a sinusoidal wave

For an initially sinusoidal, progressive plane wave, an inviscid, weakly nonlinear model predicts the shock-formation distance

\[z_s=\frac{c_0^2}{\beta\omega_0v_0} =\frac{\rho_0c_0^3}{\beta\omega_0p_0},\qquad \beta=1+\frac{B}{2A}.\]

Here, \(p_0\) and \(v_0=p_0/(\rho_0c_0)\) are positive pressure and particle-velocity amplitudes at the source, \(\omega_0\) is angular frequency, and \(B/A\) is the equation-of-state nonlinearity parameter. This distance is a lossless reference scale, not a prediction of an infinitely sharp front in a dissipative fluid.

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Steepening of a finite-amplitude plane wave.
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A closer view of the waveform.

Single-cycle pulses and polarity

A pulse that starts with compression and ends with rarefaction can develop an N-shaped waveform with steep outer fronts. Reversing the polarity changes where the characteristic lines converge and can produce a steep transition near the pulse centre. Pulse duration, amplitude and dissipation all affect the evolution.

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Compression followed by rarefaction.
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Opposite initial polarity.
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Detail of the N-shaped pulse.
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Detail of the opposite-polarity pulse.

Sonic booms

A sonic boom is associated with shock waves generated during supersonic motion. A vehicle produces them continuously while flying supersonically; an observer hears the boom when the shock system reaches their position. It is not a sound emitted only at the instant the vehicle crosses Mach 1.

Recorded space-shuttle sonic-boom pressure waveform
Space-shuttle sonic-boom waveform from the original collection; see Young (2002).
Space shuttle in flight with a visible condensation cloud
Condensation around a space shuttle. A visible cloud is not a direct image of an acoustic shock or proof of crossing Mach 1.

Whip cracking provides another example of rapid motion and shock formation, although its mechanics differ from plane-wave steepening in a stationary fluid.

References & further reading