Traveling Sound Waves — Question 9

Section 17-3 · Physics pages 2688–2689

Question 9 Density and velocity obey a local conservation law Linear acoustic continuity is δρt + ρ0ux = 0 and the pressure response is p = c2δρ. For p = P cos(kx −ωt), use ω = ck and no background flow. x c Compression reflects a local change in density caused by converging particle motion. (a) Derive u directly from continuity and recover the progressive-wave impedance relation. (b) For P = 4.0 Pa, c = 400 m/s and ρ0 = 1.0 kg/m3, calculate density amplitude and maximum fractional density change.
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Question 9 - Solution Density and velocity obey a local conservation law x c (a) Method and calculation The density field is δρ = (P/c2) cos Φ. Hence δρt = ωP c2 sin Φ, ux = −ωP ρ0c2 sin Φ. Integrating in x with no uniform-flow component gives u = ωP ρ0c2k cos Φ = P ρ0c cos Φ. (b) Interpretation and further calculation The numerical density amplitude is δρm = 4 4002 = 2.50 × 10−5 kg/m3, δρm ρ0 = 2.50 × 10−5. The velocity amplitude is 4/(1 × 400) = 0.010 m/s. Continuity and momentum therefore lead to the same impedance relation. Physical check The fractional density perturbation equals um/c for a progressive linear wave. Both are small here.

Question 9

Density and velocity obey a local conservation law

Linear acoustic continuity is δρt+ρ0ux=0\delta\rho_t+\rho_0u_x=0 and the pressure response is p=c2δρp=c^2\delta\rho. For p=Pcos⁡(kx−ωt)p=P\cos(kx-\omega t), use ω=ck\omega=ck and no background flow.

Diagram shown in the original SVG worksheet.

  1. Derive uu directly from continuity and recover the progressive-wave impedance relation.

  2. For P=4.0PaP=4.0\,\mathrm{Pa}, c=400m/sc=400\,\mathrm{m/s} and ρ0=1.0kg/m3\rho_0=1.0\,\mathrm{kg/m^3}, calculate density amplitude and maximum fractional density change.

Question 9 - Solution

Density and velocity obey a local conservation law

Diagram shown in the original SVG worksheet.

(a) Method and calculation

The density field is δρ=(P/c2)cos⁡Φ\delta\rho=(P/c^2)\cos\Phi. Henceδρt=ωPc2sin⁡Φ,ux=−ωPρ0c2sin⁡Φ.\delta\rho_t=\frac{\omega P}{c^2}\sin\Phi,\qquad u_x=-\frac{\omega P}{\rho_0c^2}\sin\Phi.Integrating in xx with no uniform-flow component givesu=ωPρ0c2kcos⁡Φ=Pρ0ccos⁡Φ.u=\frac{\omega P}{\rho_0c^2k}\cos\Phi=\frac P{\rho_0c}\cos\Phi.

(b) Interpretation and further calculation

The numerical density amplitude isδρm=44002=2.50×10−5kg/m3,δρmρ0=2.50×10−5.\delta\rho_m=\frac4{400^2}=2.50\times10^{-5}\,\mathrm{kg/m^3},\qquad\frac{\delta\rho_m}{\rho_0}=2.50\times10^{-5}.The velocity amplitude is 4/(1×400)=0.010m/s4/(1\times400)=0.010\,\mathrm{m/s}. Continuity and momentum therefore lead to the same impedance relation.

Physical check

The fractional density perturbation equals um/cu_m/c for a progressive linear wave. Both are small here.