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In an answer, there is this equation:

$$p = \frac{\rho S_D}{2 \pi r} \, a$$

This describes that the sound pressure ($p$) is proportional to the acceleration ($a$) of the cone of a loudspeaker.

($\rho$ is the density of air, $S_D$ is the surface area of the cone, and $r$ is the distance from the cone)

I wonder, where does this equation come from? What's the theory behind it?

geza
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1 Answers1

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To derive this result, there are various possible starting points. Probably the most rigorous approach is to start from the pressure due to a baffled rigid piston. In this case, at a distance $r$ along the axis of the piston we have

$$p(r,t) = \rho c \left( 1-e^{-ik\phi} \right) v(r,t) \; , $$

where $\rho$ is the density of air, $c$ is the speed of sound,

$$ \phi \doteq \sqrt{r^2+r_0^2} - r \quad\text{and}\quad v(r,t) = v_0 e^{i(\omega t-kr)} \; . $$

Above, $v$ is the (oscillating) piston velocity and $r_0$ is the piston radius. This textbook result can be found, for example, in Section 7.4 of Kinsler (4th Ed). Note that the motion is assumed to be harmonic, such that $\omega$ is the oscillation frequency and $k$ is the wavenumber such that $\omega = ck$. In the far-field, for which $\phi \ll 1$, this reduces to

$$ p(t) = i \rho c k \phi \, v(t) \; . $$

The presence of the $i$ shows that the velocity is out of phase with the pressure. Since the motion is harmonic, we can rewrite this in terms of the acceleration using $a = \partial_t v = i \omega v$. Then, the complex pressure becomes

$$ p(t) = \rho \phi \, a(t) \; . $$

Taking $r \gg r_0$ gives $\phi \sim r_0^2/(2r)$, or

$$p(t) = \frac{\rho r_0^2}{2r} \, a(t) \; .$$

The area of the cone is $S_D=\pi r_0^2$, so we are left with

$$p(t) = \frac{\rho S_D}{2\pi r} \, a(t) \; .$$

jcandy
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  • Thank you very much for your precise answer! Does this mean, that if I want to approximate the sound pressure (for audible range) from a vibrating plate (~0.5 m size), at a distance of farther than 5 m, it is a good approximation if I take the acceleration of little plate elements, and integrate them? Like if every plate element would be a little loudspeaker. Or is there a better approximation for this? – geza May 11 '18 at 07:35
  • The formula is useful is you want to get the simplest (far-field) approximation for any vibrating element (circular, square, concave, convex). If you want to do better, then you probably want to use a specific, known result. Is your plate circular? Is it baffled? In general you would not sum accelerations; rather, you would solve the problem in such a way as to satisfy normal velocity boundary conditions (some fixed velocity V on the radiator, and V=0 on rigid surfaces). – jcandy May 11 '18 at 15:36
  • I'm dealing with guitar top-plate simulation, so in a way, it is baffled (I mean, the air is mostly closed to the body). Currently, I'm using summed accelerations, and it is kinda okay. I'd just use some alternative solution, if it is not much more complicated, so worth the effort. I'm sorry, I don't understand your last sentence (I'm completely new to acoustics). – geza May 11 '18 at 16:27
  • Much of the effort in solving the Helmholtz equation is connected with satisfying the boundary conditions on all surfaces. The normal velocity must be zero on fixed surfaces (wall, floor, loudspeaker box) and finite on moving surfaces (string, woofer, tweeter, plate). The formula above in terms of acceleration is really not suitable for this. One way to solve the problem is to expand the pressure in terms of point sources with arbitrary amplitudes, then apply the boundary conditions to determine the unknown amplitudes. To get further clarification you'd need to ask this as a question. – jcandy May 11 '18 at 17:08
  • Thanks for the information, you're a great help! I've asked this question. – geza May 11 '18 at 17:38
  • I've just studied your answer, and one thing is not clear to me: if $\omega=ck$ (is it always true, or just an approximation?), then why don't textbooks apply this formula at the beginning? I mean, a lot of equations have $c$, $\omega$ and $k$ in the same equation. Why don't we apply $\omega=ck$, so we can get rid of one of the variables? – geza May 12 '18 at 12:52
  • Its not true for complicated waves (for example in a plasma) but for sound waves in air $\omega = ck$ is always true. I think its simply a matter of convenience to carry around all the symbols. – jcandy May 12 '18 at 18:41
  • @jcandy, how come Kinsler ends up with pressure proportional to acceleration while other sources (e.g. Blackstock) talk about pressure being proportional to velocity? While Blackstock talks about "particle velocity", I'd assume it is equivalent to the piston's velocity. See also: https://www.acs.psu.edu/drussell/Demos/phase-p-u-sine/phase-p-u-sine.html – Bartosz Ciechanowski Sep 09 '22 at 02:12
  • @BartoszCiechanowski The relation between the complex pressure and velocity for this 3D problem is given in the first equation in my original answer. Generally speaking, it is never a direct proportionality. For 1D fluid motion, $\partial p / \partial x = -\rho , \partial u/\partial t$ and $\kappa , \partial p / \partial t = -\partial u/\partial x$ (Morse and Ingard, p243), which for a sinusoidal wave $\sin(kx-\omega t)$ implies proportionality as in Blackstock. – jcandy Sep 10 '22 at 20:58