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So apart from minor changes in notation, this is identical to the exact boundary integral result. A rather remarkable consequence of equation (P6) is that for a constant value of u0, on the z-axis the pressure is a linear function of frequency from DC up. Considering the complex behavior that occurs as a function of frequency, this is extraordinary.
Sound Pressure in the Near-field
Substituting the solution for D(b ) into equation (P2), the pressure at an arbitrary point in space is
This integral is tricky to evaluate numerically. To obtain results at the baffle surface z=0 it is best to divide the integration range into 3 segments. The first segment from 0 to 4k is evaluated using a change of variables b =sing . From 4k to 10k the form above works best. The final infinite segment can be evaluated as a Weber-Schefheitlin type integral [NBS Handbook equations 11.4.33 and 11.4.34] less another numerical integration. A plot of the pressure at the baffle surface z=0 shows the result of this equation as solid lines, for ka=2p [30kb]. The piston velocity profile is in blue. Pressure is normalized by Zo, so it is expected to approach the velocity value of 1.0 for large ka. The result of the boundary integral is shown by the dots. A rather dense set of integration points were used, spaced .01 wavelengths apart. The pressure was evaluated at z=.05 wavelengths, and then a phase shift applied to approximate the surface value. Finally, the results of the numerical solution are shown, as the dashed line. I am quite happy with the agreement between these three results. The boundary integral is off a bit, but the agreement between the other two is pretty darn good. In all of the remaining plots, the exact equation result is shown as a solid line, and the numerical result as dashed. The agreement so good you have to look carefully in some cases to see that there really are two curves.