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. Author manuscript; available in PMC: 2008 Apr 12.
Published in final edited form as: J Acoust Soc Am. 2004 May;115(5 Pt 1):1942–1954. doi: 10.1121/1.1687835

FIG. 5.

FIG. 5

A comparison of measured computation times for beam patterns calculated with a constant number of Gauss abscissas using the expressions H1, H2, H3, and H4. As in Fig. 4, each beam pattern is computed on the same spatial grid as Fig. 3 for a piston with radius a = 5λ. A single sector that covers the entire computational grid in Fig. 1 is defined for these computations. A comparison of the raw computation times indicates that, for the same number of Gauss abscissas, the times required to compute the pressure field using the expressions in H2, H3, and H4 are roughly the same, although H3 (dot dash) is somewhat slower because of the additional complex term in the numerator of Eq. (7). Likewise, for the source geometry and computational grid evaluated here, the expressions H2, H3, and H4 are all nearly three times faster than the impulse response solution H1 (dotted line).