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. Author manuscript; available in PMC: 2008 Sep 13.
Published in final edited form as: J Acoust Soc Am. 2008 Jun;123(6):4071–4081. doi: 10.1121/1.2903865

FIG. 5.

FIG. 5

Angular variation of the peak pressure of laser-generated shock waves near F1, in the plane (a) Θ=90° and (b) φ=90°. Measurements were made at a stand-off distance of 3 mm from the laser spark, PRF=5 Hz, using signal averaging over 20 shots. Error bars represent standard deviation from three independent experiments.