Research Article

Focusing Modeling of OPFC Linear Array Transducer by Using Distributed Point Source Method

Figure 12

Acoustic pressure in the - plane in different interaction effects. (a) Acoustic pressure in the - plane for steering angle 0. (b) Acoustic pressure in the - plane when the interaction effect is considered.
840748.fig.0012a
(a)
840748.fig.0012b
(b)