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To investigate the mechanism of wave trapping, acoustic embedded trapped modes associated with two-resonant-mode interference in two-dimensional duct-cavity structures are calculated by the feedback-loop closure principle, which allows us to analyze the traveling modes that construct the trapped modes. The exact two coexisting resonant modes that underpin an embedded trapped mode in a cavity open to two semi-infinite ducts are numerically demonstrated. At the interface between the cavity segment and a duct, total reflection can occur for a particular combination of two propagative guided waves in the cavity. With a particular cavity length and a particular frequency, total reflection also happens for the two reflected waves at the opposite end of the cavity. In this way, the two coexisting standing waves underpin a trapped mode. It is found that the two standing waves are not two closed-cavity modes. Thus, this work presents a new understanding of such embedded trapped modes as a product of total reflection of two guided waves at the interface between two waveguides, rather than interference between two eigenmodes of a closed cavity. Such total reflection of multiple guide modes is a result of mutual cancellation in transmission to the propagative channel(s) of the ducts. Thus, trapped modes involving more than two standing waves may occur at higher frequencies where more traveling modes in the ducts are propagative. For quasi-trapped modes, the Fano scattering phenomenon owing to the effects of two acoustic channels is also shown. [ABSTRACT FROM AUTHOR]

This paper presents a theoretical study of the nonlinear acoustic properties of a slit in a thin plate subjected to high-intensity sound excitation. In the present model, the conventional discrete vortex method is employed to simulate the near-field two-dimensional unsteady flow in order to capture the mechanism of the sound-vortex interaction, which is in combination with a spanwise-averaged three-dimensional Green's function method used to connect the near-field flow quantities with the far-field sound pressure. This model is compared with an existing particle image velocimetry flow visualization and a direct numerical simulation model, showing good qualitative agreement. It is revealed that the oscillatory slit flow is dominated by a pair of spiral-like counter-rotating vortices moving away from the slit and eventually colliding into each other. Because of the vortical flow effect, increases in the sound pressure level result in significant increases in acoustic resistance and modest decreases in acoustic reactance. For the parametric range in this study, increases in the aspect ratio of the slit result in slight increases in acoustic resistance but unnegligible reductions in acoustic reactance. However, the influence of the aspect ratio on acoustic impedance tends to be less important when the sound pressure level exceeds a certain high value. [ABSTRACT FROM AUTHOR]