This formulation models a 16-channel ($4 \times 4$) beamforming audio array utilizing Distributed Mode Loudspeakers (DML). Accurate acoustic steering requires solving for both the spatial interference patterns and the structural modality of the individual radiating planes.
Assuming the array lies in the $xy$-plane, radiating forward along the $z$-axis. With elements at coordinates $(x_n, y_m)$, the far-field complex Array Factor (AF) at elevation angle $\theta$ (from the $z$-axis) and azimuth angle $\phi$ (in the $xy$-plane) is computed as a phasor summation:
Where $k = \frac{2\pi}{\lambda}$ is the wavenumber, $w_{nm}$ is the amplitude weight (coherence) of the specific element, and $\Delta\Phi_{nm}$ is the programmatic phase shift required to steer the main lobe to target coordinates $(\theta_0, \phi_0)$:
The transverse out-of-plane displacement $W(x,y,t)$ of a compliant DML plate is governed by the biharmonic equation:
Symmetrical plates generate degenerate eigenmodes (Chladni patterns) that severely degrade phase coherence. We suppress these by breaking geometric symmetry: applying off-center excitation and distributing localized backing weights in a Fibonacci spiral to disrupt nodal formation:
To transition from continuous analytical boundaries to a real-time visualization and design tool, the continuous surface integrals must be discretized and optimized algorithmically.
Visualizing structural symmetry breaking. Red/Blue = phase. White = nodal lines.
Pausing will sync the optimized geometry back to Tab 2 for detailed 2D analysis.
Warning: Ensure system volume is low. Audio clarity and amplitude scale aggressively with mathematical fitness $J$.