Ohmic Audio

⚙️ ENGINEER LEVEL: Modal Analysis and Loss Mechanisms

Finite Element Analysis for Enclosure Design

Panel vibration is a distributed-parameter problem — the response at every point on the panel depends on geometry, boundary conditions (how the edges are supported), material properties, and excitation.

Modal frequencies of a simply-supported rectangular panel:

f_mn = (π/2) × √(D/ρ_s) × √[(m/Lx)² + (n/Ly)²]

Where: - D = flexural rigidity = E×h³ / (12(1−ν²)) - ρ_s = surface mass density (kg/m²) - m, n = mode numbers (1,2,3...) - Lx, Ly = panel dimensions

For 3/4" MDF (E = 3 GPa, ρ = 750 kg/m³, ν = 0.3), 400mm × 500mm panel:

D = 3×10⁹ × (0.019)³ / (12 × (1−0.09)) = 1,897 N·m
ρ_s = 750 × 0.019 = 14.25 kg/m²

f_11 = (π/2) × √(1897/14.25) × √[(1/0.4)² + (1/0.5)²]
     = 1.571 × 11.53 × √(6.25 + 4.0)
     = 18.12 × 3.20
     = 58 Hz

The first panel mode at 58 Hz is squarely in subwoofer territory. This panel resonates at every bass note near 58 Hz — adding colored output that doesn't come from the driver.

Effect of bracing:

Adding a cross-brace at the panel center divides each dimension by approximately √2, raising f_11 by a factor of 2:

f_11_braced ≈ f_11 × 2 = 116 Hz

Still within problematic territory for some builds. Add a second brace for f_11 × 3 = 174 Hz — above most subwoofer crossover points.

Constrained Layer Damping — Loss Factor Calculation:

Layered cross-section of constrained layer damping showing the base panel, viscoelastic damping layer, constraining sheet, and the shear deformation that dissipates panel energy.
CLD works because the thin damping layer gets sheared between the main panel and the constraining sheet. That shearing wastes vibrational energy each cycle, which lowers ringing without pretending the base panel has become infinitely rigid.

When a viscoelastic layer is sandwiched between the base panel and a constraining layer, bending of the base causes shear in the viscoelastic layer. Shear dissipates energy.

System loss factor:

η_total = η_v × H_c × g_c / (1 + g_c)

Where: - ηv = loss factor of viscoelastic layer (0.5–2.0 for butyl) - Hc = thickness parameter ratio - g_c = shear parameter

For practical CLD with butyl damping compound (2mm thick) on 19mm MDF:

Achievable η_total ≈ 0.1–0.3

Effect on Q of panel resonance:

Q_panel = 1 / η_total

Undamped: Q = 50–100 (sharp, ringing resonance) With CLD: Q = 3–10 (well-damped, minimal coloration)

Reduction in resonance peak:

Reduction_dB = 20 × log₁₀(Q_undamped / Q_damped)
             = 20 × log₁₀(50/5) = 20 dB

10.6 Advanced Subwoofer Integration