Dynamics and Vibration Formulae
Natural frequency, damping ratio, dynamic magnification, PSD units, RMS and modal effective mass relationships for SDOF and MDOF systems.
SDOF System
Natural frequency (angular): ω_n = √(k / m) Natural frequency (Hz): f_n = (1 / 2π) · √(k / m) Damping ratio: ζ = c / (2 · √(k · m)) = c / c_cr Critical damping: c_cr = 2 · √(k · m) Damped natural frequency: ω_d = ω_n · √(1 − ζ²) (ζ < 1)
Dynamic Amplification (SDOF, harmonic excitation)
Frequency ratio:
r = ω / ω_n = f / f_n
Dynamic magnification factor:
1
DMF = ─────────────────────
√[(1 − r²)² + (2ζr)²]
At resonance (r = 1):
DMF = 1 / (2ζ) = Q
Logarithmic decrement:
δ = (1/n) · ln(x_i / x_{i+n}) = 2πζ / √(1 − ζ²)
(≈ 2πζ for small ζ)Random Vibration
PSD definition: S(f) = lim [G(f) / Δf] (units: g²/Hz or (m/s²)²/Hz) Overall RMS from PSD: σ_RMS = √[ ∫ S(f) df ] 3-sigma stress (Gaussian): σ_3σ = 3 · σ_RMS Margin of safety: MS = (σ_allow / σ_3σ) − 1
Modal Effective Mass
Modal effective mass (mode j, direction i):
M_eff,j,i = (L_j,i)² / M_j
where L_j,i = φ_j^T · M · e_i (participation factor)
M_j = φ_j^T · M · φ_j (generalised mass)
e_i = influence vector (unit displacement in direction i)
Cumulative effective mass:
Σ M_eff,j,i → M_total (as sufficient modes are included)
Rule: include modes until Σ M_eff > 90% of total mass in the excitation direction.Variables
| Symbol | Definition | Units |
|---|---|---|
| ω_n | Natural angular frequency | rad/s |
| f_n | Natural frequency | Hz |
| k | Stiffness | N/m |
| m | Mass | kg |
| c | Damping coefficient | N·s/m |
| ζ | Damping ratio | — |
| c_cr | Critical damping | N·s/m |
| Q | Quality factor (resonance amplification) | — |
| r | Frequency ratio (ω/ω_n) | — |
| DMF | Dynamic magnification factor | — |
| S(f) | Power spectral density | g²/Hz |
| σ_RMS | Root-mean-square response | varies |
| M_eff | Modal effective mass | kg |
Notes and Limitations
- SDOF formulae apply to single-mode response — for multi-mode response, use modal superposition
- PSD-based RMS assumes a stationary Gaussian random process
- The 3-sigma criterion (99.7% of peaks) may be exceeded for narrowband response — use the exact peak factor
- Damping ratio ζ is typically 0.01-0.05 for aerospace metallic structures, 0.03-0.08 for bolted/joint-rich structures
Related Knowledge
See the Dynamics, Vibration & Shock Knowledge category for modal theory and random vibration. See How to Perform a Modal Analysis and related guides.