Wave Mechanics and Sound Notes

Types of Vibrations

  • Free Vibrations: Vibrations occurring at the body's natural frequency without external periodic forces.
  • Forced or Driven Vibrations: Vibrations caused by an external periodic force (e.g., sonometer wire, resonance tube, microphone diaphragm).
  • Resonance: A special case of forced vibration where the external driving frequency matches the body's natural frequency (n1=n2n_1 = n_2), resulting in maximum amplitude and sound intensity.
  • Undamped Vibrations: Occur when frictional forces are zero, maintaining a constant amplitude (aa) with no energy dissipation.
  • Damped Vibrations: Occur in the presence of friction, causing continuous dissipation of energy and decreasing amplitude over time.

Plane Progressive Waves

  • Definition: A wave continuously propagating forward through periodic particle vibrations, transferring energy across space.
  • Properties:
    • All particles vibrate with equal amplitude (aa) and period (TT).
    • All particles pass equilibrium positions successively at maximum speed (aρa\rho or a2πTa\frac{2\text{π}}{T}).
    • No particles remain permanently at rest or cross equilibrium simultaneously.
  • General Equation:
    • y=asin⁡((ωt±kx)+ϕ0)y = a \sin((\omega t \pm kx) + \phi_0)
    • Negative sign between tt and xx indicates wave propagation along the positive x-axis; positive sign indicates propagation along the negative x-axis.
    • Wave Number / Propagation Constant: k=2πλk = \frac{2\pi}{\lambda}
    • Angular Frequency: ω=2πf=2πT\omega = 2\pi f = \frac{2\pi}{T}
    • Phase Velocity: v=ωkv = \frac{\omega}{k}
  • Particle Velocity (vparticlev_{\text{particle}}) & Wave Slope:
    • vparticle=dydt=ωacos⁡(ωt−kx)=ωa2−y2v_{\text{particle}} = \frac{dy}{dt} = \omega a \cos(\omega t - kx) = \omega \sqrt{a^2 - y^2}
    • Maximum velocity occurs at mean position (y=0y = 0): vmax=ωav_{\text{max}} = \omega a
    • Minimum velocity occurs at extreme position (y=ay = a): vmin=0v_{\text{min}} = 0
    • Relation to wave slope: vparticle=−Wave velocity×Slope of the wavev_{\text{particle}} = -\text{Wave velocity} \times \text{Slope of the wave}

Velocity of Transverse and Longitudinal Waves

  • Transverse Waves on a String:
    • Velocity: v=Tmv = \sqrt{\frac{T}{m}}, where TT is tension and m=ρAm = \rho A is mass per unit length.
    • In solid media (e.g., S-seismic waves): v=√ηρv = √{\frac{\eta}{\rho}}, where η\eta is the modulus of rigidity.
    • For a heavy string of length LL suspended vertically under gravity:
    • Speed at bottom free end A: VA=0V_A = 0
    • Speed at distance xx from free end (point B): VB=x gV_B = \sqrt{x \, g}
    • Speed at top support C: VC=L gV_C = \sqrt{L \, g}
    • Speed at B relative to C: VB w.r.t C=(L−x)gV_{B \text{ w.r.t } C} = \sqrt{(L - x) g}
    • Time taken by wave from A to B: TAB=xgT_{AB} = \sqrt{\frac{x}{g}}
  • Longitudinal Sound Waves:
    • General relation: v=Eρv = \sqrt{\frac{E}{\rho}}, where EE is elastic modulus and ρ\rho is density.
    • Elasticity order: Es>El>Eg  ⟹  vsolid>vliquid>vgasE_s > E_l > E_g \implies v_{\text{solid}} > v_{\text{liquid}} > v_{\text{gas}}.
    • Sound velocity in solid rods: vs=Yρv_s = \sqrt{\frac{Y}{\rho}} (YY = Young's modulus).
    • Sound velocity in unbounded solids: v=B+43ηρv = \sqrt{\frac{B + \frac{4}{3}\eta}{\rho}} (BB = Bulk modulus).
    • Sound velocity in liquid or gas: v=Bρv = \sqrt{\frac{B}{\rho}}.
  • Newton's Formula & Laplace Correction:
    • Newton assumed isothermal propagation (Biso=PB_{\text{iso}} = P): v=Pρ=280 m/sv = \sqrt{\frac{P}{\rho}} = 280\,\text{m/s} at NTP (lower than experimental 332 m/s332\,\text{m/s}).
    • Laplace correction assumed adiabatic propagation (Badia=γPB_{\text{adia}} = \gamma P): v=γPρ=γRTM=331.3 m/sv = \sqrt{\frac{\gamma P}{\rho}} = \sqrt{\frac{\gamma R T}{M}} = 331.3\,\text{m/s} at NTP, where γ=CpCv=1.4\gamma = \frac{C_p}{C_v} = 1.4.

Factors Affecting Velocity of Sound

  • Density: Inverse relation to square root of gas density (v∝1ρv \propto \frac{1}{\sqrt{\rho}}).
  • Temperature: Direct relation to square root of absolute temperature (v∝Tv \propto \sqrt{T}).
    • For small temperature changes near 0 ∘C0\,^\circ\text{C}: v′=v0+0.61×t (m/s)v' = v_0 + 0.61 \times t\,(\text{m/s}).
  • Pressure: Sound velocity is independent of pressure changes at constant temperature.
  • Humidity: Sound travels faster in moist air than in dry air because moist air is less dense than dry air at equal temperatures.
  • Wind: v=vs+vwcos⁡(θ)v = v_s + v_w \cos(\theta).
    • In direction of wind: v=vs+vwv = v_s + v_w
    • Opposite to wind: v=vs−vwv = v_s - v_w
  • Invariance: Amplitude, frequency, phase, loudness, pitch, quality, and wave shape do not affect sound velocity.

Reverberation and Sound in Gas Mixtures

  • Reverberation: Persistent repetition of sound due to multiple reflections in an enclosed space.
  • Sabines Formula: Reverberation time T=KVAS=0.18V∑SAT = \frac{K V}{A S} = \frac{0.18 V}{\sum S A}, where VV is volume, AA is absorption coefficient, SS is area, and K=0.18K = 0.18.
  • Refraction of Sound: Follows Snell's law: sin⁡(i)sin⁡(r)=1μ2=μ2μ1=v2v1\frac{\sin(i)}{\sin(r)} = {1}\mu_2 = \frac{\mu_2}{\mu_1} = \frac{v_2}{v_1}.
  • Gas Mixture Properties:
    • Velocity in mixture: vmix=γmixPρmix=γmixRTMmixv_{\text{mix}} = \sqrt{\frac{\gamma_{\text{mix}} P}{\rho_{\text{mix}}}} = \sqrt{\frac{\gamma_{\text{mix}} R T}{M_{\text{mix}}}}
    • Density of mixture: ρmix=ρ1V1+ρ2V2V1+V2\rho_{\text{mix}} = \frac{\rho_1 V_1 + \rho_2 V_2}{V_1 + V_2}
    • Specific heats: (Cv)mix=n1Cv1+n2Cv2n1+n2(C_v)_{\text{mix}} = \frac{n_1 C_{v1} + n_2 C_{v2}}{n_1 + n_2}, (Cp)mix=(Cv)mix+R(C_p)_{\text{mix}} = (C_v)_{\text{mix}} + R
    • Adiabatic index: n1+n2γmix−1=n1γ1−1+n2γ2−1\frac{n_1 + n_2}{\gamma_{\text{mix}} - 1} = \frac{n_1}{\gamma_1 - 1} + \frac{n_2}{\gamma_2 - 1}
    • Molecular weight: Mmix=M1n1+M2n2n1+n2M_{\text{mix}} = \frac{M_1 n_1 + M_2 n_2}{n_1 + n_2}

Displacement, Pressure Waves, and Wave Energy

  • Displacement Wave Equation: y=asin⁡(ωt−kx)y = a \sin(\omega t - kx)
  • Pressure Wave Equation: P=−Bdydx=aBkcos⁡(ωt−kx)=P0cos⁡(ωt−kx)P = -B \frac{dy}{dx} = a B k \cos(\omega t - kx) = P_0 \cos(\omega t - kx)
    • Pressure Amplitude: P0=aBkP_0 = a B k
    • Phase relationship: Pressure is maximum where displacement is minimum, and pressure is minimum where displacement is maximum.
  • Energy Transport: Total energy transported equals maximum kinetic energy:
    • dE=12(dM)×(vmax)2=12μ dx×(aω)2dE = \frac{1}{2} (d M) \times (v_{\text{max}})^2 = \frac{1}{2} \mu \, dx \times (a \omega)^2