Math 2.0

Fluid mechanics Definition

Ffowcs Williams–Hawkings equation

Builds on Lighthill's acoustic analogyAcoustic wave equationHeaviside step functionDirac delta function

Definition

Consider a compressible fluid in ℝ3\R^3 with density ρ\rho, velocity uu, pressure pp and viscous stress tensor τij\tau_{ij}. Let ρ0\rho_0, p0p_0, c0c_0 be the constant density, pressure and speed of sound of the fluid at rest. Let a closed surface move in the fluid, given as the zero set of a smooth function f(x,t)f(x, t). Assume f>0f > 0 outside the surface and ∣∇f∣=1\abs{\nabla f} = 1 on it. Let n=∇fn = \nabla f be the outward unit normal, vnv_n the normal velocity of the surface and un=u⋅nu_n = u \cdot n the normal velocity of the fluid. Let HH be the Heaviside function and δ\delta the Dirac delta. Set ρ′=ρ−ρ0\rho' = \rho - \rho_0, Pij=(p−p0)δij−τijP_{ij} = (p - p_0) \delta_{ij} - \tau_{ij}, and let TijT_{ij} be the Lighthill stress tensor of Lighthill's acoustic analogy. The Ffowcs Williams–Hawkings equation is the equation, in the sense of distributions, (1c02∂2∂t2−Δ)(c02ρ′H(f))=∂∂t[Q δ(f)]−∂∂xi[Li δ(f)]+∂2∂xi∂xj[TijH(f)],\left( \frac{1}{c_0^2} \frac{\partial^2}{\partial t^2} - \Delta \right) \big( c_0^2 \rho' H(f) \big) = \frac{\partial}{\partial t} \big[ Q \, \delta(f) \big] - \frac{\partial}{\partial x_i} \big[ L_i \, \delta(f) \big] + \frac{\partial^2}{\partial x_i \partial x_j} \big[ T_{ij} H(f) \big], where Q=ρ0vn+ρ(un−vn)Q = \rho_0 v_n + \rho (u_n - v_n) and Li=Pijnj+ρui(un−vn)L_i = P_{ij} n_j + \rho u_i (u_n - v_n), with summation over repeated indices.

Remarks

The equation follows from the mass and momentum equations of the fluid outside the surface, written for the generalised functions ρ′H(f)\rho' H(f) and ρuiH(f)\rho u_i H(f). The surface terms come from the derivatives of H(f)H(f). The three terms on the right are the thickness (monopole), loading (dipole) and quadrupole sources. Outside the source region c02ρ′c_0^2 \rho' equals the acoustic pressure p′p'.

Example: for a solid surface the fluid does not cross the boundary, so un=vnu_n = v_n. The sources then reduce to Q=ρ0vnQ = \rho_0 v_n and Li=PijnjL_i = P_{ij} n_j, the force per unit area that the surface exerts on the fluid.

Special case: when no surface is present, so that H(f)=1H(f) = 1 everywhere, the surface terms vanish and the equation reduces to Lighthill's equation.

Reading path

To understand this page from the ground up, read these 10 pages in order. The foundations come first.

Show the path as a graph
Each page uses the pages above it. The colour of the bar on a box shows how strong the evidence is, and the box also gives it as text. The list has the same pages.
  • no evidence level
  1. Acoustic wave equation concept
  2. Compressible flow concept
  3. Function concept
  4. Navier–Stokes equations concept
  5. Speed of sound concept
  6. Laplace transform definition
  7. Lighthill's acoustic analogy statement
  8. Heaviside step function object
  9. Dirac delta function object
  10. Ffowcs Williams–Hawkings equation definition

Further reading

  1. Web https://en.wikipedia.org/wiki/Aeroacoustics
About this page
TagFDP9G4BCMF
URIm2://FDP9G4BCMF
Kinddefinition
WritingW0 stub
MSC76Q05
DefinesFfowcs Williams–Hawkings equation
UsesLighthill's acoustic analogy, Acoustic wave equation, Heaviside step function, Dirac delta function
Changed3 November 2026

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