FW-H Steady Model Reference

The Ffowcs Williams-Hawkings Steady model is based on the convergent steady-state RANS approach for aerodynamic computation of propeller blade loads for a single or multiple rotating reference frames with the FW-H Acoustic Analogy Model. It is for three-dimensional simulations with impermeable FW-H surfaces. It cannot be used for non-rotating cases.

Theory See Ffowcs Williams-Hawkins Model.
Provided By [physics continuum] > Models > Aeroacoustics Models
Example Node Path Continua > Physics 1 > Models > Ffowcs Williams-Hawkings Steady
Requires
  • Material: one of Gas, Liquid, Eulerian Multiphase, Multi-Component Gas, Multi-Component Liquid
  • (For Eulerian Multiphase, Multi-Component Gas or Multi-Component Liquid, further models are required to expose the Flow models.)
  • Flow: Coupled Flow or Segregated Flow
  • Time Models: Steady
  • Optional Models: Aeroacoustics
  • Viscous Regime: Turbulent or Laminar
Activates Solvers FW-H Steady Solver

See FW-H Steady Solver Properties.

FW-H Steady Solver Properties

The solver provides an approximation of the results that you can expect from a steady state simulation. On computation of the thickness and loading noise, the term corresponding to the time derivative of the surface pressure is set to zero.

This solver implements the advanced time approach, to account for the time delay between the emission time and reception time. The FW-H Steady model is able to compute noise from propellers in the subsonic as well as transonic and low supersonic domain at low numerical cost. It is suited for propeller optimization because it is inexpensive and reliable, though it is an approximate method.

Number of Time Steps per Revolution
Number of time-steps per revolution of the rotating reference frame. The defaults is 360.
Number of Revolutions
Number of revolutions of the rotating frame of reference. The default is 10.
Right-Click Actions
Execute Solver

Runs the FW-H Steady Solver.