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. | ||
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Activates | Solvers | FW-H Steady Solver |
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.