This item is available under a Creative Commons License for non-commercial use only
The three-dimensional, compressible, viscous flow field around a general propeller geometry with the inflow at zero angles of incidence and yaw is computed using a Reynolds-Averaged Navier-Stokes equations solver. Results from validation test cases in which the laminar and turbulent incompressible flow over a flat plate are calculated demonstrate the flow solver is capable of accurately capturing boundary-layer behaviour. Euler solutions from flow field calculations around two very different propeller geometries show a high level of accuracy and efficiency. Preliminary results from a viscous flow field calculation around a two-bladed propeller are very encouraging.
Boyle, F.: Solution Of The Navier-Stokes Equations For Transonic Propeller Flows. 21st American Institute of Aeronautics and Astronautics Applied Aerodynamics Conference, AIAA Paper No. 2003-4083. Orlando, Florida, USA, 2009.