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Published on Mar 3, 2016
The CAD file for the F4U Corsair was obtained from GrabCAD. More information about Stallion 3D can be found at http://www.hanleyinnovations.com The analysis was performed in the following steps: 1. Import the aircraft STL file 2. Set the flow field conditions (angle = 2 deg, speed =150 m/s) 3. Setup the CFD. Number of cells about 800,000, RANS solver 4. Automatic grid generation 5. Grid generation & flow solution was about 4 hours to 3000 iterations on a 4 core laptop PC. 6. Perform aerodynamics analysis using Stallion 3D built-in tools. Thanks for watching. Please visit http://www.hanleyinnovations.com for more information.