Aerofoil Simulation Using Solidworks Flow Simulation
grabcad
My very first attempt at using Solidworks Flow Simulation. The airfoil specs have been collected from this site http://m-selig.ae.illinois.edu/ads/coord_database.html#T I have chosen this airfoil my experiment UA(2)-180 (smoothed) airfoil for ultralight category aircraft The condition used here are Pressure: 1 bar Temp: 25 degree Celsius Relative humidity: 25% Fluid: Air Velocity at X direction: 500m/s These are just some default conditions that were already set in the flow simulation wizard. I just tweaked some settings. Results obtained: 1) Mach number 2) Static Pressure Distribution cuz I only selected this two outputs.
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