The flow solver will then be run to calculate the flow over the aerofoil.įirstly you need to create a text file with your coordinates in it. In this note you will be shown how to read these coordinates into SolidWorks and how to create a straight 3D shape from them. The coordinates for this should be available from the same place that you found this tutorial, they consist of x,y and z coordinates in a simple text file. ![]() NACA was the predecessor to NASA and the four digits of the aerofoil name are a code for a series of equations that completely define the shape. The example consists of a NACA 5012 aerofoil. For those of you looking at this for the L4 Fluid Mechanics assignment please note the NACA 5012 is NOT the aerofoil used in the experiment! ![]() SolidWorks is the 3D CAD package used by the School and this note assumes you are familiar with basic usage. This note explains how to draw an aerofoil in three dimensions in SolidWorks and then how to run a simple calculation of the flow over the geometry. Using SolidWorks Flow Simulation to Calculate the Flow Around a NACA5012 Aerofoil Introduction
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