PotentialFlow2DSim.m – generates 2D potential flow field from given combination of elementary flow such as uniform flow, source, sink, doublet, and vortex (requires CalculateVelocityFromSource2D.m, CalculateVelocityFromDoublet2D.m, and CalculateVelocityFromVortex2D.m). GenerateNACASeries6Airfoil.m – generates vertexes of the specified NACA series 6 airfoil’s surface and camber line.ĬalculateVelocityFromSource2D.m – calculates a velocity at a certain location that caused by a source at a certain location.ĬalculateVelocityFromSourcePanel2D.m – calculates a velocity at a certain location that caused by a uniformly distributed source panel at a certain location (requires CalculateVelocityFromSource2D.m).ĬalculateVelocityFromDoublet2D.m – calculates a velocity at a certain location that caused by a doublet at a certain location.ĬalculateVelocityFromVortex2D.m – calculates a velocity at a certain location that caused by a doublet at a certain location. GenerateNACASeries16Airfoil.m – generates vertexes of the specified NACA series 16 airfoil’s surface and camber line. GenerateNACASeries5Airfoil.m – generates vertexes of the specified NACA series 5 airfoil’s surface and camber line. GenerateNACASeries4Airfoil.m – generates vertexes of the specified NACA series 4 airfoil’s surface and camber line. GenerateNACACamberLine.m – generates vertexes of the specified NACA camber line. GenerateAirfoil.m – generates vertexes of an airfoil from the specified camber line and thickness distribution. GenerateCSpline.m – generates cubic Hermite curve from the specified control points and the tangent of each control point. GenerateBezierCurve.m – generates Bezier curve from the specified control points. To download the m-files, simply click the link on each m-file name and a pop-up window will appear, allowing you to download the m-files from my dropbox. All of these m-files are free and you may use or modify them as you like. This page contains my library of MATLAB function m-files for aerodynamics problem solver.
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