Potential flow past an airfoil

So I'm trying to visualise potential flow over an airfoil at different AOA. I want to be able to see streamlines, velocity vectors and potential contours. I've called in a dat file of the airofil onto MATLAB and defined rotation. I want a potential flow past it using solely the source panel method.

[Image Analyst]

OK, have fun. If you have any actual specific questions, then ask them and attach your data and code to read it in with the paperclip icon after you read this:

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Also say if it's your homework or not.

Answer 1

[Star Strider]

Check the File Exchange.

When I did and searched on ‘airfoil’, I found: Plot Pressure Distribution (Cp) Over an Airfoil / Aerofoil ; Vector Plot ; Arrow Plot

There may be others that more closely match what you want to do. You have to determine that.

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