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Higher order 3D Panel Method - Wing

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August 27, 2018, 14:22	Higher order 3D Panel Method - Wing	#1
aradisa New Member Adrian Join Date: Feb 2012 Location: India Posts: 2 Rep Power: 0	I am coding a 3D higher order panel method in Matlab. My pressure coefficient values and the velocities are wrong, and I can't seem to figure out the error in the code. Please help

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3d wing, cfd aerospace, panel methods

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