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August 27, 2018, 14:22 |
Higher order 3D Panel Method - Wing
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#1 |
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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Tags |
3d wing, cfd aerospace, panel methods |
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