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| Need Help with 2D Panel Method Code |
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Posted Fri March 31, 2006 @10:45PM
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joshua_123_99 writes "Hi guys,
I just completed writing a code for calculating the surface pressure of a 4 digit 2D aerofoil section, using the panel method and the classic Hess and Smith approach, in the c language, however my results are not correct>
Can someone help me regarding this matter?
Thank you,
Joshua"
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