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#1 |
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Guest
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I am running a turbulent incompressible flow on an airfoil. for angle of attack of 10 or more degrees Spalart almaras model gives negative drag. should I modify turbulent parameters? or any idea???
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#2 |
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Are yours force vectors defined right?
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#3 |
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yes...
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#4 |
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I have been modelling airfoils for a while for my final year project, it is defiantly your force vectors-sorry.
Andy |
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