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#1 |
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Guest
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Hi
I have a problem when trying to get Coeffecient of lift for an external flow around a circular cylinder at Re = 10e4, because Cl doesn't occilate around the zero line. I changed the domain and the grid too but in vain. Any Ideas as a solution before using 3D will be great. Thanks alot. Yours, Rola |
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#2 |
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What is your flow Mach number? is the operating pressure set correctly - including its location?
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#3 |
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Guest
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hi
Thanks Mark, I don't use pressure, I just use the velocity components and every thing was alright till Re = 10e4 the problem exists, any idea Thanx, Rola |
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