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Search: Posts Made By: dicapriok
Forum: FLUENT January 15, 2011, 10:53
Replies: 1
Views: 3,152
Posted By dicapriok
Unhappy how to get cd,cl values of an airfoil correctly?

I have worked on these for about two weeks,but i just can't get these values correctly.If i plot these values vs AOA,some particular points(AOA=40-60 or even more)will not go smoothly,and had a rapid...
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