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Old 01-05-2003, 10:40 PM
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Bruce Thompson
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Default Reynald's number
Since you all seem to be WAY over my head let me ask a question and see what comes of it. I am trying to design a wing for a racecar. from what I read above the RE# are approx 1.4mill to 2.4 mill. How do I choose an airfoil that will have a high Cl and low Cd?
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