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December 24, 2005, 06:17
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range of lift to drag ratio in airfiols
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Guest
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i can nyone plz giv me d range of Cl/Cd..its urgent..
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December 24, 2005, 11:44
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Re: range of lift to drag ratio in airfiols
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#2 |
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Guest
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i want to know the range of lift to drag ratio in airfiols
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December 25, 2005, 09:51
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Re: range of lift to drag ratio in airfiols
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Please be more specific..for which airfoil do you want it?
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December 26, 2005, 02:47
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Re: range of lift to drag ratio in airfiols
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Guest
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From zero (obvious) to 150..200 for "normal" airfoils. I guess it can be even higher for supercirculation and multielement.
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