I was using a airfoil in a wind tunnel in school to find out drag and Co-efficient of drag.. anyway. Drag was given from the computer and i need to calculate the coefficient. I found that i need the surface area. I have the dimensions of the wing im using. They are 19.5cm x 10.3. So do i just multiply those, or do i also multiply by 2 to account for the top and bottom. Or is the surface area when calculating Cd just one side. thanks
2007-11-27
09:48:24
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2 answers
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asked by
joe
1
in
Science & Mathematics
➔ Engineering