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Old 01-02-2013, 05:13 PM   #7 (permalink)
ryannoe
Not Ordinary Engineering
 
Join Date: May 2011
Location: Alabama
Posts: 57
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Quote:
Originally Posted by kennybobby View Post
ratio should be 1.276/1.212= 1.053, 5.3% more drag.

if you fix the numbers in your post then i'll delete this one...
I goofed and didn't fix the middle equation numbers. I updated the first pressure value, did the calculations in excel and posted the results. The 1.276 and 1.212 values are old and should be deleted... which I'm doing now.

Once again.. thanks!
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