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Old 01-02-2003 | 04:03 PM
  #6  
ksechler
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From: Frederick, MD
Default Airfoil selection

Just a little more information I dug up....

RE can be calculated using the following:
68459*V*c
my Re is 2,200,000 ...

I went to:
http://www.nasg.com

and used to following:
http://www.nasg.com/afdb/show-polar-e.phtml?id=869