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March 26, 2016, 11:48 |
Wind tunnel results
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#1 |
New Member
karthikeyan
Join Date: Aug 2012
Location: India
Posts: 15
Rep Power: 14 |
In low Reynold airfoils experimental results are available in Vol 1-5 by selig. In these volumes experimental values are represented as polar plot in chapter 4 or 5 and plotted values in given in appendix E. In polar values given for Re 60,000, 100,000, 150,000. But in appendix values are not matching with former one. which could be taken as reference value?
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