|September 19, 2013, 10:55||
Papers for validation
Join Date: Aug 2013
Posts: 37Rep Power: 4
I am working on airfoil analysis,and finding the Cl,Cd values for S-series blade profile.Can anybody please suggest me some published work of results for blade S818 , S825 , S826 , S831 at low velocity (4,6,8,10,12, 15 m/s) at various angle of attack.
I am stuck with it for a month.
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