|September 19, 2013, 10:55||
Papers for validation
Join Date: Aug 2013
Posts: 36Rep 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.
|Thread||Thread Starter||Forum||Replies||Last Post|
|ASME CFD Symposium - Call for Papers||Chris Kleijn||Main CFD Forum||0||September 25, 2001 10:17|
|ASME CFD Symposium, Atlanta, 22-26 July 2001||Chris R. Kleijn||Main CFD Forum||0||August 1, 2000 10:07|
|CFD Symposium (Call for Papers)||Chris R. Kleijn||Main CFD Forum||0||October 5, 1998 10:25|
|ASME CFD Symposium - Call for Papers||Chris R. Kleijn||Main CFD Forum||0||September 8, 1998 08:19|
|ASME CFD Symposium - Call for Papers||Chris R. Kleijn||Main CFD Forum||0||September 3, 1998 08:45|