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[Other] NACA 65 series(cambered Airfoil) design using blade modlerer. |
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August 7, 2010, 04:01
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NACA 65 series(cambered Airfoil) design using blade modlerer.
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#1 |
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New Member
Pradeep
Join Date: Nov 2009
Location: Duisburg
Posts: 24
Rep Power: 17  |
Hello..
Can anyone give me some info. regarding the above mentioned topic. I tried using ANSYS Blademodeler. But I could only create NACA 65 Standard blade with zero lift. Is there any method to provide camber in ANSYS Blade modeler.?? Like by providing lift coefficient.. or is it possible to import NACA coordinates (in form of .txt or .dat file) into blademodler?? Awaiting for your response. Regards, Pradeep 18 hours ago |
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November 14, 2012, 10:25
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#2 |
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New Member
yasaman
Join Date: Jan 2011
Posts: 1
Rep Power: 0 |
hello, I want to know how to draw a 2d blade(airfoil) NACA65 in MATLAB at blade mid height . with CL0=0.9. in fact I wanna know how to use NACA65 table? what is the y/c coefficient and t/c coefficient? thanx for your quick help
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| Tags |
| ansys, bladedesign, bladgen |
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