|August 7, 2010, 03:01||
NACA 65 series(cambered Airfoil) design using blade modlerer.
Join Date: Nov 2009
Posts: 24Rep Power: 9
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.
18 hours ago
|November 14, 2012, 10:25||
Join Date: Jan 2011
Posts: 1Rep 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
|ansys, bladedesign, bladgen|
|Thread||Thread Starter||Forum||Replies||Last Post|
|Symmetric NACA Airfoil Lift and Drag Data||jrider22||Main CFD Forum||3||April 15, 2010 04:59|
|Basic Blade Design Code||apoorv||Main CFD Forum||0||April 5, 2010 06:37|
|I need help with an unusual airfoil design!!||mugsy||OpenFOAM||0||September 22, 2009 18:15|
|Drag prediction for Naca 23012 airfoil||Ravel Bogatec||CFX||17||February 15, 2008 01:21|
|Info: Short Course On Thermal Design of Electronic Equipment||Arnold Free||Main CFD Forum||0||August 10, 1999 10:18|