|November 24, 2011, 02:31||
naca 23015 mm reference values
Join Date: Nov 2011
Posts: 8Rep Power: 7
I have my NACA 23015 airfoil(flow speed 36m/s) which has a chord length of 100mm, max thickness 15.05mm,...
after scaling the grid to metres...what should be the reference values for area, length and depth...
i am unable to obtain correct values for Cl and Cd and am quite inexperienced in using fluent...please help me
its very urgent....
viscous model is spalart allmaras
boundary conditions are pressure farfield for the whole
i later intend to convert the 23015 to a kline fogleman type 2 backward facing step airfoil as a part of my project. Any suggestions?
|kline fogleman, reference values|
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