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New Member
Shibin Mohamed
Join Date: Nov 2011
Posts: 8
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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? |
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Tags |
kline fogleman, reference values |
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