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February 27, 2011, 10:54 |
Biconvex Airfoil in incompressible flow
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#1 |
New Member
Join Date: Jan 2011
Posts: 6
Rep Power: 15 |
Hi all,
having this biconvex (quadrilateral) airfoil Leading Edge: A(0,0) Trailing Edge B(1,0) C(.7,.03) D(.45,-.05)
I'm quite new to CFD so any help is really appreciated. Thanks a lot. |
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February 27, 2011, 14:41 |
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#3 | |
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Quote:
Ciao truffaldino, innanzi tutto ti ringrazio della risposta, comunque mi interessa veramente la base, cioč vedere come le linee di corrente vanno sul profilo al variare della freccia e dell'angolo d'attacco. I'm interested mainly to see how streamlines are directed varying the camber and/or the angle of attack. Only secondarily I'd like to calculate polars at M=0. |
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February 27, 2011, 15:34 |
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#4 |
Senior Member
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Ciao Courant,
I have a very simple code in "scilab" that uses 2D hess-smith panel method to calculate incompressible potential flow and streamlines past airfoils. It is extremely easy to use. Scilab is a free analog of mathlab that can be downloaded from the web. Ti posso inviare il programma, se vuoi. Truffaldino |
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February 27, 2011, 15:52 |
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#5 | |
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Quote:
Thanks. |
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