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Old   January 15, 2009, 00:45
Default hi heydlauff sir
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NAVEEN.K.M
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hi heydlauff sir

i am new to openfoam 1.4.1....could u please send me the procedure of solving naca 0012 airfoil and how to mention the different angle of attack...
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Old   January 15, 2009, 06:02
Default hi heydlauff sir
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hi heydlauff sir

i am new to openfoam 1.4.1....could u please send me the procedure of solving naca 0012 airfoil and how to mention the different angle of attack...
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Old   January 19, 2009, 01:21
Default hi heydlauff sir can
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hi heydlauff sir


can u tell me how to install liftDragtool in openfoam 1.4.1...
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Old   February 2, 2009, 05:44
Default hi everybody can any one
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hi everybody


can any one tell me how and where to install liftDragtool in openfoam 1.4.1...
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Old   February 2, 2009, 07:44
Default hey naveen, use openfoam 1.
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hey naveen,

use openfoam 1.5 with its force-tool!!

the different angle of attack you will have to set in die /0/U file in oyur casefolder. there is the vector for "inlet" velocity (0 0 0). just change the x and y component to the wished value (must calculate from SIN or COS).

e.g. (1 1 0) for angle of 45deg and speed of sqrt(2) (=1.41 m/s).
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Old   September 2, 2009, 17:56
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Hi Emanuele,
Are you defining the airfoil surfaces as a single patch, and if so, how are you doing that? I'm having problems simulating flow at 5 degrees aoa. When I try to visualize the streams, there are very few streams visible and the Cl and Cd values don't make sense. What mesh generator are you using?
Would it be possible to post your case files so I can gain more insight into the solvers and variables you're setting?
Thanks.
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