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Lift Coefficient of an Airfoil.

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Old   August 3, 2002, 19:40
Default Lift Coefficient of an Airfoil.
pandelis chatzis
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Hello Everyone

How it is possible to obtain the value of the Lift Coefficient for an airfoil ?

Many Thanks.
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Old   August 5, 2002, 03:38
Default Re: Lift Coefficient of an Airfoil.
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Try the command accoef.
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Old   September 5, 2002, 03:00
Default Re: Lift Coefficient of an Airfoil.
Sulaiman akhlaken
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try command ACOEFF,DRAG,U(STREAM VELOCITY),D(AIR DENSITY),A(FRONTAL AREA).. then u will get straight way..
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