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August 3, 2002, 20:40
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Lift Coefficient of an Airfoil.
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#1 |
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Guest
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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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August 5, 2002, 04:38
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Re: Lift Coefficient of an Airfoil.
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#2 |
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Guest
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Hi,
Try the command accoef. |
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September 5, 2002, 04:00
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Re: Lift Coefficient of an Airfoil.
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#3 |
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Guest
Posts: n/a
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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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