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Lift Coefficient of an Airfoil.

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August 3, 2002, 20:40	Lift Coefficient of an Airfoil.	#1
pandelis chatzis Guest Posts: n/a	Hello Everyone How it is possible to obtain the value of the Lift Coefficient for an airfoil ? Many Thanks.

August 5, 2002, 04:38	Re: Lift Coefficient of an Airfoil.	#2
HVN Guest Posts: n/a	Hi, Try the command accoef.

September 5, 2002, 04:00	Re: Lift Coefficient of an Airfoil.	#3
Sulaiman akhlaken Guest Posts: n/a	try command ACOEFF,DRAG,U(STREAM VELOCITY),D(AIR DENSITY),A(FRONTAL AREA).. then u will get straight way..

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