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Need Formulas for Calculating Aero Forces
Source:Internet Author:Unknow Pubdate:2008-04-03  
traindriver (Automotive) 19 Nov 03 22:06
Can anyone provide the basic calculations for converting Cd and Cl in real force numbers. I have volumns of tunnel data in coefficient form and I need to convert it to force numbers so the end user can understand it.
Thanks

aerobab (Aerospace) 20 Nov 03 10:30
Ummmm.....I'm presuming this is what you are looking for:

L = 0.5*(rho)*(V^2)*(Planform Area)*Cl

D = 0.5*(rho)*(V^2)*(Planform Area)*Cd

where L = Lift
        D = Drag
        rho = fluid (air?) density
        V = relative freestream velocity of working fluid

Cheers,


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