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Thread: ATR 42 Lift coefficient data
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Old 1st Jul 2010, 07:26
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runway2
 
Join Date: Oct 2009
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hi, i want to calculate the lift force and drag force during a typical landing for ATR 42 aircraft and canadair regional jet..
there for i need the CL and Cd values to calculate those forces for a flap setting (e.g.40). would u have any reasonable values to use for this?

thanks
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