Question: An F - 1 6 generating 3 0 , 0 0 0 lbs of lift has a dynamic pressure of 1 3 4 lb /

An F-16 generating 30,000 lbs of lift has a dynamic pressure of 134 lb/ft^2. The zero-lift drag coefficient for the F-16 is 0.019 and it has a k of 0.117. With a wing area of 300ft^2, what is the drag on this aircraft?

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