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Drag Coefficient -- What is the constant K?
As I understand, the drag coefficient looks as follows: CD=CD0+CL/πAe however, the professor threw in a new constant, K, and I am having trouble understanding what this means. The formula now looks like this: CD=CD0+k1CL+k2CL^2 could someone help? Thanks!- eliasss
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- Aerodynamics Coefficient Formula
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- Forum: Aerospace Engineering