Question: - Consider a General Dynamics F - 1 6 Fighter plane with a Weight of 1 9 0 0 0 kg , wing surface of

-Consider a General Dynamics F-16 Fighter plane with a Weight of 19000 kg, wing surface of 28 m^2, wing span of 9.96 m, in a steady flight at 10000 m and flying with your highest velocity value and effective drag force is your highest drag value. Calculate the Oswald efficiency factor and zero-lift drag coefficent.

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