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QUESTION
. An aircraft has a mass of 7200 kg and a wing span of 12 m. If the wing loading is 1.968 kN/m2 , what is the induced drag when flying at speeds of
. An aircraft has a mass of 7200 kg and a wing span of 12 m. If the wing loading is 1.968 kN/m2 , what is the induced drag when flying at speeds of 200 knots and 300 knots at sea-level? (Assume δ = 0).
