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Determine the weight of an aircraft in level flight if the lift coefficient is 0.5, the dynamic pressure 10439 Pa, and the wing has a
Determine the weight of an aircraft in level flight if the lift coefficient is 0.5, the dynamic pressure 10439 Pa, and the wing has a span of 12 m and average chord of 2 m. Submit your answer in kilo-newtons, kN
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