Consider a jet aircraft with a weight of 44.5 kN, a wing area of 18 m,...

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Consider a jet aircraft with a weight of 44.5 kN, a wing area of 18 m², static thrust 8.9 kN at sea level, and a drag polar Cp = 0.02 +0.05C₁². Calculate: (a) the max angle of climb, and the climb rate under that condition (b) the max rate of climb, and the angle of climb under that flight condition Consider a jet aircraft with a weight of 44.5 kN, a wing area of 18 m², static thrust 8.9 kN at sea level, and a drag polar Cp = 0.02 +0.05C₁². Calculate: (a) the max angle of climb, and the climb rate under that condition (b) the max rate of climb, and the angle of climb under that flight condition

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