Determine the required wing area

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Determine the required wing area for a 1350-kg airplane to cruise at 125 km/h if the airfoil is set at an angle of attack of 2.5°. The airfoil has the characteristics shown in Fig. 17.11. The cruise altitude is 5000 m in the standard atmosphere.

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Reference no: EM131174161

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Determine the required wing area : Determine the required wing area for a 1350-kg airplane to cruise at 125 km/h if the airfoil is set at an angle of attack of 2.5°. The airfoil has the characteristics shown in Fig. 17.11. The cruise altitude is 5000 m in the standard atmosphere.
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