Problem

Determine the required wing area for a 1350-kg airplane to cruise at 125 km/h if the airfo...

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.

FIGURE 17.11 Airfoil performance curves.

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Solutions For Problems in Chapter 17

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