Problem

Calculate the total drag on an airfoil that has a chord length of 2 m and a span of 10 m....

Calculate the total drag on an airfoil that has a chord length of 2 m and a span of 10 m. The airfoil is at 3000 m flying at (a) 600 km/h and (b) 150 km/h. Use Fig. 17.11 for CD and a = 15°.

FIGURE 17.11 Airfoil performance curves.

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Solutions For Problems in Chapter 17

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