The question is often asked: Can an airfoil fly upside-down? To answer this, make the following calculation.

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The question is often asked: Can an airfoil fly upside-down? To answer this, make the following calculation. Consider a positively cambered airfoil with a zero-lift angle of −3°. The lift slope is 0.1 per degree. 

(a) Calculate the lift coefficient at an angle of attack of 5°. 

(b) Now imagine the same airfoil turned upside-down, but at the same 5° angle of attack as part 

(ii). Calculate its lift coefficient. 

(c) At what angle of attack must the upside-down airfoil be set to generate the same lift as that when it is right-side-up at a 5° angle of attack?

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