Question: Show that, if Eqs. (7.70) and (7.71) are valid, the maximum lift-to-drag ratio occurs when CD = 2CD. What are (L/D) max and for a

Show that, if Eqs. (7.70) and (7.71) are valid, the maximum lift-to-drag ratio occurs when CD = 2CD∞. What are (L/D) max and α for a symmetric wing when AR = 5.0 and CD∞ = 0.009?

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