Which limit maximizes lift-to-drag coefficient when soaring avian wing loading exceeds its optimum?

💡 Explanation

When avian wing loading exceeds optimum, stall speed increases, reducing maneuverability because a higher angle of attack is required to maintain lift. Therefore, stall speed occurs, rather than increased parasitic drag, or hindered vortex shedding which occur due to different aerodynmaic mechanisms.

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