Which outcome arises when an aircraft's angle-of-attack exceeds the critical limit, defying predictions from the ideal Bernoulli equation?

💡 Explanation

Boundary layer separation and stall occur because when exceeding the critical angle-of-attack, the adverse pressure gradient overwhelms airflow, leading to turbulence that disrupts lift; therefore creating stall rather than increased lift because the pressure gradients and airflow assumptions become invalid.

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