Which outcome sharply increases drag when ice accretion compromises wing geometry and flight envelope expands?

💡 Explanation

A turbulent boundary layer transition occurs because ice disrupts laminar flow, increasing pressure drag and flow separation; therefore stall speed rises sharply, rather than decreasing or generating premature landing gear deployment, which is a separate system.

• Overflight stall speed increases when ice accumulates; which mechanism decreases lift?
• Which outcome results when three-phase systems experience underdamped oscillations?
• Which consequence results when receiver Automatic Gain Control (AGC) misinterprets noise as a low-level signal?
• Which risk increases when seawater permeates concrete rebar supports?
• Which risk increases when cavitation stalls an evaporator feed pump in a large-scale ammonia refrigeration system?
• Which failure consequence arises when reverse recovery current exceeds a clamping diode junction's capacity?