Which risk increases when aircraft experience icing conditions?

💡 Explanation

Ice accretion changes the airfoil shape; this causes flow separation because adverse pressure gradient exceeds the boundary layer's ability to remain attached therefore severely degrading lift and control effectiveness on control surfaces rather than improving other irrelevant systems.

• Which consequence results when uncontrolled sublimation of solid CO₂ occurs?
• Which behavior changes occurs in two cascaded Carnot heat engines when the intermediate temperature increases?
• Which risk increases near flash memory cells when write voltages scale down?
• Which consequence results when a refrigeration cycle uses non-isentropic compressors?
• Which risk increases when exhaust gas recirculation (EGR) significantly slows reaction rate?
• Which outcome occurs when applying reverse bias excessively to Zener diodes?