Which risk increases when a morphing wing aircraft experiences icing?

💡 Explanation

Icing causes a rougher wing surface, disrupting airflow; therefore flow separation occurs earlier lowering stall angle because it disrupts the boundary layer adhesion, causing decreased lift, rather than stable airflow or altered frame properties.

• Which damaging outcome occurs when localized pressure drops below vapor pressure in high speed hydraulic pumps?
• Which risk increases when insufficient magnetizing impedance exists in a large power transformer causing sympathetic breaker tripping?
• Which actuator response occurs when the hydraulic servo-valve's dither amplitude decreases to zero?
• Which risk increases when investment casting employs insufficient vacuum degassing?
• Which consequence results when excessive vibration induces fatigue cracking in steel I-beams supporting a bridge?
• Which outcome occurs when anisotropic sensitivity arises in anisotropic magnetoresistive (AMR) sensors?