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Which risk increases when a morphing wing aircraft experiences icing?

A)Decreased stall angle of attack
B)Elevated engine combustion temperatures
C)Reduced magnetic field shielding
D)Increased structural frame elasticity

💡 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.

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