Which risk increases when a commercial aircraft wing's boundary layer experiences premature transition to turbulence?

💡 Explanation

Total lift rapidly diminishes because the *adverse pressure gradient separation* worsens due to increased friction, therefore causing a stall rather than maintaining laminar flow; improved fuel consumption or decreased structural icing would not occur in this scenario.

• Which risk increases when excessive Optical Carrier (OC) signals are added to a SONET fiber optic network?
• Which consequence results when rapid turbine shaft deceleration occurs?
• Which consequence results when ice blockage occurs in an aircraft's bleed air system?
• Which calibration error occurs when robotic arm IMU experiences drift?
• Which consequence results when joint angle sensors fail in inverse kinematics calculation for a welding robot arm?
• Which risk increases when parasitic capacitance is not mitigated in high-frequency MOSFET circuits?