Which risk escalates under icing conditions during aerial turbine engine operation?

💡 Explanation

Compressor stall risk increases because ice accretion disrupts airflow over the compressor blades thus leading to flow separation and pressure fluctuations, initiating compressor stall rather than sustained combustion, and if uncorrected leads to complete engine surge.

• Which kinematic consequence appears from resolver signal quantization?
• Which outcome occurs when lubricating oil viscosity is too low during a CNC grinder operation?
• Which control outcome occurs when a turboprop aircraft flies in icing conditions without activated de-icing systems?
• Which outcome occurs when excessive dither in a servo valve controlling a hydraulic actuator generates frequency close to the natural resonance?
• Which limitation commonly arises when exceeding a turbocharger's surge line?
• Which reliability issue appears first due to transformer excitation asymmetry from unbalanced capacitor bank switching?