Which consequence results when incompressible flow assumptions fail within the Bernoulli equation during aircraft icing?

💡 Explanation

Icing changes airflow density; the Bernoulli equation relies on constant density. Pitot tubes measure dynamic pressure using this equation; ice disrupts this measurement. Therefore, airspeed errors increase, rather than combustion instability, because flow density approximation deteriorates.

• Which polarization shift results when a laser beam reflects off a dielectric surface near Brewster's angle?
• Which risk increases when molten salt reactor fuel cools?
• Which effect occurs when exceeding the design-limit temperature of a gas turbine?
• Which outcome occurs when a pump laser's coherence diminishes within an interferometer?
• Which outcome results when irreversibilities increase during transcritical Rankine cycle operation?
• Which outcome results when high stress deforms a metallic lattice?