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← ScienceWhich efficiency decrease impacts turbofan engines at altitude?
A)Brayton cycle's temperature ratio limit✓
B)Compressor blade stall aerodynamics
C)Turbine material creep elongation
D)Nozzle erosion from particulate friction
💡 Explanation
A decrease in air density reduces inlet pressure, raising the isentropic temperature ratio, because the Brayton cycle relies on temperature differences for efficiency; therefore efficiency declines rather than mechanical failure increasing compression demands.
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