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Which efficiency loss occurs when a turbine utilizes a Carnot cycle’s heat exchanger at supersonic flow?

A)Irreversible aerodynamic shock heating
B)Reduced blade boundary layer adhesion
C)Increased vibrational resonant frequency
D)Catalytic surface decarbonization increases

💡 Explanation

Irreversible aerodynamic shock heating degrades the efficiency, because energy is dissipated by viscous effects via increased entropy during shock wave formation, thereby lowering available energy by exergy destruction, rather than efficient work extraction.

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