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Which effect increases around a high-bypass turbofan engine’s nacelle during flight?

A)Spacetime curvature
B)Boundary layer separation
C)Compressible flow choking
D)Acoustic resonance amplification

💡 Explanation

Spacetime curvature will increase in regions of higher energy density because mass-energy equivalence directly links them. Therefore, option A is the correct consequence, rather than options reflecting aerodynamic or structural effects under flight conditions.

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