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Which efficiency decrease occurs with turbine blade scaling?

A)Decreased cooling surface area
B)Increased boundary layer thickness
C)Reduced stator blade curvature
D)Elevated rotor disc temperatures

💡 Explanation

As turbine blades increase drastically in scale, the relative boundary layer thickness increases due to skin friction effects; therefore, momentum transfer gets disrupted more significantly, adding extra losses, rather than other geometric effects becoming dominant.

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