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Which risk increases in a gas turbine combustor due to fuel-air mixture variations?

A)Increased nitrogen oxides ($NO_x$) emissions
B)Decreased turbine blade creep rate
C)Reduced turbine disk thermal stressing
D)Amplified surge margin robustness

💡 Explanation

Increased nitrogen oxide emissions occur because the *Zeldovich mechanism* is highly temperature-sensitive. Therefore, regions of stoichiometric combustion produce excessive $NO_x$, rather than forming mostly $N_2$ and $O_2$, because of localized temperature spikes in the diffusion flame.

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