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← TechnologyWhich 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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