The overall mixture in a gas turbine combustor is near stoichiometric. True or false?
Answer: C
Correct answer: False, it is roughly four times leaner
The overall air-fuel ratio is about 60 to 1 by mass, against a stoichiometric ratio near 15 to 1, so the chamber as a whole is about four times leaner than a flame will sustain. The whole architecture of zones exists to resolve this: a fifth of the air makes the primary zone near stoichiometric, and the rest is added downstream.
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