The stoichiometric fuel-to-air ratio in an aircraft engine combustor varies with the compressor pressure ratio as follows:
(A) increases linearly
(B) decreases linearly
(C) is independent
(D) increases nonlinearly
The stoichiometric fuel-to-air ratio in an aircraft engine combustor varies with the compressor pressure ratio as follows:
(A) increases linearly
(B) decreases linearly
(C) is independent
(D) increases nonlinearly