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Combustion in gas turbine engines is ideally represented as the following process:
(A) Adiabatic
(B) Isentropic
(C) Isobaric
(D) Isochoric


Question ID - 155643 | SaraNextGen Top Answer

Combustion in gas turbine engines is ideally represented as the following process:
(A) Adiabatic
(B) Isentropic
(C) Isobaric
(D) Isochoric

1 Answer
127 votes
Answer Key / Explanation : (C) -

(C) Isobaric

127 votes

127
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