Question:
Which of the following process ideally represents combustion in gas turbine engines?
Which of the following process ideally represents combustion in gas turbine engines?
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Brayton cycle assumes isobaric heat addition and rejection.
Updated On: June 02, 2025
- Adiabatic
- Isentropic
- Isobaric
- Isochoric
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The Correct Option is C
Solution and Explanation
In ideal Brayton cycle (gas turbine cycle), combustion is assumed to occur at constant pressure.
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