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Performance analysis of scCO2 closed Brayton cycle applied to aero engine thermal protection considering flow and heat transfer characteristics inside the scCO2-fuel heat exchanger
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DOI：10.1016/j.supflu.2025.106787.png)
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Abstract
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• This article focuses on the performance of scCO2 CBC cooling system for aero engine. • A calculation model considering scCO2 flow and heat transfer is constructed. • A relative performance coefficient is proposed to evaluate cycle performance. • An optimal scCO2 mass flow rate exists to make cycle net power maximum. • A critical fuel mass flow rate exists to make cycle performance roughly constant.
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