Thermodynamic Analysis of the Second Fluid Brayton Cycle for Scramjet Engine

Thermodynamic Analysis of the Second Fluid Brayton Cycle for Scramjet Engine

The burning chamber wall of the ramjet engine is facing an extremely thermal environment during normal conditions. Thermal protection measures must be taken on the wall surface of the combustion chamber. At the same time, the aircraft faces high-power electrical demand problems under high-speed crui...

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Bibliographic Details
Main Authors: Jiamao Luo, Xin Qi, Si Jiao, Yunlei Xiao, Shengfang Huang, Shunhua Yang
Format: Article
Language:English
Published: MDPI AG 2024-11-01
Series:Energies
Subjects:
scramjet engine
Brayton cycle
helium
thermal cycle
thermal protection
thermoelectric conversion
Online Access:https://www.mdpi.com/1996-1073/17/23/6003

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https://www.mdpi.com/1996-1073/17/23/6003

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