Parametric optimization and exergy analysis of a high mach number aeroengine with an ammonia mass injection pre-compressor cooling cycle
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DOI: 10.1016/j.energy.2023.128906
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- Ma, Guangwei & Zhao, Guoyan & Sun, Mingbo & Xiong, Dapeng & Li, Fan & Liu, Mingjiang & Wang, Hongbo, 2024. "On compression level of hypersonic airflow in high-mach scramjet," Energy, Elsevier, vol. 295(C).
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Keywords
Ammonia mass injection pre-compressor cooling; Parametric optimization; Exergy analysis; High mach number aeroengine; Optimal operating line;All these keywords.
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