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Thermodynamic coupling mechanisms in precooled turbine-based combined cycle:From fuel properties to multi-objective performance characterization

Yusen XU Yifan WANG Huoxing LIU Kun HE Jun ZENG Qinqin WANG Qinghui MA

中国航空学报（英文版）2026，Vol.39Issue(6)：162-179,18.

中国航空学报（英文版）2026，Vol.39Issue(6)：162-179,18.DOI:10.1016/j.cja.2025.103970

Thermodynamic coupling mechanisms in precooled turbine-based combined cycle:From fuel properties to multi-objective performance characterization

Yusen XU ¹Yifan WANG ¹Huoxing LIU ²Kun HE ¹Jun ZENG ³Qinqin WANG ³Qinghui MA³

作者信息

1. Research Institute of Aero-Engine,Beihang University,Beijing 102206,China
2. Research Institute of Aero-Engine,Beihang University,Beijing 102206,China||National Key Laboratory of Science and Technology on Aero-Engine and Aero-Thermodynamics,Beihang University,Beijing 102206,China
3. AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
折叠

摘要

关键词

Fuel thermophysical proper-ties/Hypersonic vehicles/Multi-objective parameter optimization/Precooled turbine-based combined cycle/Propulsion

Key words

Fuel thermophysical proper-ties/Hypersonic vehicles/Multi-objective parameter optimization/Precooled turbine-based combined cycle/Propulsion

引用本文复制引用

Yusen XU,Yifan WANG,Huoxing LIU,Kun HE,Jun ZENG,Qinqin WANG,Qinghui MA..Thermodynamic coupling mechanisms in precooled turbine-based combined cycle:From fuel properties to multi-objective performance characterization[J].中国航空学报（英文版）,2026,39(6):162-179,18.

基金项目

This study was supported by the National Natural Science Foundation of China(No.52406004),the China Aviation Industry Corporation's Independent Innovation Special Fund Project(No.JSYJ-2024-0155). （No.52406004）

中国航空学报（英文版）

ISSN：1000-9361

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