Thermodynamic coupling mechanisms in precooled turbine-based combined cycle:From fuel properties to multi-objective performance characterizationOA
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
Research Institute of Aero-Engine,Beihang University,Beijing 102206,ChinaResearch Institute of Aero-Engine,Beihang University,Beijing 102206,ChinaResearch 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,ChinaResearch Institute of Aero-Engine,Beihang University,Beijing 102206,ChinaAECC Sichuan Gas Turbine Establishment,Chengdu 610500,ChinaAECC Sichuan Gas Turbine Establishment,Chengdu 610500,ChinaAECC Sichuan Gas Turbine Establishment,Chengdu 610500,China
Fuel thermophysical proper-tiesHypersonic vehiclesMulti-objective parameter optimizationPrecooled turbine-based combined cyclePropulsion
Fuel thermophysical proper-tiesHypersonic vehiclesMulti-objective parameter optimizationPrecooled turbine-based combined cyclePropulsion
《中国航空学报（英文版）》 2026 (6)
162-179,18
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).
评论