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- W2356575883 abstract "This paper aims at developing a performance analysis tool to evaluate the performance and design constraints of aturbine based combined cycle engine concept withthe tandemlayout for a hypersonic cruise vehicle.To meet the conflict require-ments inthelongrangefromtake-off to Mach5,the combine cycle engine applies a variable cycle engine concept viathe modula-tion of five variable geometries andfuel flow.Thistool uses one-dimensional aerodynamic thermodynamic analysistechniques,con-sidering the test proved components characteristics andthe property of calorically perfect gas etc.The objects oriented software de-sign methodis adoptedinthe tool which can afford a platformsuitable for parametric cycle analysis,performance cycle analysisand control lawstudy of theturbofan mode,the ramjet mode andturbo/rammodetransition.Assisted bythistool,parametric cycleanalysis of the turbofan mode andthe ramjet mode was investigated.It shows recirculation marginis a keyfactor to be consideredinthe cycle parameters selection of the turbofan mode;highramjet afterburner discharge temperature isfavorable tothe ramjet cy-cle performance." @default.
- W2356575883 created "2016-06-24" @default.
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- W2356575883 date "2006-01-01" @default.
- W2356575883 modified "2023-09-23" @default.
- W2356575883 title "Performance Analysis Tool for Turbine Based Combined Cycle Engine Concept" @default.
- W2356575883 hasPublicationYear "2006" @default.
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