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- W2371686824 abstract "To discuss the operating characteristics of the inlet which is used in Turbojet/Ramjet Combined Cycle engine at Mach 0 to 5,the profile of an over/under TBCC variable geometry inlet was given.Using CFD tools,the two-dimensional flow-field of the inlet was shown with properties of flow at different operating points.At every flight Mach number,the inlet can start without boundary layer suction.Based on the flow-field of cruise and transition states,the operating characteristics at different back pressure were analyzed.The result indicates that the back pressure at exit has effect on the performance of the inlet,especially at the transition state——change of back pressure between over and under exit can bring on aerodynamic coupling effects in the two ducts.The aerodynamic characteristic diagram varied with flight conditions of the inlet was presented.The factors affecting the performance of the inlet and the aerodynamic characteristics at typical flight conditions were analyzed." @default.
- W2371686824 created "2016-06-24" @default.
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- W2371686824 date "2008-01-01" @default.
- W2371686824 modified "2023-09-28" @default.
- W2371686824 title "Aerodynamic characteristics of over/under inlet for turbine based combined cycle engine" @default.
- W2371686824 hasPublicationYear "2008" @default.
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