Series view method based thermodynamic modeling and analysis for innovative precooled aeroengines with different turbine-compressor coupling schemes
Xuanfei Yu, Cong Wang, Daren Yu
Topics & Concepts
Overall pressure ratioGas compressorTurbineCombustionCombined cycleThermodynamic cycleGas turbinesAutomotive engineeringAir compressorCombustion chamberEngineeringMechanical engineeringNuclear engineeringChemistryOrganic chemistryRocket and propulsion systems researchHeat transfer and supercritical fluidsGas Dynamics and Kinetic Theory