Mode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustor
Chengkun Lv, Haiqi Xu, Juntao Chang, Youyin Wang, Ruoyu Chen, Daren Yu
Topics & Concepts
RamjetCombustorMach numberGas compressorTurbineSpecific impulseThrustAerospace engineeringEngineeringMechanicsMechanical engineeringPhysicsChemistryCombustionOrganic chemistryComputational Fluid Dynamics and AerodynamicsGas Dynamics and Kinetic TheoryRocket and propulsion systems research