INFLUENCE OF INJECTOR-TO-ANNULUS AREA RATIO ON ROTATING DETONATION ENGINE OPERABILITY
AIAA Propulsion and Energy Forum ; 2019 ; Indianapolis, Ind.
Pressure gain combustion ; 131-143
2019
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Role of Ignition Delay in Rotating Detonation Engine Performance and Operability
AIAA | 2019
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