DEMONSTRATED LOW LOSS AND LOW EQUIVALENCE RATIO OPERATION OF A ROTATING DETONATION ENGINE FOR POWER GENERATION
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
Pressure gain combustion ; 373-388
2020
Aufsatz (Konferenz)
Englisch
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Equivalence Ratio Scans in a Rotating Detonation Engine
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