Time-Resolved Stagnation Pressure Measurement Technique in a Rotating Detonation Rocket Combustor
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
2023
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Performance analysis of a rotating detonation combustor based on stagnation pressure measurements
German Aerospace Center (DLR) | 2020
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