Particle Image Velocimetry Measurements of Unsteady Exhaust from a Linearized Continuous Detonation Combustor
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
2023
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Flow Measurements Using Particle Image Velocimetry in the Ultracompact Combustor
DOAJ | 2012
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