Vortex-Exhaust Nozzle Interactions in Ramjets Combustors
COLORADO UNIV AT BOULDER DEPT OF MECHANICAL ENGINEERING
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The objective of our work was to understand the role of large scale vortical structures in the low-frequency pressure oscillation ramjet problem. We were particularly interested in vortex-nozzle interactions and the relative role of acoustically versus connectively coupled instability mechanisms.
- Combustion and Ignition
- Jet and Gas Turbine Engines