Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; 2009 ; Orlando , Florida
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure
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