Acoustic Characteristics of Compressible Jet from Different Nozzle exit Geometry
25th AIAA/CEAS Aeroacoustics Conference
01.01.2019
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure
British Library Conference Proceedings | 2009
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