Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust
2018 Joint Propulsion Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust (AIAA 2018-4744)
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