Computational Study of an Axisymmetric Dual Throat Fluidic Thrust Vectoring Nozzle for a Supersonic Aircraft Application
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2007-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2007
|British Library Conference Proceedings | 2007
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