Experimental results for a two-dimensional supersonic inlet used as a thrust deflecting nozzle

Nearly all supersonic V/STOL aircraft concepts are dependent on the thrust deflecting capability of a nozzle. In one unique concept, referred to as the reverse flow dual fan, not only is there a thrust deflecting nozzle for the fan and core engine exit flow, but because of the way the propulsion sys...

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Bibliographische Detailangaben

Hauptverfasser:	Johns, Albert L., Burstadt, Paul L.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Fluid Mechanics And Heat Transfer
Online-Zugang:	Volltext bestellen
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