Corrugated and Composite Nozzle-Inlets for Thrust and Noise Benefits

The following research results are based on development of an approach previously proposed and investigated in for optimum nozzle design to obtain maximum thrust. The design was denoted a Telescope nozzle. A Telescope nozzle contains one or several internal designs, which are inserted at certain loc...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Gilinsky, M., Blankson, I. M., Gromov, V. G., Sakharov, V. I.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aircraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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