Experimental Investigation of Nozzle Exit Reflector Effect on Supersonic Jet

The present study describes an experimental work to investigate the effect of a nozzle exit reflector on a supersonic jet that is discharged from a convergent–divergent nozzle with a design Mach number of 2.0. An annular reflector is installed at the nozzle exit and its diameter is varied. A high-qu...

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Veröffentlicht in:	Shock waves 2006-07, Vol.15 (3-4), p.229-239
Hauptverfasser:	Kweon, Y.-H., Miyazato, Y., Aoki, T., Kim, H.-D., Setoguchi, T.
Format:	Artikel
Sprache:	eng
Schlagworte:	Convergent-divergent nozzles Diameters Impact loads Jets Mach number Pressure measurement
Online-Zugang:	Volltext
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