Shock-wave structure of supersonic gas flows in a radial nozzle

In the present paper, results of a study of supersonic flows in radial nozzles of various widths, and jet flows discharged into ambient space, are reported. We show that, at fixed nozzle inlet area, depending on the nozzle width, two types of nozzle flow are possible. If the nozzle width is greater...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Kiselev, S. P., Kiselev, V. P., Zaikovskii, V. N., Trubacheev, G. V.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Deceleration Gas flow Nozzle flow Nozzles Shock waves
Online-Zugang:	Volltext
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