Shock train behavior affected by continuous Mach number variation of incoming flow

Experimental and numerical investigations have been performed to study the influence of continuous Mach number variation on the shock train. An adjustable Laval nozzle which could continuously change the throat area was developed to change the Mach number from 2.4 to 1.8. As the incoming flow Mach n...

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Veröffentlicht in:	Acta astronautica 2020-12, Vol.177, p.652-665
Hauptverfasser:	Hou, Wenxin, Chang, Juntao, Wang, Ziao, Wang, Youyin, Bao, Wen
Format:	Artikel
Sprache:	eng
Schlagworte:	Background waves Continuous mach number variation Downstream effects Mach number Nozzles Oscillation type Oscillations Shock train Upstream Waves
Online-Zugang:	Volltext
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