Numerical Investigation on the Response Characteristics of Hypersonic Boundary Layer under Different Types of Finite Amplitude Pulse Disturbance Waves

The hypersonic transient flow pass a blunt cone under three types of pulse disturbances is calculated using DNS. The response characteristic of hypersonic boundary layer among different types of pulse disturbance is compared. The distribution and evolution characteristics of disturbance modes are in...

Ausführliche Beschreibung

Bibliografische Detailangaben

Hauptverfasser:	X. Tang, J. Yu, H. Zhang, H. Li, M. Shi
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	Isfahan University of Technology 2021-01-01
Schriftenreihe:	Journal of Applied Fluid Mechanics
Schlagworte:	hypersonic flow; disturbance type; pulse wave; mode analysis; boundary layer.
Online-Zugang:	http://jafmonline.net/JournalArchive/download?file_ID=54355&issue_ID=1010
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