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...

Descrizione completa

Salvato in:
Dettagli Bibliografici
Autori principali: X. Tang, J. Yu, H. Zhang, H. Li, M. Shi
Natura: Artigo
Lingua:Inglês
Pubblicazione: Isfahan University of Technology 2021-01-01
Serie:Journal of Applied Fluid Mechanics
Soggetti:
hypersonic flow; disturbance type; pulse wave; mode analysis; boundary layer.
Accesso online:http://jafmonline.net/JournalArchive/download?file_ID=54355&issue_ID=1010
Tags: Aggiungi Tag
Nessun Tag, puoi essere il primo ad aggiungerne! !

Documenti analoghi