Response of a Hypersonic Boundary Layer to Freestream Pulse Acoustic Disturbance

The response of hypersonic boundary layer over a blunt wedge to freestream pulse acoustic disturbance was investigated. The stability characteristics of boundary layer for freestream pulse wave and continuous wave were analyzed comparatively. Results show that freestream pulse disturbance changes th...

Descripción completa

Detalles Bibliográficos
Autores principales: Wang, Zhenqing, Tang, Xiaojun, Lv, Hongqing
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2014
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3967397/
https://www.ncbi.nlm.nih.gov/pubmed/24737993
http://dx.doi.org/10.1155/2014/748504

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3967397/
https://www.ncbi.nlm.nih.gov/pubmed/24737993
http://dx.doi.org/10.1155/2014/748504

Ejemplares similares