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...

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Bibliographic Details
Main Authors: Zhenqing Wang, Xiaojun Tang, Hongqing Lv
Format: Article
Language:English
Published: Wiley 2014-01-01
Series:The Scientific World Journal
Online Access:http://dx.doi.org/10.1155/2014/748504
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