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

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...

書誌詳細
主要な著者:	X. Tang, J. Yu, H. Zhang, H. Li, M. Shi
フォーマット:	論文
言語:	English
出版事項:	Isfahan University of Technology 2021-01-01
シリーズ:	Journal of Applied Fluid Mechanics
主題:	hypersonic flow; disturbance type; pulse wave; mode analysis; boundary layer.
オンライン･アクセス:	http://jafmonline.net/JournalArchive/download?file_ID=54355&issue_ID=1010

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