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...

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Những tác giả chính:	X. Tang, J. Yu, H. Zhang, H. Li, M. Shi
Định dạng:	Bài viết
Ngôn ngữ:	English
Được phát hành:	Isfahan University of Technology 2021-01-01
Loạt:	Journal of Applied Fluid Mechanics
Những chủ đề:	hypersonic flow; disturbance type; pulse wave; mode analysis; boundary layer.
Truy cập trực tuyến:	http://jafmonline.net/JournalArchive/download?file_ID=54355&issue_ID=1010

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