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...
| Những tác giả chính: | , , , , |
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| Định dạng: | Bài viết |
| Ngôn ngữ: | English |
| Được phát hành: |
Isfahan University of Technology
2021-01-01
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| Loạt: | Journal of Applied Fluid Mechanics |
| Những chủ đề: | |
| Truy cập trực tuyến: | http://jafmonline.net/JournalArchive/download?file_ID=54355&issue_ID=1010 |