Linear modal instabilities around post-stall swept finite wings at low Reynolds numbers
Linear modal instabilities of flow over untapered wings with aspect ratios and 8, based on the NACA 0015 profile, have been investigated numerically over a range of angles of attack, and angles of sweep, at chord Reynolds numbers. Laminar base flows have been generated using direct numerical simulat...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Cambridge University Press
2022
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| Subjects: | |
| Online Access: | View Fulltext in Publisher |