Stabilization of crossflow mode by grooves on a supersonic swept wing.

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Bibliographic Details
Title: Stabilization of crossflow mode by grooves on a supersonic swept wing.
Authors: Fedorov, Alexander1, afedorov55@gmail.com, Novikov, Andrey1,2
Source: Theoretical & Computational Fluid Dynamics; Apr2023, Vol. 37 Issue 2, p261-268, 8p
Database: Applied Science & Technology Source
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