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Transition mechanisms in hypersonic wind-tunnel nozzles: a methodological approach using global linear stability analysis.

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Bibliographic Details
Title: Transition mechanisms in hypersonic wind-tunnel nozzles: a methodological approach using global linear stability analysis.
Authors: Lemarquand, Hugo1, hugo.lemarquand@onera.fr, Lugrin, Mathieu1,2, Content, Cédric2,3, Caillaud, Clément3,4, Esquieu, Sébastien1,3, Sipp, Denis2,4
Source: Flow: Applications of Fluid Mechanics; 2025, Vol. 5, p1-21, 21p
Database: Applied Science & Technology Source
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