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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, Mathieu^1,2, Content, Cédric^2,3, Caillaud, Clément^3,4, Esquieu, Sébastien^1,3, Sipp, Denis^2,4
Source:	Flow: Applications of Fluid Mechanics; 2025, Vol. 5, p1-21, 21p
Database:	Applied Science & Technology Source

Description
DOI:	10.1017/flo.2025.10033