Laminar-turbulent transition prediction in three-dimensional flows

By D. Arnal, G. Casalis. 2000

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Effects of Roughness on Hypersonic Boundary-Layer Transition (2007, unknown): “These mechanisms include the concave-wall Görtler instability [1], the first and second instability modes described by Mack [2], and the 3-D crossflow instability [3,4].”
Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels (2013, background): “The crossflow instability occurs in three-dimensional boundary layers, and has both traveling and stationary forms [5, 6, 7].”
Development of Hypersonic Quiet Tunnels (2008, unknown): “[8], [9], [10], [11] and [12]).”
Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies (2004, background): “Relevant instabilities include the concavewall Görtler instability [16], the first and second mode streamwise-instability waves described by Mack [17], and the 3D crossflow instability [18, 19].”