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physics.flu-dyn2023★ 1 cited
Adjoint-based linear sensitivity of a hypersonic boundary layer to steady wall blowing-suction/heating-cooling
Arthur Poulain, Cédric Content, Georgios Rigas +2
For a Mach 4.5 flat-plate adiabatic boundary layer, we study the sensitivity of the first, second Mack modes and streaks to steady wall-normal blowing/suction and wall heat flux. T…
physics.flu-dyn2023
Global stability analysis of a hypersonic cone-cylinder-flare geometry
Clément Caillaud, Mathieu Lugrin, Sébastien Esquieu +1
Characterizing the boundary layer transition to turbulence around realistic hypersonic vehicles is a challenging task due to the numerous parameters that affect the process. To add…