Direct numerical simulations of the shock-induced separation of a laminar boundary layer

Guillaume Fournier (1) , Amer Chpoun (1) , Yann Fraigneau (2) , Christian Tenaud (2)

1 LMEE - Laboratoire de Mécanique et d'Energétique d'Evry
2 LIMSI - Laboratoire d'Informatique pour la Mécanique et les Sciences de l'Ingénieur

In the aeronautical and aerospace industries, the flow configurations where an incident oblique shock wave impinges upon a boundary layer are very common. The supersonic flow around an aircraft, in a rocket nozzle or in a supersonic inlet are some examples among others.

Domaines: Mécanique [physics.med-ph]

Guillaume Fournier, Amer Chpoun, Yann Fraigneau, Christian Tenaud. Direct numerical simulations of the shock-induced separation of a laminar boundary layer. Direct and Large-Eddy Simulation X, 24, pp.327-332, 2017, 9783319632117. ⟨10.1007/978-3-319-63212-4_41⟩. ⟨hal-01629644⟩