Despite over fifty years of research on shock wave boundary layer effects and interactions,
many related technical issues continue to be controversial and debated. The present survey …

The normal shock wave-boundary layer interaction (SBLI) phenomenon is known to
constitute a main factor limiting the aerodynamic performance in many aeronautical …

A modeling framework for boundary layer effusion has been developed based on the use of
source (or sink) terms instead of the usual practice of specifying bleed directly as a boundary …

Assessment of various low-Re two-equation turbulence models in transonic flow with shock-
boundary layer interaction and separation, is presented. The study includes seven different …

The passive control of a shock wave-boundary-layer interaction involves placing a porous
surface beneath the interaction, allowing high pressure air from the flow downstream of the …

Passive control applied to a turbulent shock wave/boundary layer interaction has been
investigated by considering a two-dimensional channel flow. The field resulting from …

Abstract Shock-Wave/Boundary layer Interaction is a complex phenomenon commonly
occurring in all high-speed flow applications. Scramjets, re-entry vehicles, launch vehicles …

Passive control applied to a turbulent shock wave/boundary layer interaction has been
investigated by considering a two-dimensional channel flow. The field resulting from …

In aircraft with jet propulsion engine intakes at supersonic speed, strong pressure waves
referred to as shock waves occur, which may interact with any present boundary layers …

The present contribution describes two prediction methods for flows around transonic
airfoils, including shock control devices. The whole work was done in the frame of the …