The vast majority of shock wave–boundary-layer interactions in practical applications like
supersonic aircraft intakes are three dimensional in nature. The complex behaviour of such …

Flexible panels deforming under pressure loads have been suggested as a passive form of
adaptive oblique shock control. This study investigates oblique shock–boundary-layer …

Nomenclature a= speed of sound, m/s Hi= incompressible shape factor l= fillet length, cm
M= Mach number p= static pressure, kPa pu= static pressure at the farthest upstream …

This report is the final report of a NASA Phase I SBIR contract, with some revisions to
remove company proprietary data. The Shock Boundary Layer Interaction (SBLI) …

A wedge-shaped micro vortex generator is placed on a flat plate over which a turbulent
boundary layer at Mach number 2.5 is developed. The interaction between an oblique shock …

Supervising Professor: Chaoqun Liu Vortices are seen everywhere in nature, from smoke
rings to tornadoes. Vortical structures play an essential role in the turbulence dynamics such …

Experiments and computations were made to obtain the influence of vortex generator on the
flow field around cylindrical protrusion. The experiments were performed using the …

Flow control is used on aerodynamic surfaces to improve flow quality by reducing or
eliminating undesirable flow features such as thick boundary layers and possible flow …