The origins of transition to turbulence in a bounded shear flow within a low disturbance
environment are typically found in the instabilities of the basic state. There are, of coursc, a …

Görtler instability occurs due to the action of centrifugal forces in boundary layers over
curved surfaces, where it most commonly results in the generation of steady streamwise …

This work is focused on a hypersonic aeroelastic experiment involving a shock im**ing on
compliant cantilevered plate at Mach 5.8. The shock induces a pressure differential across …

Görtler vortices developed in laminar boundary layer experience remarkable changes when
the flow is subjected to compressibility effects. In the present study, five. The subharmonic …

A sharp leading-edge ramp model with 15°, 20°, and 25° ramp angles is experimentally
investigated at a freestream Mach number 7.7 and a unit Reynolds number 4.2× 10 6 m− 1 …

Görtler vortices are thought to be the cause of transition in many fluid flows of practical
importance. In this paper a review of the different stages of vortex growth is given. In the …

This work presents an experimental and numerical study of hypersonic transitional shock-
wave–boundary-layer interaction, wherein transition occurs between separation and …

The receptivity problem for Görtler vortices induced by wall roughness is investigated. The
roughness is modelled by small amplitude perturbations to the curved wall over which the …

Görtler vortices (GVs) in dual-incident shock-wave/turbulent-boundary-layer interactions
(dual-ISWTBLIs) are experimentally investigated in a Mach 2.48 flow. A double-wedge …

This work discusses the design, measurement, and simulation of an oscillating shock-
wave/boundary-layer interaction on a flat plate at Mach 5.8 and R e∞= 7× 10 6 m− 1. The …