The shock wave/boundary-layer interaction is a common phenomenon, and it occurs in the
internal and external flow fields of the hypersonic vehicle. Then, the separation, the …

The paper summarizes recent developments in boundary layer suction for high-speed air
intakes. Bleed has been efficiently used in supersonic and hypersonic intakes for three …

The separation bubble caused by the shock wave/boundary layer interaction (SWBLI) has
adverse influence on the field performance, and the passive control approach should be …

Liutex and Its Applications in Turbulence Research reviews the history of vortex definition,
provides an accurate mathematical definition of vortices, and explains their applications in …

In this paper, we utilized high-speed schlieren technology to investigate the impact of
expansion degrees on the evolution of subsonic-supersonic mixing layers. Specifically, we …

The supersonic mixing layer in a model scramjet has been simulated using large eddy
simulation (LES) with the consideration of complex shock waves. A comparison with …

In this paper, a new visualization method for vortex structure is presented. Several widely
used techniques for local vortex visualization in turbulent flows are reviewed and compared …

Despite 150 years of research after the reference work of Stokes, it should be acknowledged
that some confusion still remains in the literature regarding the importance of bulk viscosity …

Shock oscillation with low-frequency unsteadiness commonly occurs in supersonic flows
and is a top priority for the control of flow separation caused by shock wave and boundary …

In this paper, a novel slotted ramp-type micro vortex generator (slotted micro-ramp) for flow
separation control is simulated in the supersonic flow of Ma= 1.5, based on large eddy …