Understanding, modeling and control of the high-speed wall-bounded transition and
turbulence not only receive wide academic interests but also are vitally important for high …

Direct numerical simulations (DNS) are performed to investigate the spatial evolution of flat-
plate zero-pressure-gradient turbulent boundary layers over long streamwise domains () …

The inherent difficulty of understanding turbulence has led to researchers attacking the topic
in many different ways over the years of turbulence research. Some approaches have been …

The need for better understanding of the low-frequency unsteadiness observed in shock
wave/turbulent boundary layer interactions has been driving research in this area for several …

We study the organization of turbulence in supersonic boundary layers through large-scale
direct numerical simulations (DNS) at, and momentum-thickness Reynolds number up to …

A model to explain the low-frequency unsteadiness found in shock-induced separation is
proposed for cases in which the flow is reattaching downstream. It is based on the properties …

In this paper, we perform direct numerical simulations (DNS) of turbulent boundary layers
with nominal free-stream Mach number ranging from 0.3 to 12. The main objective is to …

In this paper, we perform direct numerical simulation (DNS) of turbulent boundary layers at
Mach 5 with the ratio of wall-to-edge temperature Tw/Tδ from 1.0 to 5.4 (Cases M5T1 to …

The low-frequency unsteadiness is characterized in the direct numerical simulation of a
shock wave–turbulent boundary layer interaction generated by a compression ramp in Mach …

Direct numerical simulation data of a Mach 2.9, 24○ compression ramp configuration are
used to analyse the shock motion. The motion can be observed from the animated DNS data …