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 …

We study the structure of high-speed zero-pressure-gradient turbulent boundary layers up to
friction Reynolds number and heat transfer at the wall are considered. The present …

In this work, the linear responses of turbulent mean flow to both harmonic and stochastic
forcing are investigated for supersonic channel flow. Well-established universal relations are …

It is generally believed that the temperature and the velocity fields are highly coupled in
compressible wall-bounded turbulence. In the present study, we employ a linear model, ie …

There are fewer reports on the impinging shock/boundary layer interaction in the high Mach
number and high-temperature flow than that in the supersonic flow. High-temperature flow …

High-speed vehicles experience a highly challenging environment in which the freestream
Mach number and surface temperature greatly influence aerodynamic drag and heat …

The complex behaviours of supersonic turbulent boundary-layer flows interacting with
combustion is explored through the use of direct numerical simulations. The chosen flow …

Boundary layer transition from laminar to turbulence is of vital importance to the design of
hypersonic vehicles. With continuous expansion of flight speed and altitude domains, the …

The Reynolds number and wall cooling effects on correlations between the thermodynamic
variables are systematically investigated in hypersonic turbulent boundary layers by direct …

An extension to the normal shock relations for a thermally perfect, calorically imperfect gas,
modelling the vibrational excitation with an anharmonic oscillator model and including the …