Aerodynamics, aerothermodynamics and thermal protection system response in high-
enthalpy and high-speed flow is heat transfer with interface effects in nature. Modelling and …

A hypersonic, spatially evolving turbulent boundary layer at Mach 12.48 with a cooled wall is
analysed by means of direct numerical simulations. At the selected conditions, massive …

边界层由层流向湍流的转捩是高超声速飞行器设计面临的重大空气动力学问题.
随着飞行速域与空域的不断拓展, 高超声速高焓边界层中的高温气体效应会使得量热完全气体 …

The influence of high-enthalpy effects on hypersonic turbulent boundary layers is
investigated by means of direct numerical simulations (DNS). A quasiadiabatic flat-plate air …

There has been renewed interest in supersonic modes in hypersonic boundary layers,
which have been previously thought to be insignificant due to their smaller amplitudes than …

The prediction of the transition dynamics of high-enthalpy boundary-layer flows requires
appropriate thermodynamic and transport models. This work quantifies the influence of …

Supersonic modes, previously thought to be insignificant due to their smaller amplitude than
Mack's traditional second mode, occur in hypersonic boundary layers when a disturbance …

There has been renewed interest in studying supersonic modes in hypersonic boundary
layers. Recent computational results have shown supersonic modes in hot-wall flows …

Realistic flight vehicles for reentry into the Earth's atmosphere are commonly similar to
blunted cones. The main reason for blunting a cone is to mitigate high heat loads at the …

We investigate the hydrodynamic stability of compressible boundary layers over adiabatic
walls with fluids at supercritical pressure in the proximity of the Widom line (also known as …