Hypersonic boundary layer (BL) transition generates a significant increase in viscous drag
and heat flux, which leads to severe restrictions on the performance and thermal protection …

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 …

The effects of a wavy wall on the stability of a hypersonic boundary layer on a flared cone
are investigated by detailed experimental measurements and direct numerical simulations …

高超声速边界层转捩直接影响飞行器表面的摩擦系数与热流分布, 对于高超声速飞行器的气动
布局以及热防护设计至关重要. 尽管高超声速边界层层/湍流转捩的相关研究已经开展长达半个 …

In this study, a numerical investigation of the perturbation evolution in a Mach 6 flat-plate
boundary layer with a local heating or cooling strip is presented. The position of the …

Hypersonic flow over a two-dimensional compression corner is investigated using
computational fluid dynamics and global resolvent analysis in this study, which is a …

Hypersonic boundary layer transition is a hot yet challenging problem restricting the
development and breakthrough of hypersonic aerodynamics. In recent years, despite great …

由于高超声速情况下边界层从层流转捩成湍流后, 壁面摩阻和热流出现数倍增长,
控制高超声速边界层使转捩延迟对飞行器减阻降热具有十分重要的意义. 本文首先概述了高 …

The influence of a wavy wall on the hypersonic boundary layer transition and the related
aerodynamic heating is investigated on a flared cone at a range of unit Reynolds numbers …

In the paper, the results of numerical modeling are presented of the 3D turbulent flows in a
channel with backward-facing step, and argon jets injected into the supersonic crossflow …