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

The basic problems of transition in both incompressible and compressible boundary layers
are reviewed. Flow structures in low-speed transitional and developed turbulent boundary …

高超声速边界层转捩对高超声速飞行器气动设计具有重要影响. 转捩控制一直是转捩研究的主要
目的之一, 在高超声速情况下主要采用粗糙元进行边界层转捩控制. 回顾了近年来不同类型粗糙 …

The fluid flow phenomenon of boundary layer transition is a complicated and difficult
process to model and predict. The importance of the state of the boundary layer with regard …

Interest in the development of micro vortex generators (MVGs) to control high-speed flow
separation has grown in the last decade. In contrast to conventional vortex generators …

This paper describes the design of a class of three-dimensional (3D) smooth humps
mounted on a yawed cone model for a high-precision compressible Navier–Stokes solver …

The hypersonic flow around a tip of a rocket-mounted Hypersonic Boundary-Layer
Transition experiment has been simulated with direct numerical simulations. The numerical …

Hypersonic boundary layer transition induced by an isolated cylindrical roughness element
is investigated using direct numerical simulation method based on a finite volume …

Hypersonic boundary layer transition from laminar to turbulent induced by three isolated
roughness elements (ramp, diamond, and cylinder) was investigated by direct numerical …

This work expands on previous efforts that observed high-intensity resonance in the
dynamic shock motion generated by shock wave/boundary layer interactions with Mach 1.8 …