This article reviews the hypersonic laminar-turbulent boundary layer transition over a blunt
circular cone under support of the National Key Research and Development Program of …

APCAT II (Long-Term Advanced Propulsion Concepts and Technologies)[1] is a follow-up of
the previous EC co-funded project LAPCAT [2]. The objective is to develop different vehicle …

Boundary layer transition over a lifting body of 1.6 m length at. The model geometry is the
same as the Hypersonic Transition Research Vehicle designed by the China Aerodynamics …

The linear global instability and resulting transition to turbulence induced by an isolated
cylindrical roughness element of height) roughness element sustaining only the sinuous …

Görtler vortices developed in laminar boundary layer experience remarkable changes when
the flow is subjected to compressibility effects. In the present study, five. The subharmonic …

A numerical investigation is carried out to study the transition of a subsonic boundary layer
on a flat plate with roughness elements distributed over the entire surface. Post-transition …

Global stability analysis and direct numerical simulation of boundary layers with an isolated
roughness element Page 1 J. Fluid Mech. (2022), vol. 949, A12, doi:10.1017/jfm.2022.749 Global …

This paper is concerned with the rather broad issue of the impact of abrupt changes (such as
isolated roughness, gaps and local suctions) on boundary-layer transition. To fix the idea …

Large eddy simulations were conducted to investigate the effects of distributed roughness
on separated flow transitions over a highly loaded compressor blade at a Reynolds number …

Flow phenomena on maneuverable vehicles that fly at hypersonic speeds and altitudes that
reach the Earth's upper stratosphere and lower mesosphere pose challenges that …