▪ Abstract Recent considerable progress in the field of rarefied hypersonic computational
fluid dynamics (CFD) gives reason to address its evolution to an independent CFD branch …

Hypersonic and high-enthalpy wind tunnels and their measurement techniques are the
cornerstone of the hypersonic flight era that is a dream for human beings to fly faster, higher …

高焓风洞及其试验技术是助力人类进入高超声速飞行时代的基石, 近年来取得了长足的进展.
本文首先重点介绍了四种典型驱动模式的高焓风洞, 即直接加热型高超声速风洞 …

In order to improve the operation of a high-enthalpy free piston shock tunnel its tuned
operation was studied analytically and experimentally. First, the piston motion in the free …

A zonal nonequilibrium model (ZNM) based on the concept of zonal representation of the
nonequilibrium relaxation times is proposed. ZNM, together with dynamic zone flamelet …

A high enthalpy shock tunnel is a potential facility for gaining knowledge to develop modern
aerothermodynamic and propulsion technologies. The largest high enthalpy shock tunnel …

The influence of localized nitrogen transpiration on second mode instabilities in a
hypersonic boundary layer is experimentally investigated. The study is conducted using a 7 …

Basic aerodynamic configurations are well suited to study fundamental aspects of high
enthalpy flows. A test campaign of the flow around a cylinder has been performed in the …

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 …

Combined free-stream disturbance measurements and receptivity studies in hypersonic
wind tunnels were conducted by means of a slender wedge probe and direct numerical …