Shock/shock interactions (SSIs) often lead to high thermal loads. To understand the
influences of thermochemical non-equilibrium effects on the Type III SSI, four gas models …

低空域高速飞行条件下的飞行器表面边界层具有高马赫数, 高雷诺数, 高总焓的特点.
较高的来流雷诺数使边界层发生从层流到湍流的转捩, 而强激波压缩形成的高温环境将导致气体 …

As a classic aerodynamic phenomenon, shock-shock interferences (SSI)[1-6] widely present
in high-speed vehicles' internal and external flow fields. This phenomenon has received …

ABSTRACT A review is presented of the characteristics of regions of shock interaction in
laminar, transitional and turbulent hypersonic flows and the simple prediction methods to …

HYPERSONIC shock/shock interference ows might be the most complicated ow problems
that appear around the hypersonic vehicle. Edney1 classifi ed them into six types. The most …

A new variation of holographic interferometry has been utilized to perform simultaneous two-
wavelength measurements, allowing quantitative analysis of the heavy particle and electron …

In this paper, we summarize the most important results from an extensive series of studies
conducted over a range of Reynolds numbers from 102 to 106 at Mach numbers from 6 to 18 …

In order to obtain a good quality ie parallel and uniform flow in the test section of the High
Enthalpy Shock Tunnel Göttingen (HEG) the facility was equiped with an axisymmetric …

This paper describes the numerical solutions of type‐IV shock‐on‐shock interactions in
hypersonic thermochemical nonequilibrium air flows around blunt bodies. The Navier …

Numerical solutions of shock-on-shock interactions are presented for hypersonic
thermochemical nonequilibrium air flows around a blunt body. The Navier-Stokes equation …