Hypersonicflow相关论文
The reaction control systems(RCS)will be the main and key technology to implement the highmaneuver,fast response,and hig......
The technology of oil visualization is be used to depict the local separation flowfield structures induced by 3D wedge w......
Study on the characteristics of interaction flowfields induced by supersonic jet on a revolution bod
When a sonic or supersonic jet is injected laterally into supersonic or hypersonic free stream,the complex jet interacti......
Deflected beam visualization(such as Schlieren and shadowgraph technique)is usually used to detect the flow structure in......
High Speed Schlieren Visualization of Hypersonic Separated Flow Induced by a Perpendicular Blunt Fin
Shock wave/boundary layer interaction,which often accompanied by separation,is a common feature of high speed flow o......
The configuration and structure of hypersonic vehicles are becoming more complicated,which is bringing about more in......
Visualization of Separated Flow Features Induced by different Geometric Shapeof Cylinder at Hyperson
During the last seven decades,extensive work has been done on the separated flows induced by the shock wave/boundary......
The non-equilibrium dissociation of oxygen in air is studied using a quasi-one-dimensional model for hypersonic flow......
The efficient parabolized stability equation (PSE) for hypersonic flow stability, which is very important for develo......
A hybrid CFD/characteristic method(CCM) was proposed for fast design and evaluation of hypersonic inlet flow with nose b......
Investigation of hypersonic flows through a cavity with sweepback angle in near space using the DSMC
Near space has been paid more and more attentionin recent years due to its military application value.However,flow chara......
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiat
The strong background radiation in high enthalpy hypersonic shock tunnels has posed severe challenges for measurement us......
给出半圆柱前缘舵诱导的高超声速湍流分离激波运动特性。实验气流Ｍ数为７．８，单位长度Ｒｅ为３．５＊１０＾７／ｍ。......
