高超声速流动

高超声速流动中侧向喷流干扰特性的实验研究

Experimental investigations of lateral jet interaction in hypersonic flows

单次扫描空间推进算法在高超声速流动中的适用性研究

Study on the reliability of a single-sweep space marching algorithm for hypersonic flows

高超声速流动转捩的数值研究

Numerical Research on Supersonic Flow Transition

高超声速流动滞止区预测；

Stagnation flow region prediction ;

针对高速流动，特别是超声速和高超声速流动的非平行边界层稳定性问题进行了研究。

The parabolized stability equations ( PSEs ) for high speed flows , especially supersonic and hypersonic flows , are derived and used to analyze the nonparallel boundary layer stability .

各种典型算例的计算表明该方法数值计算稳定，捕捉激波分辨率高，能很好地模拟超声速和高超声速流动中激波反射及激波与边界层的干扰等各种复杂流动现象。

Typical illustrations indicate that the algorithm is quite robust and can generate good shock capturing properties , and simulate correctly some complicated problems of supersonic and hypersonic viscous flow , such as the reflection of shock , the interference between shock and layer .

化学非平衡高超声速电离流动数值研究

Numerical Study of Hypersonic Ionized Flows in Chemical Nonequilibrium

高超声速复杂流动中湍流模式应用的评估

Turbulence modeling validation in hypersonic complex flows

超声速风洞的起动过程涉及到湍流、激波及低亚声速和高超声速混合流动，是一个非常复杂的瞬态过程。

The starting process of wind tunnel , involving turbulence , shock wave , low subsonic and high supersonic mixing flows , is a very complex transient process .

基于线性稳定性的结果，以类似于处理湍流脉动的方式来模化流场脉动，用以研究高超声速的流动转捩，包括转捩起始位置及转捩区长度。

Based on the liner stability analysis , a approach that treats non-turbulent fluctuations in a turbulence-like manner is used to research supersonic flow transition including onset and extent of transition .

绕HERMES外形高超声速无粘流动的数值模拟

Numerical Simulation of Hypersonic Inviscid Flow Around the HERMES Configuration

高超声速边界层流动转捩研究

Stability and Transition of Hypersonic Boundary Layer Flow

依据流动子过程特征量分析方法，导出了高超声速化学反应流动的相似律。

According to the analyzing method of characteristic quantities for flow 's sub processes , this paper presents a law of similitude for hypersonic chemical reaction flows .

高超声速化学非平衡流动MHD效应的数值模拟

Numerical simulation of MHD effects on hypersonic chemical nonequilibrium flow

绕Apollo飞船的高超声速化学非平衡流动的数值模拟

Numerical simulation for hypersonic flow of nonequilibrium gases around the Apollo command module

高超声速飞行器/发动机流动控制研究

Study on Flow Controls for Hypersonic Flying Vehicle Fuselage / Propulsion