1.
Experimental Investigations of Hypersonic Boundary Layer Transition on a Sharp Cone Based on the Method of Wavelet Analysis;
基于小波分析方法的高超音速尖锥边界层转捩的实验研究
2.
The Numerical Study of Evolution of Perturbations in the Supersonic Blunted Cone Boundary Layer Flow;
高超音速钝锥边界层中扰动演化的数值研究
3.
Stability Characteristics of the Boundary Layer of an Axisymmetric Blunt Nosed Cone in the Supersonic and Hypersonic Flow
超声速高超声速球锥绕流的边界层稳定性特点初探
4.
The Stability Analysis and Transition Pridiction of the Hypersonic Boundary Layer over Blunt Cone at Zero Angle of Attack
高超声速零攻角钝锥边界层稳定性分析及转捩预测
5.
Numerical simulation of disturbance evolution in the boundary layer of a hypersonic blunt cone at low incidence
小攻角高超声速钝锥边界层内扰动演化的数值模拟
6.
Direct numerical simulation of a spatially evolving hypersonic blunt cone turbulent boundary layer at Mach 6
马赫数为6的高超声速钝锥湍流边界层空间演化的直接数值模拟
7.
A Numerical Study of the Evolution of Perturbations in Hypersonic Flat Plate Boundary Layer at High Altitude;
高空高超音速平板边界层扰动演化的数值研究
8.
A NEW TRANSITION/TURBULENCE MODEL FOR THE FLOW TRANSITION IN SUPERSONIC BOUNDARY LAYER
一种适用于超音速边界层的湍流转捩模式
9.
The Mechanism of Laminar-turbulent Transition and the Characteristics of Turbulence in a Supersonic Boundary Layer on a Flat Plate;
超音速平板边界层从层流到湍流的转捩机理及湍流特性
10.
A Numerical Study for the Generation of Shocklet by 3-D Disturbance in Supersonic Boundary Layer;
超音速边界层中三维扰动引起小激波的数值研究
11.
The Study of Receptivity of Supersonic Boundary-layer to Local Periodic Disturbance in Free-stream;
超音速边界层对自由流中空间局部周期扰动感受性问题的研究
12.
A Numerical Study for the Resonant Triad Interaction and Secondary Instability in a Three-dimensional Supersonic Boundary Layer;
三维超音速边界层中三波共振和二次失稳机制的数值模拟研究
13.
A Numerical Study of the Evolution of the Disturbance in 2-D Supersonic Boundary Layer with Pressure Gradient;
具有压力梯度的二维超音速边界层扰动演化的数值模拟研究
14.
The Effects of Thermophysical Parameters of Air on the Stability of Two-dimensional Supersonic Boundary Layer on a Flat Plate
热物性参数对超音速平板边界层稳定性影响研究
15.
A Numerical Study of the Evolution of 2-D Disturbance in Supersonic Sharp Cone Boundary Layer with Zero Angle of Attrack;
零攻角尖锥边界层中二维扰动演化特征的数值研究
16.
Using Roughness Surface on Control of Supersonic Laminar Flow Boundary Layer
用表面粗糙度控制超声速层流边界层
17.
A study of the boundary condition in the DNS of the supersonic boundary layer flow
超声速边界层流动数值模拟的边界条件研究
18.
The interaction between an oblique blast wave and supersonic blunt conewas discussed.
本文讨论了斜爆炸波与超音速钝锥激波层的相互作用问题.