1.
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
2.
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
3.
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
4.
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
5.
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
6.
An example for hypersonic blunted cone flow in ballistic range is illustrated.
示例给出了弹道靶中高超声速钝锥流动的应用
7.
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
8.
Analysis of dynamic images based on wavelet transform in a hypersonic boundary layer
基于小波变换的高超声速边界层动态图像分析
9.
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
10.
NUMERICAL SIMULATION OF SUPERSONIC SEPARATED FLOW OVER BLUNT CONES AT HIGH ANGLES OF ATTACK
钝锥大攻角超声速分离流场的数值模拟
11.
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
12.
Weak Nonlinear Evolution of Small Amplitude Disturbances in 2D Supersonic Boundary Layer
小扰动在二维超声速边界层中的弱非线性传播
13.
Examination of the application of BL model in supersonic turbulent boundary layers
BL模式在超声速湍流边界层中应用的检验
14.
Performance and boundary layer of flow in axisymmetric mixed-compression supersonic inlet with cavity
槽对超声速混压式进气道性能及边界层的影响
15.
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.
16.
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
17.
Integrative Hypersonic Waverider Design Based on Osculating Cones Method;
基于密切锥方法的高超声速乘波机一体化设计
18.
Numerical Simulation on Hypersonic Flowfield of Cone-derived Waverider
高超声速锥导乘波体流场的数值模拟研究