1.
NUMERICAL SIMULATION OF PASSIVE SCALAR IN SUPERSONIC PLANAR MIXING LAYERS
超音速平板混合层被动标量的数值模拟
2.
The Numerical Study of the Enhancement Effect in 3D Supersonic Mixing Layer with Swirl;
三维超音速旋转混合层增混作用的数值研究
3.
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
4.
NUMERICAL MODELING OF SUPERSONIC FLUORINE/ HYDROGEN COLD FLAME IN LAMINAR MIXING REGIME
超音速层流混合氟/氢冷火焰的模型计算
5.
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
6.
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
7.
Properties of Cu-Al_2O_3 Composite Coating in Supersonic Cold Gas Dynamic Spraying
超音速冷喷涂Cu-Al_2O_3复合涂层特性
8.
The quantificational measurement of supersonic mixing layer growth rate
超声速混合层增长速度定量测量与比较
9.
Investigations of Supersonic Mixing Enhancement Technology and Drag of Strut;
支板超声速混合增强技术及其阻力特性研究
10.
Investigation on supersonic cold flow and liquid jet over struts
支板超声速冷流流场及液体喷流混合特性
11.
Numerical Analysis of Damage in FRP/Metal Hybrid Laminates Under Low Velocity Impact;
FRP/金属混杂层合板低速冲击损伤数值分析
12.
Integrated Modeling of Ballistic Limit Equations of Single Plate under Hypervelocity Impact
单层板超高速撞击弹道极限方程综合建模
13.
Bonding mechanism of WC-12Co coatings prepared by supersonic plasma spraying on 45 steel
超音速等离子喷涂WC-12Co涂层的结合机理
14.
The Design and Experimental Studies of Supersonic Straight Through Wind Tunnel and "Supersonic-supersonic" Mixing Layer Wind Tunnel;
直连式超声速风洞与“超—超”混合层风洞的设计和实验研究
15.
Non-linear Time Series Analysis of Evolution Status of Supersonic Mixing Layer
超声速混合层发展情况的非线性时间序列分析
16.
Study of hybrid scheme for the prediction of aerodynamic heat transfer-rate in hypersonic laminar flow
高超声速层流气动热预测混合算法研究
17.
Large eddy simulation of two-phase mixing layer with droplets
超声速混合层液滴两相流动的大涡模拟
18.
Nonlinear analysis of large eddy simulated supersonic two-phase mixing layer
大涡模拟超声速两相流混合层的非线性分析