1.
Prediction method for noise radiated from boundary layer transition
边界层转捩区声辐射的预报方法研究
2.
The experiments successfully indicated that the transition location of laminar boundary layer can be controlled by internal acoustic excitation with an appropriate input power in a frequency range which is far beyond the Tollmien-Schlichting wave range.
实验结果表明:边界层转捩位置可以用内声激发扰动控制。
3.
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
4.
The Influence of Root Fillet and Boundary Layer Transition on the Aerodynamic Performance of Centrifugal Impeller;
叶根倒角及边界层转捩对离心叶轮气动性能的影响
5.
Transition studies for the boundary layer on a swept wing based on sublimation technique
基于升华法实验研究后掠翼三维边界层的转捩
6.
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
7.
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
8.
Investigation on Transition of Laminar-turbulent in a Boundary Layer on a Flat Plate Based on the Spatial Model;
基于空间模式的平板边界层层流到湍流转捩的研究
9.
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
10.
Numerical Simulation and Control of Separated Transition Flows in High-lift Low-pressure Gas Turbine Cascade
低压高负荷燃气透平叶片边界层分离转捩数值模拟与流动控制
11.
LARGE-EDDY SIMULATION OF LAMINAR SEPARATION BUBBLE TRANSITION UNDER ADVERSE PRESSURE GRADIENT
逆压梯度下层流分离泡转捩的大涡模拟
12.
boundary -layer air
附面层[边界层]空气
13.
Transition Control Experiment Based on Linear Stability Theory
基于线性稳定性理论的转捩控制试验
14.
Numerical Investigation on a Transition Prediction Model
关于一个新型转捩模式的研究与应用
15.
An analysis of transition coherent structuresin convective Mach Number 0.4 compressible free shear flow
可压缩自由剪切流混合转捩大涡模拟
16.
Attack of angle effect for supersonic blunt cone transition flow
超声速小攻角下的圆锥转捩攻角效应
17.
Prandtl's boundary-layer approximation
普兰特尔边界层近似法
18.
incompressible boundary layer
不可压缩流体边界层