1.
Direct Numerical Simulation of Spatial Smooth Pipe Flow Transition;
空间发展光滑圆管流动转捩的直接数值模拟
2.
Measurement of Transition Location Change of Swept Wing in a Low-Speed Flow Based on Sublimation Method
后掠机翼低速流动转捩位置的升华法测量
3.
Prediction of transitional flows using an improved low-Reynolds-number turbulence model with transition sensitivity
应用改进的低雷诺数湍流模型预测转捩流动
4.
Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile
大负荷低压涡轮叶型分离转捩流动的大涡模拟
5.
Application of gamma-theta transition model to flows around airfoils
Gamma-Theta转捩模型在绕翼型流动问题中的应用
6.
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
7.
Transitional Flow and Heat Transfer Characteristics in a Rectangular Duct with Stagger-arrayed Short Pin Fins
短小针肋阵列通道内转捩流动与传热性能的实验研究(英文)
8.
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
9.
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
10.
Direct Numerical Simulation Investigation of Gas-Solid Flow Around Square Cylinders;
气固两相绕方柱流转捩的直接数值模拟研究
11.
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
12.
Passive Oxidation Mechanism and Transition Temperature of Silicon Carbide
碳化硅材料被动氧化机理及转捩温度分析
13.
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
14.
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
15.
Inherent Mechanism of Breakdown in Transition & the Eddy Viscosity Model of Periodic Turbulent;
转捩中“breakdown”的内在机理及周期湍流场中的涡粘系数
16.
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。
17.
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
18.
Accurate drag calculation by coupling automatic prediction of transition point to the Navier-Stokes method
NS方程计算中耦合转捩自动判断的阻力精确计算方法初探