turbulent separation
英 [ˈtɜːbjələnt ˌsepəˈreɪʃn]
美 [ˈtɜːrbjələnt ˌsepəˈreɪʃn]
网络 湍流界层分离; 湍林离; 湍流分离
双语例句
- Turbulent boundary layer separation, reattachment and redevelopment over a back ward-facing step
湍流，激流，射流后向台阶湍流边界层分离、再附及发展 - A Two-phase Turbulent Flow Model for Suspended Sediment Transport under Waves; Studies on Microfluidic Chip-Based Liquid-Liquid Extraction and Multiphase Laminar Flow Separation Techniques
基于固液两相紊流理论的近岸悬移质泥沙运动数值研究微流控芯片液-液萃取和多相层流技术的研究 - Large Eddy Simulation of Turbulent Statistical and Transport Properties in Stably Stratified Flows LARGE-EDDY SIMULATION OF LAMINAR SEPARATION BUBBLE TRANSITION UNDER ADVERSE PRESSURE GRADIENT
稳定分层流动中湍流统计特性和输运特性的数值研究逆压梯度下层流分离泡转捩的大涡模拟 - Experimental investigation on the turbulent coherent structures of laminar separation flow over a backward-facing step
后向台阶层流分离湍流结构的实验研究 - LDV measurement of a turbulent separation-reattachment flow
激光测速测量湍流分离-再附流动 - Design and Adjustment of a Hydrodynamic Model of Turbulent Flow Separation Area for In Vitro Experiment on the Downstream of Tubal Stenosis
圆管狭窄下游湍流场流动分离区流体力学实验模型的设计和调试 - By using the Baldwin-Lomax turbulent model, the formation of the leading edge separation bubble, as well as the convection of vortex along the airfoil surface and unsteady phenomena of vortex are simulated at high angle of attack.
应用BaldwinLomax湍流二层代数模型模拟了大攻角时前缘分离涡的形成，旋涡对流及其非定常现象。 - Step induced hypersonic turbulent boundary-layer separation
表面台阶引起的高超声速湍流边界层分离 - The Effect of Modelling the Turbulent Stresses on Prediction of the Behavior of 3-D Boundary Layer with separation
湍流应力模式对计算有分离三维边界层的效果研究 - Measurement and prediction of internal 2-D turbulent boundary layer separation
测量与预测二维不可压湍流附面层分离 - The characteristics of an axisymmetric turbulent boundary layer near separation
轴对称湍流边界层接近分离时的特性 - The incipient separation induced by shock wave/ turbulent boundary layer interactions at sharp fin was studied and a method for predicting the incipient separation was developed based on the compressible boundary layer theory.
本文对由平板上直立尖劈产生的激波/湍流边界层干扰引起的起始分离进行了研究，提出了一种预测起始分离条件的方法。 - Numerical and Experimental Study on Turbulent Boundary-Layer Separation in a 2-D Internal Channel
二元内流通道内湍流附面层分离的数值与实验研究 - A predicting method of wing turbulent separation area and the influence of different turbulent models on the results of prediction are introduced.
介绍了机翼气流分离区的预测方法和不同湍流模型对其预测结果的影响。 - A new quasi-simultaneous viscous/ inviscid interaction model was used to predict two-dimensional incompressible turbulent boundary-layer separation flows in internal chan-nels.
本文采用适合于内流的准同时粘性/无粘性流匹配模型，快速求解二维通道内的不可压湍流附面层分离流动。 - Experimental study of turbulent boundary-layer separation in a 2-D channel flow
二维通道内湍流边界层分离的实验研究 - Finally recent studies of turbulent boundary layer separation are also briefly reviewed.
最后简单介绍了目前在研究湍流边界层分离方面的进展。 - It provides qualitative information mainly concerning the overall flow structure, such as the turbulent boundary layer separation, reattachment locations and the dimensionalities of the flow.
它主要提供关于整个流动的定性信息，诸如湍流边界层分离、再附着位置以及流动的维数等。 - A second filtering was applied to the convective and turbulent stress terms, and a new separation of the turbulent stresses was proposed.
对对流项和湍流应力项进行二次显式滤波，并对湍流应力的分解形式作了相应改进。 - Turbulent separation features induced by blunt fins in hypersonic flow
钝缘舵高超音速湍流分离特性 - A three-dimensional oil-water 2-phase turbulent flow and separation process in a single-cone hydrocyclone is numerically simulated using FLUENT software.
使用FLUENT软件中的多相流欧拉分析方法，结合雷诺应力湍流模型，实现单锥型旋流器内油水分离过程的三维数值模拟并预测其分离效率。 - Numerical simulation of liquid-liquid turbulent separation flows in a double-cone hydrocyclone
双锥型旋流器内液&液分离过程的流动数值模拟 - Calculation of compressible turbulent boundary layers with separation
可压缩紊流分离边界层的计算 - Experimental studies and numerical simulations are used to analyze the strongly turbulent flow field and the gas-solid separation characteristic in this thesis.
本文利用试验和数值模拟两种途径分析了不同结构及操作条件旋风分离器内强旋流场以及气固两相分离特性。 - Turbulent separation occurs on pressure surface at small attack angles for the airfoils which relative thickness more than 40%, making airfoil stall at small attack angles and the lift coefficient decrease.
通过CFD模拟发现，具有后加载造型、相对厚度大于40%的翼型压力面出现明显分离，造成翼型小攻角失速、升力系数下降。