该词条未找到_海词词典

您要查找的是不是：

Parallel computation for low mach number flows 低马赫数流动分区并行计算研究
The book is aimed at chemical engineering applications, and consequently it is limited to thermally compressible flows ( low Mach numbers). 书针对化学工程应用，并且从而这热局限于是可压缩的流动(低的马赫数)。
Study on a novel method for low mach number flows computation 低马赫数流动数值模拟方法的研究
THE FOURIER PSEUDOSPECIRAL METHOD FOR FLUID FLOW WITH LOW MACH NUMBER 低Mach数流动的Fourier拟谱方法
Low Diffusion TVD Schemes and Simulation of Low Mach Number Flow in Turbomachinery 低耗散TVD格式及叶轮机内低马赫数流动模拟
Effect of Turning Angle on Flow Field Performance of Linear Bowed Stator in Compressor at Low Mach Number 低马赫数条件下几何折转角对平面扩压叶栅弯叶片流场性能的影响
low Mach number 低马赫数
fluid flow with low Mach number 流体低马赫数流动
Boundary Conditions for Solving Flowfields at Low Mach Numbers by Preconditioning 预处理方法求解低马赫数流场的边界条件
Influence of Mach Number on Tornado Corner Flow Dynamics. 数对龙卷角流动力学的影响。
The main flow is approximately dependent only on Mach number. 主流仍然近似地只同马赫数有关。
It shows the indicated airspeed and the Mach number. 它显示了飞行速度和马赫数。
The method for the unstart Mach number is described. 本文还提出了一种确定不起动马赫数的方法。
And this investigation has predicted the possibility of bending flutter at high subsonic inlet Mach number and low negative incidence. 本研究还预测到在高亚音进口M数,低负攻角条件下出现弯曲颤振的可能。
The investigation indicates that isolator tend to resist higher back pressure and provide exit airflow with better quality under conditions of high mach number and low distortion. 研究结果表明隔离段进口在马赫数高，畸变小的情况下承受反压能力强，流场出口品质好。
An aircraft instrument that indicates speed in Mach numbers. 马赫表装于飞机上的一种以马赫数来显示速度的仪器
Zsoy, E., Rambaud, P., Stitou, A., Riethmuller, M.L., “Vortex Characteristics in Laminar Flow at Low Mach”, Experiments in Fluids, 2005, Vol. 38, p.p. 133-145. 张志伟,“具有上盖平板之空穴内振荡流场之探讨”,中兴大学机械工程研究所硕士论文,1996。
The aerodynamic performances of two typical wind turbineairfoils with different Reynolds number and Mach number was predicted using thesoftware XFOIL, which is a kind of analysis and design software for low Reynoldsnumber airfoil. 论文中详细讨论了计算理论模型，并用低雷诺数翼型分析和设计软件XFOIL分析了两种典型翼型在相同马赫数、不同雷诺数和相同雷诺数、不同马赫数时的气动性能。
On basis of the modeling results, the effects of Mach number, attack angle and ramp angle on the inlet performance are analyzed. 根据此数学模型，分析了攻角和进口气流马赫数对进气道性能的影响，同时给出了斜板对进气道性能的影响。
The profiles of density, velocity, temperature, pressure and Mach number can be obtained by the computation. 通过计算可以得出密度、速度、温度、压力和马赫数的分布。