supersonic flow发音

意思翻译

[流]超音速流动

相似词语短语

flow───vi.流; 垂; 流出; （谈话、文体等）流畅；n.流动；生产，供应；车流；流量；传播；流通；滔滔不绝；连贯，流畅；涨潮；泛滥；（苏格兰）湿地，沼泽；月经；vt.使泛滥; 淹没; 排出；n.流动; 滔滔不绝; 涨潮; 连贯；v.（使）流动，涌流；流通；传播；流畅；充满；大量供应；涨；涨潮；川流不息；飘扬；来自，由……产生；来月经；（矿物、岩石等）变形；n.(Flow)（美）弗洛（人名）

ceaseless flow───源源不断的流动

cohesive flow───粘性流

flow controller───[自]流量控制器

current flow───电流

flow about───流动

flow production───流水线生产；大规模生产

flow diagram───n.流程图，作业图，生产过程图解; 框图；[工业]流程图；作业图

eulerian flow───欧拉流

双语使用场景

We present a method of analyzing flutter characteristics of wing with nonlinear stiffness in supersonic flow.───提出了带结构刚度非线性的超音速弹翼的颤振分析方法。

A numerical method of computing steady supersonic flow fields by using adaptive streamline grids.───提出一个用自适应流线网格计算定常超声速流场的数值方法。

experimental Study of a two dimensional inlet model in non-uniform supersonic flow are presented.───介绍一种二元进气道模型在非均匀超音来流中的初步研究结果。

At last the mechanism of secondary breakup of the liquid droplets in the supersonic flow was researched into.───初步分析了超声速下液滴二次破碎的特性和机理。

A method has been presented for calculating the aerodynamic characteristics of grid fin in subsonic and supersonic flow.───本文提出了计算栅格翼亚、超音速气动特性的计算方法。

To reveal the mechanisms of the mixing enhancement in supersonic flow, the work studied the basal free shear mixing layer at first.───针对超声速流动混合增强机理，从最基本的自由剪切混合层入手，研究了混合层的发展过程。

Nonlinear dynamic behaviors of heated panels in supersonic flow were studied.───研究了超音速气流中受热壁板的非线性动力学行为。

Supersonic flow characteristics of grid fins are analysed.───详细分析了栅格翼在超音速情况下的流场特性。

英语使用场景

Covers the basics - grid generation, numerics, incompressible flow and supersonic flow.

The time averaged velocities in fluid flow can be measured simply and conveniently by investigating the effect of the pitot tube in supersonic flow.

In supersonic flow, results indicate that the disintegration of the jet column is caused by the surface waves induced by aerodynamic forces and the breakup point is at the wave trough.

Based on the piston theory of supersonic flow, the second lagrange equation is used to set up the dynamic equations of an airfoil with store in the supersonic or hypersonic flow.

Rarefaction effect on supersonic flow fields in the transition from near continuum to near free-molecule flow is analyzed numerically.

To prevent the engine structure from melting because of air friction from the supersonic flow, engineers use "active cooling" schemes.