supersonic flow的意思

supersonic flow中文翻譯：

[流]超音速流動

相似詞語短語

flow───vi.流; 垂; 流出; （談話、文體等）流暢；n.流動；生產，供應；車流；流量；傳播；流通；滔滔不絕；連貫，流暢；漲潮；泛濫；（蘇格蘭）濕地，沼澤；月經；vt.使泛濫; 淹沒; 排出；n.流動; 滔滔不絕; 漲潮; 連貫；v.（使）流動，涌流；流通；傳播；流暢；充滿；大量供應；漲；漲潮；川流不息；飄揚；來自，由……產生；來月經；（礦物、巖石等）變形；n.(Flow)（美）弗洛（人名）

ceaseless flow───源源不斷的流動

cohesive flow───粘性流

flow controller───[自]流量控制器

current flow───電流

flow about───流動

flow production───流水線生產；大規模生產

flow diagram───n.流程圖，作業圖，生產過程圖解; 框圖；[工業]流程圖；作業圖

eulerian flow───歐拉流

雙語使用場景

We present a method of analyzing flutter characteristics of wing with nonlinear stiffness in supersonic flow.───提出了帶結構剛度非線性的超音速彈翼的顫振分析方法。

A numerical method of computing steady supersonic flow fields by using adaptive streamline grids.───提出一個用自適應流線網格計算定常超聲速流場的數值方法。

experimental Study of a two dimensional inlet model in non-uniform supersonic flow are presented.───介紹一種二元進氣道模型在非均勻超音來流中的初步研究結果。

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

A method has been presented for calculating the aerodynamic characteristics of grid fin in subsonic and supersonic flow.───本文提出了計算柵格翼亞、超音速氣動特性的計算方法。

To reveal the mechanisms of the mixing enhancement in supersonic flow, the work studied the basal free shear mixing layer at first.───針對超聲速流動混合增強機理，從最基本的自由剪切混合層入手，研究了混合層的發展過程。

Nonlinear dynamic behaviors of heated panels in supersonic flow were studied.───研究了超音速氣流中受熱壁板的非線性動力學行為。

Supersonic flow characteristics of grid fins are analysed.───詳細分析了柵格翼在超音速情況下的流場特性。

英語使用場景

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.