separated flow信息详情
[流]分离流;独立水流
separated───v.分开;隔开(separate的过去式和过去分词);adj.分开的;分居;不在一起生活的
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)
sharply separated───急剧分离
get separated───分开;分散
separated from───隔离,分离
separated into───把…分成,分离成
separated shoulder───分离式路肩
be separated───被拆开(separated是separate的过去分词);被分离(separated是separate的过去分词);暌离;仳离
legally separated───合法分居
A vortex panel method is presented to simulate low speed inviscid separated flow past an airfoil with a spoiler.───本文介绍用涡面元法模拟带扰流片的翼型低速无粘分离绕流。
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.───对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
there is no separated flow and closed streamline in porous media region near the sudden-changed cross-section.───截面附近的渗流区域中不存在回流和分离流,也不存在封闭的流线。
Separated flow can be efficiently controlled by the flow control technique of using co-flow jets.───采用边界层流动控制能够有效抑制扩压叶栅的流动分离。
The separated flow can be suppressed when the voltage amplitude and duty cycle reach their threshold values.───电压幅值和占空比必须达到一定的阈值才能有效抑制流动分离;
It is shown that there exist three types of separated flow structure for different pitching rate.───揭示了在不同的翼型转动角速度范围内,存在三种分离流结构。
The splitter vanes (14) serve to minimize or eliminate regions of reverse or separated flow, resulting in improved compressor performance.───分流叶片(14)用来尽量减小或消除反向或分离流动区,从而导致改善的压缩机性能。
A Comparison of Two Turbulence Models on Computation of Three-Dimensional Separated Flow Around a Prolate Spheroid───两种湍流模式对绕椭球体三维分离流计算的比较
Numerical Research on Separated Flow Around a WIG Craft in Flight Close to Ground at High Incidence Angle───地效飞行器大迎角近地面飞行分离流动数值研究
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
A model of vapor-liquid two-phase cocurrent separated flow, for the first time, is established for saturated flow boiling heat transfer in a vertical narrow rectangular channel in this paper.
The maximum lift coefficient could be raised by 30%. It has been shown that moving surface is an excellent technique to control separated flow over the strake wing.
In many experiments, the entry geometry has involved sharp edges or corners and there was probably a region of separated flow.
Separated flow around after - body of automobile is numerically calculated and studied.
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