可压缩紊流的英文
发音:
"可压缩紊流"怎么读用"可压缩紊流"造句
英文翻译手机版
- compressible turbulence
- "可"英文翻译 approve
- "压缩"英文翻译 compress; condense; reduce; ...
- "紊"英文翻译 disorderly; confused
- "不可压缩紊流" 英文翻译 : incompressible turbulence
- "可压缩性紊流" 英文翻译 : compressible turbulence
- "可压缩" 英文翻译 : coercible gas; compressible
- "不可压缩" 英文翻译 : [物理学] incompressible◇不可压缩边界层 incompressible boundary layer; 不可压缩流动 incompressible flow; 不可压缩流体 incompressible fluid; 不可压缩射流 incompressible jet; 不可压缩性 incompressibility; incoercibility; inflexibility
- "不可压缩层" 英文翻译 : incompressible stratum
- "不可压缩场" 英文翻译 : incompressible field
- "不可压缩的" 英文翻译 : incoercible; incompre ible; incompressible; non-compressible; uncompressible; unyielding
- "不可压缩铃" 英文翻译 : incompre ible fluid; incompressible fluid
- "不可压缩流" 英文翻译 : incompre ible flow; incompressible flow
- "不可压缩性" 英文翻译 : incoercibility; incomprassibility; incompre ibility; incompressibility; inflexibility; rigidity
- "可压缩波导" 英文翻译 : squeezable wave-guide
- "可压缩参数" 英文翻译 : compre ible parameter; compressible parameter
- "可压缩层" 英文翻译 : compressible stratum
- "可压缩层段" 英文翻译 : compactible interval
- "可压缩的" 英文翻译 : compre ible; compressible; condensable; condensible; squeezable
- "可压缩隔垫" 英文翻译 : collapsible spacer
- "可压缩介质" 英文翻译 : compressible medium; compressiblemedium
- "可压缩铃" 英文翻译 : compre ible fluid; compressible fluid
- "可压缩流" 英文翻译 : compre ible flow; compressible flow
- "可压缩流体" 英文翻译 : compre ible fluid; compressible fluid; compressiblefluid
- "可压缩气流" 英文翻译 : compressible airflow
- "可压缩气体" 英文翻译 : coercible gas
例句与用法
- The blade inner channel cooling is a complex convection - conduction coupling problem . this thesis build a three - dimension . compressible turbulence model , and give a general solve method . with the geometrical model of the glossily rectangle straight channel , the rectangle straight channel with in - line arrays disturb plates , the rectangle straight channel with staggered arrays disturb plates , the rectangle straight channel with slant disturb plates , this thesis compute the flow and heat transfer condition when the cold air path though these channels , and gain the temperature field , pressure field , velocity filed , in addition . this thesis also analyze the influence of the different channel height , the different channel materials , the different channels , and gain the function relation between he nusselt number , friction factor and reynolds number . this thesis is emphasis on the new heat transfer enhancement structure , that is , disturb plates , with the comparison with the glossily channel and channel with pin fins , the heat transfer enhancement effect of the former is better , and the conclusion can be used in the design of aircraft blade
叶片内部通道冷却是一个复杂的对流?导热耦合传热问题,本文在分析叶片内部通道冷却的流动与传热情况的基础上,建立了三维、可压缩紊流的物理模型,得到了通用的求解办法;利用不带扰流片的矩形直通道、带顺排扰流片矩形直通道、带叉排扰流片、带倾斜扰流片的矩形直通道的几何模型,计算了冷却空气通过这几种通道时的流动与换热情况,得到了各种不同情况下计算区域的温度场、压力场、速度场;在此基础上分析了不同的通道高度、不同的叶片通道材质对叶片内部通道冷却的影响,并整理得到了各种通道形式下,努谢尔数和阻力因子与雷诺数的函数关系;本文重点研究了新型的叶片内部通道冷却强化传热措施?带扰流片的内部冷却通道的强化传热效果,通过与光滑矩形直通道、带针肋通道的冷却效果的比较,表明了这种新型鲒构的优势,对于叶片内部通道冷却结构的设计可以起到指导的作用。
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