例句與造句

1. Turbo - compressor rotor
   渦輪壓縮機(jī)轉(zhuǎn)子
2. It was found that the introduce of tip clearance deteriorate the overall performance of the compressor rotor
   數(shù)值結(jié)果表明葉頂間隙的引入惡化了壓氣機(jī)轉(zhuǎn)子的性能。
3. The influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated
   研究了頂部間隙對(duì)壓氣機(jī)轉(zhuǎn)子總性能及內(nèi)部流場(chǎng)的影響。
4. Abstract : a 3d numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance
   文摘:借助于考慮葉片頂部間隙的壓氣機(jī)轉(zhuǎn)子內(nèi)跨音速湍流流場(chǎng)的三維數(shù)值解，得到了該轉(zhuǎn)子流場(chǎng)中的復(fù)雜渦系與波系結(jié)構(gòu)。
5. After describing the scorpath software in detail , it optimizes the compressor rotor profile design and computes the rotor tool profile with the software
   在全面介紹scorpath軟件的基礎(chǔ)上，運(yùn)用該軟件，對(duì)螺桿壓縮機(jī)的轉(zhuǎn)子型線進(jìn)行了優(yōu)化設(shè)計(jì)，同時(shí)計(jì)算了加工轉(zhuǎn)子的刀具廓形。
6. It's difficult to find compressor rotor in a sentence. 用compressor rotor造句挺難的
7. The effects of layout of tip gap clearance on axial compressor rotor performance and stability have been investigated experimentally . a single - stage compressor rotor with no inlet guide vanes was tested under subsonic condition
   本文用實(shí)驗(yàn)的方法對(duì)壓氣機(jī)轉(zhuǎn)子尖部間隙沿軸向周向的布局進(jìn)行了詳細(xì)的研究。
8. Then the effects of the grooved casing treatments on the performance of the compressor rotor have been revealed and some valuable conclusions have been reasoned out
   通過(guò)對(duì)總性能和基元性能，特別是葉片尖部流動(dòng)的詳細(xì)測(cè)量，證明了這種型式的處理機(jī)匣可以提高效率，但在穩(wěn)定裕度上略有損失，并解釋了其影響轉(zhuǎn)子性能的機(jī)理。
9. The calculation of the37 # transonic compressor rotor shows that the simulation results of the author ' s multi - grid scheme fit fairly well with those of professor denton j . d . ' s , however , the author ' s converging speed is faster
   與nasarotor37的計(jì)算結(jié)果對(duì)比表明，本文多重網(wǎng)格算法的計(jì)算結(jié)果與dentonj . d .的計(jì)算結(jié)果十分接近，而在提高計(jì)算效率方面比dentonj . d的多重網(wǎng)格算法更加有效。
10. The effect of leakage flow due to the upstream hub axial gap on the rotor performance and the mechanism of interaction between the hub leakage flow and the rotor blade passage flow were studied based on the numerical simulations of the flow fields of a transonic compressor rotor with upstream hub leakage
    摘要為研究壓氣機(jī)轉(zhuǎn)子上游葉根軸向間隙泄漏流對(duì)轉(zhuǎn)子性能的影響程度以及泄漏流與轉(zhuǎn)子流場(chǎng)之間的相互作用機(jī)制，對(duì)帶有葉根泄漏流的跨聲壓氣機(jī)轉(zhuǎn)子流場(chǎng)進(jìn)行了數(shù)值模擬。