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boundary-layer interaction中文什么意思

發(fā)音:   用"boundary-layer interaction"造句
  • 附面層相互作用
  • boundary:    n. 邊界,疆界,限界 (between);(球場(chǎng))邊線 ...
  • layer:    n. 1.放置者,鋪設(shè)者,計(jì)劃者。 2.【賽馬】(一般) ...
  • interaction:    n. 1.相互作用,相互影響,互動(dòng)。 2.【航空】干擾。 ...
  • interaction involving boundary layer:    附面層相互作用
  • boundary layer:    【物理學(xué)】邊界層。
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例句與用法

  1. Nonlinear turbulence models in shock boundary - layer interaction
    邊界層相互作用的非線性湍流模式
  2. Numerical simulation of two - dimensional shock boundary - layer interaction between a rocket and booster
    助推器附近二維激波邊界層干擾的數(shù)值分析
  3. The computed results compared favorably with measurements and the corresponding shock boundary - layer interaction and energy loose during transonic speed was described
    以尋找出葉片對(duì)能量轉(zhuǎn)換過(guò)程中,因氣動(dòng)力原因而造成能量損失的原因,進(jìn)而提供改良建議。
  4. In this study , the transonic shock - wave / boundary - layer interaction and viscous shear stress for the turbine and compressor stator were simulated used the implicit two - factor flux - splitting schemes for solving the thin - layer compressible flow
    除驗(yàn)證各式正確性外并仿真葉片外形對(duì)氣流分離、震波/邊界層相互干擾及壓縮比等關(guān)系,以及流體黏滯性等影響下,引擎能量損失與效益分析。
  5. In this study , the transonic shock - wave / boundary - layer interaction and viscous shear stress for the turbine and compressor stator were simulated used the implicit two - factor flux - splitting schemes for solving the thin - layer compressible flow
    除驗(yàn)證各式正確性外并模擬葉片外形對(duì)氣流分離、震波/邊界層相互干擾及壓縮比等關(guān)系,以及流體黏滯性等影響下,引擎能量損失與效益分析。

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