wing pressure 中文意思是什麼

wing pressure 解釋
機翼壓力
  • wing : n 1 翼，翅膀；鳥；鳥群；飛行，飛翔。2 （飛機）機翼；翼狀物；（汽車的）擋泥板；〈詩常 pl 〉船帆。3...
  • pressure : n 1 壓；按；擠；榨。2 【物理學】壓力，壓強；大氣壓力；電壓。3 精神壓力，政治[經濟、輿論等]壓力。4...
  1. Air regulation systems in mining - wing air locks for travelling tracks - double - wing type doors with pressure reduction

    礦山空氣調節系統.車道用的側翼式空氣門.具有減壓平
  2. The interior temperature distribution and ablation model of projectile wing is established from general transmitting heat differential equation ; at the same time, the heat flow density and pressure distribution model of projectile wing is also established

    從一般形式的導熱微分方程出發，逐步建立了彈翼內部溫度分佈和燒蝕的數學計算模型；與此同時，建立了彈翼表面的熱流密度和壓力分佈的數學模型。
  3. Air regulation systems in mining - wing air doors for haulage tracks - double - wing type doors with pressure reduction

    采礦的空氣調節系統.運輸軌道翼形通氣門.減壓式雙翼
  4. Air regulating systems in mining ; wing air doors for haulage tracks ; double - wing type doors without pressure reduction

    礦山空氣調節系統.運輸線路用空氣風扇門，非減壓雙葉
  5. The farther knowledge has been acquired that pressure - bearing karst water in deep maoba syncline is replenished by the atmospheric water from both east wing and west wing of maoba syncline, but which from east wing is more, and it is impossible that the pressure - bearing karst water from west wing rounds to replenish east wing. 3

    得到進一步的認識；毛壩向斜核部的深部承壓水，同時接受向斜東翼和西翼大氣降水的補給，東翼的補給量相對大些；整個深部承壓水不存在西翼繞過核部補給東翼的可能性； 3
  6. In order to predict hydrodynamic characteristics a computational system is developed including determination of the pressure distribution on a wing section by use of the conformal mapping method and panel method respectively and of the flow in boundary layer according to the thin shear layer approximation ( tsl ) for navier - stokes equation approach. the wing sections of naca4412 and naca0012 are applied to test the computational system. the numerical inspection shows that the panel method with better precision and the momentum and the displacement thickness of boundary layer can be used to complete this calculation

    本文分別用守屋的保角變換法和基於源匯渦分佈的面元法，建立了計算槳葉表面壓力分佈的數學模型；應用納維-斯托克方程的薄層近似理論模式和有限差分數值方法，建立了計算機翼表面邊界層內部流動的數學模型；應用槳葉表面邊界層內部粘性流動和外部勢流流動在邊界上的匹配演算法，建立了槳葉表面二相流流動的計算方法和相應的計算機程序。
  7. Air regulating systems in mining ; wing air doors for travelling tracks ; air doors without pressure reduction

    礦山空氣調節系統.人行道用葉片調風門.非減壓的風扇
  8. Air regulating systems in mining ; wing air doors for haulage tracks ; one - wing type doors without pressure reduction

    礦山空氣調節系統.運輸道用葉片調風門.非減壓的單葉
  9. Lastly, previous vane are analysed by fluent, we calculate the pressure distribution chart and report chart of each wing form, then alter the torsion angle and the airfoil form of the vane respectively, finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power

    最後，通過fluent對設計出的葉片分析，得出其壓力分布圖和報告圖。然後從改變葉片的扭轉角度和翼型兩個方面分析其對升力和阻力的影響。得出葉片的扭轉角和翼型對升阻比的影響曲線，在文章的結尾部分估算了無人機的一些性能參數。
  10. Wing union pressure transmitters model 425 424

    放大輸出壓力傳感器a - 105a型
  11. In order to understand the rotor / wing interaction each other, firstly, the change of the isolate rotor thrust with the collective pitch and rotate speed is tested, secondly, the change of the rotor thrust with the collective pitch, rotate speed and the wing / rotor distance is scaled, when the wing is placed underside the rotor, lastly, the pressure on the wing due to the rotor wake is scaled

    為了搞清楚它們之間的相互影響，本文首先測量孤立旋翼的拉力隨總距和轉速的變化；再測量有機翼時旋翼的拉力隨總距及轉速的變化以及隨旋翼機翼間的距離變化；最後測量旋翼尾流對機翼表面壓力的影響。
  12. Experimental investigation of heat transfer enhancement and pressure drop of some wing - type vortex generators

    幾種翼型渦流發生器強化換熱及流阻性能的實驗研究
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