airfoils
美 [?er?f??l] 
英 [?e?(r)?f??l]
- na.【航】機(jī)翼；翼形
- 網(wǎng)絡(luò)翼型；翼狀物；機(jī)翼剖面
詞形變化
復(fù)數(shù)：airfoils
英漢解釋
英英解釋
例句
Sails are airfoils that work by using an airflow set up by the wind and the motion of the boat.
帆是翼型的工作使用氣流所設(shè)立風(fēng)和運(yùn)動(dòng)船。
Next, experimental investigations were completed in the wind tunnel on some modified airfoils with air jet.
其次進(jìn)行了對(duì)某翼型被動(dòng)噴氣改型的風(fēng)洞試驗(yàn)研究。
an assembly of rotating airfoils; horizontal rotors on a helicopter or compressor rotors of a jet engine.
旋轉(zhuǎn)螺旋槳的集合；直升飛機(jī)上是水平旋轉(zhuǎn)物，噴氣式飛機(jī)上是壓縮旋轉(zhuǎn)物。
The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down.
尾流測(cè)量不能用來(lái)測(cè)量失連狀態(tài)下的冀型或襟翼偏轉(zhuǎn)后的翼型阻力。
Fairly ideal airfoils were obtained. This method of airfoil design has been validated to be operational and applicable by CFD simulation.
通過(guò)CFD流場(chǎng)檢驗(yàn)驗(yàn)證了這種葉片造型方法的可操作性和適用性。
It has been applied to the design of compressor blades of some micro-engines, and fairly ideal airfoils are obtained.
通過(guò)在微小型發(fā)動(dòng)機(jī)壓氣機(jī)葉片設(shè)計(jì)中的應(yīng)用，得到了比較理想的葉片。
For steady incompressible flows, the effects of Reynolds number and thickness of airfoils on the aerodynamic characteristics are studied.
研究了在二維定常不可壓流動(dòng)狀態(tài)下雷諾數(shù)和翼型厚度等參數(shù)對(duì)翼型氣動(dòng)特性的影響。
Its comprehensive coverage focuses on drag, turbulent flow, and vibration reduction in airfoils .
它的廣泛報(bào)導(dǎo)集中在機(jī)翼阻力、湍流和振動(dòng)減少。
All airfoils in this series will have four segments - the minimum number of segment.
所有翼型這四個(gè)環(huán)節(jié)將有一系列的最少數(shù)量部分。
The computational result shows that both the design of airfoils and the location of installation are reasonable.
計(jì)算結(jié)果表明，本算例中導(dǎo)流體的葉型設(shè)計(jì)和安裝位置是合理的。
An embedded H grid technique is employed for generating grids of isolated airfoils and cascades.
提出一種嵌入式H型網(wǎng)格技術(shù)，用于生成孤立翼型和葉柵的計(jì)算網(wǎng)格。
Several example airfoils will be presented in these notes to illustrate the design method.
翼型將在幾個(gè)例子來(lái)說(shuō)明這些紙幣的設(shè)計(jì)方法。
Supersonic Channel Airfoils for Reduced Drag.
減小阻力的超音速波道翼型。
Flexible material is used as substrate of balloon actuators to enable them to bend easily and be mounted on various surfaces of airfoils.
使用柔性材料作為基底，器件可彎曲變形，便于安裝在翼型表面；
Predicting Glaze or Rime Ice Growth on Airfoils.
預(yù)報(bào)機(jī)翼面上堅(jiān)冰或毛冰的生長(zhǎng)。
Up to this point our discussion has centered on theory of lift and the shape of airfoils best
至于此點(diǎn)，我們的討論集中于抬升理論及最適合直升機(jī)的旋轉(zhuǎn)翼的機(jī)翼形狀
Nonequilibrium algebraic turbulence modeling considerations for transonic airfoils and wings
用于跨音速翼型和機(jī)翼的不平衡代數(shù)紊流模型的研究
The Experimental Study on the Performances of a New Kind of Double-head Anti-symmetric Airfoils
新型雙頭反向對(duì)稱(chēng)翼型的性能實(shí)驗(yàn)研究
The Experimental Study on the Performances of a New Kind of Double-head Airfoils
新型雙頭翼型的性能實(shí)驗(yàn)研究
Numerical simulation of oscillating excitation separation flow control over airfoils
振蕩射流控制翼型流動(dòng)分離的數(shù)值模擬
Solution of the Euler Equations with Approximate Boundary Conditions for Thin Airfoils
翼型采用近似邊界條件的歐拉方程數(shù)值解
Numerical investigation of dynamic stall vortex movement of different-thickness airfoils
不同厚度翼型動(dòng)態(tài)失速渦運(yùn)動(dòng)數(shù)值研究
Multi-point aerodynamic design optimization for compressor cascade airfoils
壓氣機(jī)葉柵多點(diǎn)氣動(dòng)優(yōu)化設(shè)計(jì)
On Comparing Flutter Characteristics of Three Supercritical Airfoils in Transonic Flow
超臨界翼型的跨聲速顫振特性研究
Efficient simulation of incompressible viscous flow over single and multi-element airfoils
有效模擬單段與多段翼型不可壓縮粘性繞流
Incremental Harmonic Balance Method for Strongly Nonlinear Flutter of Airfoils
強(qiáng)非線性顫振分析的增量諧波平衡法
Computation of the flow past multi-element airfoils using unstructured grid and N-S equations
非結(jié)構(gòu)網(wǎng)格上N-S方程解法研究及在多段翼型繞流中的應(yīng)用
Standard Specification for Stainless Steel Bars for Compressor and Turbine Airfoils
渦輪螺旋槳和壓縮機(jī)用不銹鋼棒材規(guī)范
Aerodynamic characteristics of flapping airfoils at low reynolds number
撲動(dòng)翼型的低雷諾數(shù)氣動(dòng)特性分析
Unsteady N-S Calculations Using a Dual-Time Stepping Method for Airfoils Oscillating at High Angle of Attack
雙時(shí)間法求解大迎角翼型繞流非定常N-S方程
Study on Performance of the New Type Controlled Diffusion Airfoils
新型控制擴(kuò)散翼特性研究
Analysis on aerodynamic performance of complex iced airfoils
復(fù)雜積冰翼型氣動(dòng)性能分析
a somewhat improved method for analyzing multi - element airfoils
多段翼型的一種分析方法
The Low Reynolds Number Effects on the Performance of Some Controlled Diffusion Airfoils
低雷諾數(shù)效應(yīng)對(duì)某可控擴(kuò)散葉型性能的影響
Computation of Flow around Isolated Airfoils with Embedded H-Grid
應(yīng)用嵌入式H型網(wǎng)格技術(shù)計(jì)算孤立翼型繞流場(chǎng)
Optimum aerodynamic design of transonic airfoils based on response surface methodology
基于響應(yīng)面法的跨聲速翼型氣動(dòng)優(yōu)化設(shè)計(jì)
Two-dimensional transonic flow past airfoils
繞翼型的二維跨聲速流
Navier-Stokes analysis of blunt trailing edge airfoils
鈍后緣翼型的納維爾-斯托克斯分析
Numerical Simulation of Ice Accretion on Airfoils
飛機(jī)機(jī)翼結(jié)冰過(guò)程的數(shù)值模擬
Aerodynamic Design of Airfoils Based on Variable-Domain Variational Finite Element Method
基于變域變分有限元的翼型氣動(dòng)設(shè)計(jì)
