为什么理会翼型？
These two airfoils lie on different Riemann sheets in the hodograph plane.
该两个翼型处在不同的黎曼面内。
All airfoils in this series will have four segments - the minimum number of segment.
所有翼型这四个环节将有一系列的最少数量部分。
Of course, for more complex airfoils (more practical designs) more parameters are needed.
当然，对于较复杂的翼型(更为实用设计)需要更多的参数。
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气流所设立风和运动船。
Low reflection, mid reflection and high reflection could be classified for the above 8 airfoils.
可以将上面8个翼型分为低反射，中反射和高反射三大类。
Bifurcations of airfoils with nonlinear pitching stiffness in incompressible flow are investigated.
本文分析了不可压气流中带有非线性俯仰刚度二元机翼的分叉问题。
An alternative approach is to fix the geometry and change the transformation to get different airfoils.
另一种方法是把几何学得到改造，改变翼型不同。
An arbitrary airfoils blade design procedure was adopted to redesign a transonic fan with compound swept.
采用任意中弧线叶片造型程序，将某单级跨声、常规设计的风扇改进为复合掠形设计。
Next, experimental investigations were completed in the wind tunnel on some modified airfoils with air jet.
其次进行了对某翼型被动喷气改型的风洞试验研究。
Airfoils pressure distribution has been computed by this method and is in good agreement with independent r...
采用这种方法计算所得的位流压力分布与用其它方法求得的压力分布非常吻合。
Airfoils pressure distribution has been computed by this method and is in good agreement with independent results.
采用这种方法计算所得的位流压力分布与用其它方法求得的压力分布非常吻合。
This paper represents a CFD method for the design of NLF airfoils directly under transonic viscous flow conditions.
本文介绍一种设计跨声速自然层流翼型的计算流体力学（CFD）方法。
A new method is presented to calculate the exact analytic solution of potential flow about multi - element airfoils.
本文给出了求解多段翼型位流准确解的一种方法。
Finally, a special form allows the user to prescribe any number of segments so that practical airfoils can be designed.
最后，一种特殊形式允许用户指定任何数目的片段，可以使实际翼型设计。
This method may be used to calculate the arbitrary airfoils with sharp leading edge provided that the shock wave is attached.
在激波附体的条件下，本文的方法可用于计算大迎角尖前缘任意翼型的超音速和高超音速俯仰安定性导数。
The conservative full potential equation and C H grid are used to compute the unsteady transonic flows around airfoils and wings.
采用C-H型网格、守恒型非定常全位势方程的时间精确近似因式分解差分法计算二维、三维的跨声速非定常位势流。
In this paper the Direct Iterative Surface Curvature (DISC) design method is presented for designing airfoils at transonic speeds.
本论文采用直接表面曲率迭代方法(DISC)进行跨声速翼型设计。
A simplified model of wet steam equilibrium flow past cascade of arbitrary airfoils on general surface of revolution is presented.
提出了一个通过任意谈成面叶棚的湿蒸汽平衡态流动的简化模型。
The muscular, tattooed South Carolinian has a prized job with General Electric's (GE) Greenville Airfoils Facility in Piedmont, S.C.
一个南卡罗莱纳州人为拥有一份为人称道的工作，是为在南卡罗莱纳州皮得蒙特(Piedmont)的通用公司格林维尔机翼设备制造厂工作。
A method has been developed which generates the body-fitted coordinates of multi-element airfoils by using of a grid patching technique.
本文给出了一种多段翼型绕流的分区贴体网格生成方法。
For steady incompressible flows, the effects of Reynolds number and thickness of airfoils on the aerodynamic characteristics are studied.
研究了在二维定常不可压流动状态下雷诺数和翼型厚度等参数对翼型气动特性的影响。
The pressure weighted interpolation method on collocated unstructured grid is used for numerical simulation of turbulent flow around airfoils.
利用同位非结构化网格上的压力加权修正算法，对翼型湍流绕流进行了数值分析。
In wind tunnel test, tripping wires or a local surface roughness are often applied to fixing the boundary layer transition on airfoils or wings.
在翼型或机翼的风洞试验中，常用绊线或局部表面粗糙度来固定边界层转捩。
The land vehicle that is defined in claim 12, wherein said airfoil system includes a horizontal airfoil connected to the top of said three airfoils.
土地车辆是指在索赔12 ，其中说，翼型系统包括一个横向翼型连接到顶部的说，三翼型。
The purpose of the comparison between computational and experimental results is aimed at some suggestions on the shapes of airfoils at low Reynolds number.
综合理论分析和实验结论，给出微型飞行器低雷诺数二元翼型选型的初步建议。
High-speed aircraft usually employ thin, low-drag, low-lift airfoils; slow aircraft that carry heavy loads use thicker airfoils with high drag and high lift.
高速飞机通常采用低阻力、低升力的流线型薄翼型，载重量大的低速飞机使用高阻力、高升力的厚翼型。
High-speed aircraft usually employ thin, low-drag, low-lift airfoils; slow aircraft that carry heavy loads use thicker airfoils with high drag and high lift.
高速飞机通常采用低阻力、低升力的流线型薄翼型，载重量大的低速飞机使用高阻力、高升力的厚翼型。
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