翼型

基本解释 (translations)

aerofoil

词组短语

airfoil profile · airfoil section · airfoil shape · wing section · wing profile

与翼型相关的网络例句 [注：此内容来源于网络，仅供参考]

The inverse method was used in aerofoil of fan blade design, a nonlinear algorithm of velocity distribution optimization, different optimize methods was introduced ,according to the difference of suction and pressure surface, this technique can adjust the thickness of aerofoil available.

使用反方法进行风机叶片的翼型设计，采用了一种非线性优化速度分布的方法，分别针对吸、压力面的初始速度分布采用不同的优化手段，可以有效地调节翼型的厚度。

According to the difficulties of designing and molding aerofoil blades, a application program which can be used to exactly draw profile curve of blade section is developed with VBA, which is based on the analysis of calculation method for designing and molding aerofoil blades and adopts OLE provided by CAD software SolidWorks.

在分析翼型叶片造型计算方法的基础上，针对翼型叶片造型的难点，利用三维 CAD 软件 SolidWorks 提供的 OLE 应用编程接口，使用 VBA 开发了准确绘制叶片截面轮廓曲线的应用程序，并给出了叶轮三维建模的方法和步骤。

In the airfoil design for potential flow using conformal mapping technique, the metric coefficient was written as the analytical form.

在应用保角转绘技术的位流翼型设计中，研究了保角转绘网格中度规系数的解析表达；推导了将保角转绘模还原为翼型坐标的计算公式，而且将AF3算法用于位流方程的伴随方程的求解中，并在位流翼型的设计中得到了验证。

It is found that the wing crack extend along a curved path and gradually approximate to the line which passes the middle point of the main crack and is parallel to the direction of maximum principal stress.

采用数值和试验的方法对翼型裂纹的扩展路径进行分析，发现单轴下张开型裂纹的翼型裂纹的扩展路径逼近于过原主裂纹中心点、平行于最大主应力的一条直线。

In the equation, the unknown parameters are determined by the crack initiation angle, the crack length and the angle between the direction of the maximum principal stress and the crack surface.

采用双曲线翼型裂纹路径和试验中所得翼型裂纹路径进行了对比分析，二者吻合得很好，验证了采用双曲线近似表示真实存在的翼型裂纹模型的正确性。

Airfoil profiles for wind turbines are mostly chosen from aviatic ones,but design requirements between the two types are different in many aspect.

风力机翼型主要选自航空翼型，但风力机翼型与航空翼型的设计要求存在许多的不同之处，所以，基于初始航空翼型以获得适合风力机的翼型的优化设计工作就显得十分重要。

The land vehicle that is defined in claim 11, wherein said airfoil system includes at least three substantially vertical airfoils, said one airfoil being located essentially in a vertical plane containing the longitudinal axis of the vehicle, and the other two vertical airfoils being located at generally parallel relation to said one airfoil on opposite sides thereof rearwardly of the center of gravity of the vehicle.

土地车辆是指在索赔11 ，其中说，翼型系统，其中至少有三个大大的垂直翼型说，一翼型位于基本上是在一个垂直平面载有纵向轴的车辆，和其他两个垂直翼型正位于普遍平行的关系说，一翼型对对立面存在的rearwardly该中心的重心的车辆。

A wind- and motor-powered land vehicle with a fore-and-aft longitudinal axis comprising a body supported by wheels, at least one of said wheels fixed to rotate in a plane parallel to the fore-and-aft axis of said vehicle, an airfoil system comprised of two vertically extending airfoils rigidly mounted on said body in an arrangement having bilateral symmetry about a vertical plane through said fore-and-aft axis, said airfoil system providing a forward propelling force of said vehicle when the airfoil system is subjected to certain cross wind conditions, and self-contained motor propulsion means on said vehicle for providing acceleration from a stationary position and for propelling the vehicle either independently or in combination with propelling forces generated by wind action on said airfoil system, each airfoil having a plurality of airfoil sections telescopically fitted together, the lower airfoil section being rigidly mounted in fixed relationship to said body, said airfoil system including a retracting mechanism for lowering upper airfoil sections of said airfoil system when desired and for subsequently extending said airfoil system, said retracting mechanism including a plurality of linkages interconnecting said sections and an actuator means operatively connected between said body and to said linkages for lowering and extending each airfoil, and an intermediate airfoil extending between the upper sections of each of said airfoils so as to provide an inverted U-shaped airfoil.

风力和电动机驱动的陆地车辆与前列和尾部长轴组成的一个机构的支持，车轮，至少有一说，车轮固定在一个旋转平面平行的前列和前后轴的说，车辆，翼型系统组成的两个垂直扩展翼型硬性安装在说，机构在安排后，双边对称约一垂直面说，通过国内外和前后轴，表示翼型系统提供了一个向前推进的力量说，车辆时，翼型系统是受到某些横风条件下，和自我载电机推进的手段就表示，车辆提供加速从一个固定的立场和为推进车辆单独或结合，与推进力量所产生的风的行动表示翼型系统，每个机翼有一个多元化翼型第telescopically装在一起，较低的翼型节被硬性安装在固定的关系，说身体，说翼型系统包括一个撤消的机制，降低上翼型章节说，翼型系统时，理想的和其后再将说，翼型制度，说收回机制包括多元化的联系互连说，部分和一个致动器的手段手术之间的连接说，身体和说，联系降低，并延长每翼型，及一个中间翼型延长之间的路段上的每说翼型，以便提供一个倒U -形翼型。

One type of blade airfoil with high efficiency of a general axial flow fan is adopted as original airfoil, and it is shortened according to different length scale, and then joined to the exportation circular arc of the original airfoil in the opposite direction. Assuring the streamline on the surface of the blade profile after smooth operation, a new kind of double-head anti-unsymmetrical S model airfoils has been structured to be researched in this paper.

采用一种效率比较高的普通风机叶片翼型作为原始翼型，按不同长度比例缩小原始翼型，反向搭接在原始翼型的出口圆弧处，经过光滑处理，保证叶型表面的流线形后，构成本文所研究的新型双头双机翼反向S型不对称翼型。

In the icing research,we construct three different ice shapes: sharp-angled ice,blunt nosed ice and double horn ice.

对翼型结冰问题，在结冰条件下，利用数值方法分析研究翼型和多段翼型绕流流场及气动特性的影响。

与翼型相关的网络解释 [注：此内容来源于网络，仅供参考]

aerofoil：翼型

aerial view 鸟瞰图 | aerofoil 翼型 | aerosol 悬浮微粒;喷雾

aerofoil contour：翼型, 机翼断面

light barium flint 轻钡火石玻璃 | aerofoil contour 翼型, 机翼断面 | unclaimed luggage 无人认领的行李

aerofoil section：翼型截面

aerofoil fan 轴流式通风机 | aerofoil section 翼型截面 | aerofoil 风板

aerofoil theory：翼型理论, 机翼理论

aerofoil strut | 机翼支柱 | aerofoil theory | 翼型理论, 机翼理论 | aerogams | 显花植物

airfoil：翼型

blunt body 钝体 | airfoil 翼型 | chord 翼弦

airfoil section：翼型剖面

飞翼船 airfoil boat | 翼型剖面 airfoil section | 充气,通气,空气干燥法 airing

airfoil profile：翼型, 翼剖面

airfoil lift | 机翼升力, 翼型升力 | airfoil profile | 翼型, 翼剖面 | airfoil section | 翼剖面

aliform type：翼型

aliform parenchyma | 翼状薄壁组织 | aliform type | 翼型 | aliform | 翼状的, 有翼状物的

Thick cambered airfoils：厚弧面翼型

Kutta-Joukowski theorem, 库塔-儒科夫斯基定理 | thick cambered airfoils, 厚弧面翼型 | thin-airfoils, 薄翼型

supersonic airfoils and：超音速翼型

Prandtl-Meyer perfect--gas function, 普朗特-麦耶理想气体函数 | supersonic airfoils and. 超音速翼型, | thin-airfoil theory, 薄翼型理论