airfoil
The tutorial begins with a simple four-segment airfoil.
补习始于一个简单的四部分机翼.
How does the brake act on the paraglider airfoil?
刹车是如何作用于滑翔伞的翼型?
My seat near the airfoil, Java is over there.
今次坐机翼位，下面是爪哇岛。
Airfoil flutter is one of the important problems in aeroelasticity.
在气动弹性力学中,机翼振颤是一个非常典型的问题。
PATRAN and the process in developing load module of airfoil FEM.
PATRAN进行二次开发程序编制的方法,以及开发机翼有限元模型加载模块的过程,为在msc.
A supporting surface of an airplane; an airfoil or a wing.
机翼:飞机的支撑表面;翼面或机翼。
The vertical airfoil in the tail assembly of an aircraft.
飞机尾部组成部分的垂直机翼。
Rogue Amoeba today announced the release of Airfoil 3.3.
仿生学单细胞虫今天宣布发型了3.3版机翼。
A straight line connecting the leading and trailing edges of an airfoil.
连接机翼的前缘与后缘的直线.
The aerodynamics characteristics of this airfoil is studied in wind tunnel.
进行了翼型的低速气动力性能研究，为附面层特性研究提供了方向。 结果表明，该翼型具有较好的升阻和俯仰特性，但失速特性差。
Lastly, the paper programs to simulate FRP airfoil FW moulding by VC++.
最后，本文用VC++进行编程，从而模拟FRP飞机机翼FW成型整个过程。
Near the midchord, the suction can provide a higher lift force for the airfoil.
吸气孔位置在翼面的中部附近增升效果较好;
Direct methods are based on the design-by-analysis approach in which the airfoil shape is specified first.
直接的方法是基于设计逐案分析的方法是机翼形状指定第一.
Starting with airfoil 2, the pitching moment is increased from -.15 to -.25 to provide more aft loading and aft camber.
从翼型2俯仰时刻由原来的15年至今25年至今,以提供更多后部后部拱落.
Turbulence in air or water caused by the motion or action of an oar, propeller, jet, or airfoil.
涡流由船桨、推进器、喷气机或机翼运动引起的空气或水的涡流
A fixed or movable airfoil used to stabilize an aircraft, a missile, or a projectile in flight.
安定翼，直尾翅用以稳定飞行中的飞机、导弹或发射体的固定式或活动式机翼
Turbulence in air or water caused by the motion or action of an oar,propeller,jet,or airfoil.
涡流由船桨、推进器、喷气机或机翼运动引起的空气或水的涡流
A slightly arched surface, as of a road, a ship's deck, an airfoil, or a snow ski.
弧面稍呈弧形的表面，如路面、船甲板、机翼面或滑雪板
A small auxiliary airfoil that is attached to a larger one and that helps stabilize an aircraft.
调整片，补翼附着在较大的机翼上，用来帮助稳定飞机辅助性的小机翼
Nonlinear Response of Airfoil Section with Control Surface Freeplay to Gust Load.
机翼有控制表面的部分对阵风载荷的非线性响应。
The numerical algorithm is applied for flow over an NACA 0012 airfoil with satisfactory effect.
经对绕NACA0012翼型无粘流动计算的验证，收效明显。
The airfoil shape is then adjusted until the desired velocity distribution is obtained.
然后是调整翼型的形状,直到取得预期的速度分布.
Abstract: An effective aerodynamic optimization design method of transonic airfoil is given.
文摘:提出了一种有效的跨音速翼型气动优化设计方法。
The first one of them is a 2-D model of the NASA GA(W)-1 airfoil section and has been tested as a calibration model.
最初选用的模型是NASA GA(W)-1翼型,并作为校验模型。
In this regard, several airfoil templates are given based on existing designs, eg, the SD7037 airfoil and others.
在这方面,有几个版本,基于现有翼型设计,例如,sd7037翼型等.
In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM).
基于响应面方法进行了跨声速翼型的气动优化设计。
Satisfactory results are obtained by comparison with previous works on the flow field around a two-dimensional airfoil.
整个程式在经过二维机翼流场的数值测试后，得到令人满意的可靠度。
The Web version of the code allows for the prescription of the inviscid velocity distribution about the airfoil.
网上版的代码允许处方粘速度分布的翼型.
It appears that using NLF airfoil section can get a better aerodynamic efficiency and self-starting capability.
实验结果还表明，采用自然层流翼型的斜 轴式风力机比采用普通翼型的斜轴式风力机具有更好的气动效率和起 动能力。
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.
把一些观点方法,它有助于扼要介绍两个一般方式翼型设计.
An effective aerodynamic optimization design method of transonic airfoil is given.
提出了一种有效的跨音速翼型气动优化设计方法。
The flow fields of an airfoil and simplified aircraft are calculated parallelly under MPI/PVM environmcent.
在MPI／PVM环境下用分区方法作了二维翼型和三维机翼绕流的并行计算。
The mathematical transformation is fixed and the airfoil is moved to generate different airfoil geometries.
数学变换是固定机翼的翼型几何移到产生不同.
Two pieces of foam are sandwiched onto the center piece and sanded to an airfoil shape.
两件是泡沫夹心到中心片和磨光的机翼形状。
The second part is about the airfoil analysis and design of two-dimensional inviscid incompressible potential flow.
第二部分是二维无粘不可压势流的 翼型分析和设计问题。
Wu, C. J. &Wang, L., 2003, Adaptive optimal control of the incompressible flow around an airfoil with smart surface, Proceedings of ICFM4, Dalian.
王亮,吴锤结,2003,用智能物面对非定常分离流进行最优自适应控制,《空气动力学新进展论文集》,北京.
ALPHA VANE, A small moveable airfoil on the side of the fuselage transmitting airplane angle relative to airstream for the stall warning system.
迎角叶片,位于机身侧的可动小翼面。为失速警告系统传输飞机对气流的相对角度。
As design studies progressed it was found that several airfoil shapes could be used to satisfy the new performance criteria.
当进行设计的研究工作后，发现有几种翼型可以用来满足新的性能指标。
The Hawk 4 Gyroplane is supported in the air by a horizontally mounted airfoil similar to that of a helicopter but unpowered.
鹰4旋翼机利用类似直升机的旋翼提供升力,但机顶的水平旋翼无需动力推动。
An airfoil produces a lifting force that acts at right angles to the airstream and a dragging force that acts in the same direction as the airstream.
翼型产生升力的方向与气流成直角，阻力方向与气流方向相同。
Calculation of lift-drag characteristics of OAF and NACA63a312 airfoil at low speed using Jameson/TVD mixed scheme was carried out.
以Jameson/TVD混合格式对低速时的OAF和NACA63a312翼型的升阻特性进行了计算。
This main wing is made of a carbon/epoxy composite, is about 2 m in span, uses a NACA 4415 airfoil section, and pivots just ahead of the quarter chord.
主翼由碳/环氧合成物制成，跨度约为2米，使用NACA 4415 的翼剖面，将支点设在四分之一弦的前端。
This paper shows the wind tunnel testing results of NACA four symmetrical airfoil Section cascades of Wells turbine for wave energy conversion.
本文介绍用于波能转换的威尔斯涡轮的NACA四位数对称叶型叶栅的风洞试验结果。
Thus, it would be more advantageous to specify the velocity distribution from the outset and from that determine the airfoil shape.
因此,它会更有利,指明速度分布,从一开始就确定,从机翼形状.
A LU-SSOR method combined with TVD scheme is applied to compute the transonic airfoil flow in this paper, and the Baldwin-Lomax model is used.
本文采用LU－SSOR隐式推进方法，并结合TVD格式，计算了跨声速翼型的湍流解。
It is one of approaches for unsteady inverse problems of oscillating airfoil to solve unsteady Bluer equations with finite difference method.
利用有限差分法解非定常欧拉方程是振荡机翼非定常气动反问题的一种求解方法。
A small moveable airfoil on the side of the fuselage transmittng airplane angle relative to airstream for the stall warning system.
位于机身侧的可动小翼面，为失速警告系统传输飞机对气流的相对角度。
Provide an airfoil at the sill of the sash opening.It shall be mounted to provide a 1 inch slot above the hood interior counter top.
开口拉门处有一个翼面，安装时应在内部台面上留有1英寸的狭缝。
An unstructured grid was applied to the zone near the iced airfoil, whereas a structured grid was applied to save the storage and computational time.
在靠近积冰边界的内层采用了非结构网格，在非结构网格外采用结构化网格以节省存储空间和计算时间。