欢迎光临酷猫写作网

酷猫词典

首页英语词典airfoilairfoil实用场景例句

airfoil

英 ['eəfɒɪl] 美['ɛrfɔɪl]

英英释义实用场景例句

n. 机翼；螺旋桨

实用场景例句

The Joukowski airfoil problem is the simplest application of conformal mapping to airfoil design.: joukowski问题是最简单的翼型形映射应用到机翼设计.

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.

In the design page, submit the form to design the first airfoil.: 在设计页, 递交表格设计第一翼型.

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 high speed airfoil type wind turbine has the highest efficiency in high wind speeds.: 高速机翼型风轮机在高风速下达到最高的使用效率.

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.

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.

In this regard, several are given based on existing designs, eg, the SD 7037 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.

The Web version the code allows for the prescription 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.

The experimental results of NACA 0012 airfoil dynamic pressure measurement are given here.: 12翼型动态测压的实验结果,初步分析了影响翼型动态气动特性的因素.

The given airfoil is then analyzed to determine, say, its velocity distribution.: 由于机翼的分析,以确定那是说, 它的速度分布.

A supporting surface of an airplane ; an airfoil a wing.: 飞机有后掠翼的圆滑的机翼.

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.

How does the brake act on the paraglider airfoil?: 刹车是如何作用于滑翔伞的翼型?

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 properties of bifurcation points of airfoil flutter with cubic nonlinearity in incompressible flow are studied.: 对定常空气动力作用下、含立方非线性刚度的二元机翼颤振系统的分叉点进行了研究.

A supporting surface of an airplane ; an airfoil or a wing.: 飞机尾部组成部分的垂直机翼.

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.

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.