The compressive effects of airflow are great on the aerodynamics at high speed's flight.

The large eddy simulation approach is applied to airflow field around buildings.

应用紊流大涡模拟方法对建筑物环境风场进行了数值模拟.

There they test the airflow around their latest designs.

他们在那里测试他们的最新设计(汽车)周围的气流.

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.

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.

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 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.

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.

How does the brake act on the paraglider airfoil?

刹车是如何作用于滑翔伞的翼型?

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.

A supporting surface of an airplane ; an airfoil a wing.

飞机有后掠翼的圆滑的机翼.

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.

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 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.

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.

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.

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.

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.

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.

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.

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.