aerofoil造句

• Wings are aerofoils .
  机翼是翼型面。
• Finite element analysis of aerofoil fatigue failure
  飞机机翼疲劳断裂过程的有限元分析
• Fatigue failure analysis of aerofoil girder leading to air disaster
  导致空难的机翼大梁的疲劳失效分析
• A feature of the bridge is its specially designed aerofoil shaped deck
  青马大桥的其中一项设计特式是其翼式桥面。
• Variable sweep aerofoil
  可变后掠翼
• Flutter of aerofoil
  机翼颤振
• There we remove one of the aerofoils altogether to reduce drag to a minimum on the long , fast straights
  我们拿掉了一片小翼来减少抓地力，使得赛车在直道上面更具优势。 ”
• Nf - 6 wind tunnel is a pressurizing , continuous , high - speed and return - flow aerofoil wind tunnel
  Nf - 6风洞是一座由轴流式压缩机驱动的增压、连续、高速回流式翼型风洞。
• An aircraft ' s aerofoils are shaped so that air travelling over their top surfaces moves faster than that underneath , creating an area of low pressure
  一片小翼的形状可以是通过它上方的气流比通过它下方的气流速度更快，从而产生下压力。
• Pressurizing , continuous and transonic wind tunnel is the first one in our country , and it is the world ' s first class tremendous high - speed aerofoil wind
  增压连续式跨音速风洞在我国尚属首例，是具有国际先进水平的大型高速翼型风洞。
• Loss of head is minimized by the balanced disc and its " aerofoil " design . streamlined body without pockets contributes to straight - through flow
  通过平衡阀瓣及其“翼型”结构，将水头损失(或位差损失)降到最小程度。流线型阀体，不再需要凹穴来帮助流体直线流通。
• In the end , using the product development process of aerofoil rib a software platform which supporting dmpa modeling is developed with software visual c + + 6 . 0 and access 2000
  以飞机垂尾的产品开发过程为对象，采用用visualc + + 6 . 0和access2000完成了系统的程序设计，开发了基于dmpa的过程建模系统。
• On the background of aeronautics and astronautics requirement , along with the line of modularization of fiber optic smart structure , aimed at the safety matter of aerofoil pivotal parts , build optic fiber smart layer self - diagnosing system
  以航空航天需求为背景,以光纤智能结构的集成为主线,针对飞机机翼关键部件安全性问题,建立了基于光纤智能夹层的自诊断系统。
• In this paper , some flows around naca 0012 aerofoil , m6 wing and two different blunt vehicles are simulated , the results show that the present algorithm possesses good characteristics and capability for normal mach number and for hypersonic of simple configurations
  通过对naca0012翼型、 m6机翼、钝头以及双钝锥?柱体的算例验证，本文能很好的解决一般马赫数问题，能够很好的求解简单外形的高超声速问题，对于复杂外形飞行器还需要进一步进行研究验证。
• Abstract : in this paper , a principle and method of the speed pulse waveform sampling are introduced . its object is to study an effect of the turning factor on torbulence . test is done in the aerofoil fengwen . on design of the user interface , application of the timer and displaying way of a pape and continuity are specifically discussed . expermental results and analysis is showed at the last
  文摘:以翼型风洞为对象，着重介绍了变湍流度对翼型转捩因子影响的速度脉动波形采集的原理和方法，重点对波形采集系统用户界面的设计、定时器的应用、分页显示和连续显示等技术进行了具体介绍，并给出了实验结果及分析。