翼型设计的英文

• two dimensional aerofoil design
• wing section design

• "翼型"英文翻译    airfoil profile; airfoil sec ...
• "设计"英文翻译    devise; project; plan; desig ...
• "薄型设计" 英文翻译 :    shallow profile
• "便携型设计" 英文翻译 :    protable type
• "超小型设计" 英文翻译 :    compact type
• "典型设计" 英文翻译 :    typical design
• "典型设计图" 英文翻译 :    typical design
• "定型设计" 英文翻译 :    design type; final design; finalized design; modular design; standardized design
• "发型设计" 英文翻译 :    hair design; hair setting; hair styling; hari design
• "发型设计师" 英文翻译 :    [美国] hairtician
• "改型设计" 英文翻译 :    model change
• "辊型设计" 英文翻译 :    cambering
• "剂型设计" 英文翻译 :    dosage form design
• "孔型设计" 英文翻译 :    calibrating; design of grooves; design of passes; designing; grooving; pass design
• "孔型设计人" 英文翻译 :    roll designer
• "炉型设计" 英文翻译 :    design of section
• "模型设计" 英文翻译 :    model design; pattern design; pattern layout; pattern plan
• "模型设计板" 英文翻译 :    layout board
• "模型设计法" 英文翻译 :    model design method
• "模型设计图" 英文翻译 :    pattern layout
• "收纳型设计" 英文翻译 :    selfcontainning design
• "完备型设计" 英文翻译 :    complete block design
• "线型设计" 英文翻译 :    lines design
• "小型设计" 英文翻译 :    miniature design
• "新型设计" 英文翻译 :    new design

• Nevertheless , a surprisingly wide variety of airfoils can be designed with just four segments
  然而,出乎意料的是各种各样的翼型设计可以仅4部分
• 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
• 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
• Finally , a special form allows the user to prescribe any number of segments so that practical airfoils can be designed
  最后,一种特殊形式允许用户指定任何数目的片段,可以使实际翼型设计
• Numerical results show that the method provides an effective tool for refining and designing a fransonic airfoil
  算例结果表明，本方法提供了一种跨音速翼型改型设计及新翼型设计的有效工具。
• In this paper the direct iterative surface curvature ( disc ) design method is presented for designing airfoils at transonic speeds
  本论文采用直接表面曲率迭代方法( disc )进行跨声速翼型设计。
• After the airfoil is designed , the velocity distributions , airfoil shape , converged input file ( with phi2 adjusted , see details below ) and airfoil coordinates are returned for display
  翼型设计后的速度分布、机翼形状、汇流输入档案( phi2调整细节见下文) 、翼型坐标送返展示
• The design method used here is relatively independent with the direct procedure of calculation of flow solver by finite volume method , other flow solvers can also be easily coupled with this design method
  本文的设计方法与正计算过程有相对的独立性，可分别和不同的流场分析程序耦合，形成翼型设计软件。
• Proceed from the angle of energy and taking considerations on interference factor and drag of airfoil profile , a kind of new typed calculation method on the design of vane air foil was put forward according to the vortex aerodynamics model of the rotor of wind turbines with horizontal axis
  摘要根据水平轴风力机转子的涡流气动模型，从能量的角度入手，考虑干涉因子和翼型阻力，提出了叶片翼型设计的一种新型计算方法。