airfoil shaped中文是什么意思

• 成翼型形状的

• "airfoil"中文翻译    【航空】机翼；翼形，翼剖面。
• "shape"中文翻译    n. 1.形状；样子；形态；外形；模样。 2.形式；定型 ...
• "airfoil-shaped" 中文翻译 :    成机翼形状的; 成翼型形状的
• "diamond-shaped airfoil" 中文翻译 :    菱形翼形
• "airfoil" 中文翻译 :    【航空】机翼；翼形，翼剖面。
• "shaped" 中文翻译 :    （面包）模的；模制的; 成型的; 丁字形的; 定形的; 塑造; 形似的 成形的; 异形的; 制成一定形状的
• "t shaped" 中文翻译 :    t形的
• "t-shaped" 中文翻译 :    t形的; Ｔ形; 丁字形的
• "aerofoil; airfoil" 中文翻译 :    翼面；空气动力面
• "airfoil blade" 中文翻译 :    翼型叶片
• "airfoil camber" 中文翻译 :    机翼翘曲; 机翼上翘; 翼型曲面; 翼型中弧高; 翼形弯度
• "airfoil cascade" 中文翻译 :    导向叶片系; 翼型栅; 翼栅
• "airfoil characteristic" 中文翻译 :    翼型特性
• "airfoil characteristics" 中文翻译 :    翼型特性; 翼形特性
• "airfoil chord" 中文翻译 :    机翼弦; 翼弦
• "airfoil coefficients" 中文翻译 :    翼形系数
• "airfoil configuration" 中文翻译 :    翼型形状
• "airfoil contour" 中文翻译 :    翼型外形
• "airfoil curvature" 中文翻译 :    翼型曲率
• "airfoil data" 中文翻译 :    翼型数据
• "airfoil design" 中文翻译 :    翼形设计
• "airfoil drag" 中文翻译 :    翼型阻力
• "airfoil element" 中文翻译 :    机翼型元件
• "airfoil family" 中文翻译 :    翼型族
• "airfoil fan" 中文翻译 :    机翼型叶片风机; 翼型叶片

• 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 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
• 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
• 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
• In this paper , the boundary layer characteristics of a supercritical airfoil is researched in wind tunnel . from the start to control boundary layer separation and to improve aerodynamics characteristics of this airfoil , three kinds of trapezoid , delta and airfoil shaped vortex generators are designed based on traditional , sub boundary layer and micro - vortex generators conceptual design . it include as follows : 1
  研究工作中，从控制该翼型附面层分离、提高大迎角气动性能的角度出发，通过风洞实验研究，研究了该翼型的附面层特性和气动性能，针对其附面层特性，给出了梯形、三角形和翼型式三种涡流发生器设计方案，为下一步研究工作奠定了坚实基础。
• An airfoil shape design method that couples viscous flow analysis , a complex method and parallel calculation is described in this paper . the method is applied to search an airfoil geometry with improved aerodynamic performance at single or multiple design - point while the specified design constraints being satisfied
  本文将流场分析程序、复合形优化方法和并行计算耦合起来，发展了一种工程实用的翼型优化设计方法，用以提高翼型在单个或多个设计点、多种约束条件下的气动性能。
• Three kinds of trapezoid , delta and airfoil shaped vortex generators are designed based on traditional , sub boundary layer and micro - vortex generators conceptual design , to study the influence of the shape , height , aspect ratio , chordwise position , spanwise position and direction angles of vortex generators on boundary layer separation control
  ( 5 )综合分析研究了涡流发生器的工作原理和设计原则。根据国内外资料，研究了涡流发生器形状、高度、展弦比、尖削比、弦向位置、展向位置和方位角等因素对附面层分离控制效果的影响。