Chinese translation for "airfoil shape"

翼形形状

Related Translations:

airfoil theory:  机翼理论翼型理论翼形理论

airfoil contour:  翼型外形

stalled airfoil:  失速机翼

bottom airfoil:  下翼面

swept airfoil:  后掠翼

airfoil section:  翼剖面翼型剖面纵向翼切面

pitching airfoil:  俯仰运动的机翼

slender airfoil:  细长翼型

annular airfoil:  环形翼

airfoil surface:  翼面

Example Sentences:

	1.	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。
	2.	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
	3.	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
	4.	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
	5.	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。
	6.	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。
	7.	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。

Similar Words：

"airfoil profile loss" Chinese translation, "airfoil propeller" Chinese translation, "airfoil section" Chinese translation, "airfoil section characteristic" Chinese translation, "airfoil section drag" Chinese translation, "airfoil shaped" Chinese translation, "airfoil shell" Chinese translation, "airfoil sin cascade" Chinese translation, "airfoil sin lattice" Chinese translation, "airfoil slot" Chinese translation