Chinese translation for "附面层特性"

behavior of boundary layer
boundary layer characteristics

Related Translations:

附面层计算:  boundary-layer calculationboundary-layer computation

附面层转变:  boundary layer transition

附面层稳定:  boundary layer stabilization

附面层动态:  boundary-layer behavior

进口附面层:  inlet boundary layer

亚音速附面层:  subsonic boundary layer

附面层控制:  blcboundary layer control

附面层能量:  boundary layer energy

附面层边界:  boundary layer edge

旋涡附面层:  eddying shear layer

Example Sentences:

	1.	4 . the influence of reynolds number to aerodynamics and boundary layer is investigated . 5 ( 4 )研究了雷诺数对翼型气动力和附面层特性的影响。
	2.	2 . the aerodynamics characteristics of this airfoil is studied in wind tunnel . this studies provides the direction of the research on boundary layer ( 2 )进行了翼型的低速气动力性能研究，为附面层特性研究提供了方向。
	3.	Provide the experimental research scheme to measure and diagnose boundary layer of airfoil . the satisfied results demonstrated that this scheme is correct and efficient . it provides the reliable foundation on analysis of boundary layer characteristics and vortex generators " design 研究结果表明，该方案是正确的，既切实可行、节约了实验经费，又获得了满意的实验结果，为分析附面层特性和涡流发生器的设计提高了可靠依据。
	4.	3 . the characteristics of boundary layer ' s transition , shape and separation are researched . the details as follows : ( l ) airfoil surface is turbulent boundary layer flows ; ( 2 ) velocity figure changed unsteady near the point of boundary layer separation due to randomicity of turbulent flow ; ( 3 ) the airfoil have better state of boundary layer separation and poor stall characteristics because of the upper surface of airfoil is flat 给出了该翼型的附面层特性：翼型表面基本为湍流附面层；在靠近附面层分离位置处，速度型形状、特别是靠近翼型表面的底部速度型形状变化不定，是湍流流动的随机性所致；该翼型具有较好的附面层分离形态，但在失速迎角附近，附面层分离形态变化剧烈、失速特性差，是翼型上翼面形状较为平坦所致。
	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。

Similar Words：

"附面层剖面图" Chinese translation, "附面层气流" Chinese translation, "附面层气流向翼尖流动" Chinese translation, "附面层扰流器" Chinese translation, "附面层损失" Chinese translation, "附面层条件" Chinese translation, "附面层位移" Chinese translation, "附面层位移厚度" Chinese translation, "附面层位移效应" Chinese translation, "附面层稳定" Chinese translation