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。
The variable-domain variation is a specific tool of handling unknown boundaries and suitable for designing airfoil shape.
变域变分是一种处理未知界面的独特工具，极适合于气动外形的设计求解。
Thus, it would be more advantageous to specify the velocity distribution from the outset and from that determine the airfoil shape.
因此，它会更有利，指明速度分布，从一开始就确定，从机翼形状。
This paper also presents the experimental results of effects of the blade tip clearance and the airfoil shape on the stall flutter boundary.
此外还给出了两种叶尖间隙和两种叶型对失速颤振影响的实验结果。
The variational of finite element method(FEM) using the pseudo-potential function is presented to design the airfoil shape of transonic rotational flows.
本文运用赝势函数变域变分有限元方法进行了跨音速翼型设计。
Looking at that in the lab, it becomes a function of airfoil shape, and also of the flow control technologies you use to enhance the laminar flow with conformal trailing edge surfaces.
实验室的研究表明，它已经成了机翼的一项功能，也是通过适形机翼后缘表面来增强层流的流控制技术的功能。
This paper gives the affects of airfoil tailing edge added different dimension and different shape plates on lift-drag and pitching-moment performance of airfoil.
给出了在翼型后缘加不同尺寸和形状的平板对翼型升阻特性和力矩特性的影响。
A specific shape and fixe position of shock control bump is designed for RAE2822 airfoil by testing many CFD solutions.
通过大量CFD试验，针对RAE2822翼型设计了一种特定外形的激波控制鼓包并确定了其具体安装位置。
The primary work of the proposed approach is to obtain shape curves by segmenting the overhead view image of airfoil. With exact transformation of the curves, the ice shape can be determined.
试验验证表明本文模型可以获得准确的分割结果，模拟试验的误差分析表明算法具有较高的精度。
The primary work of the proposed approach is to obtain shape curves by segmenting the overhead view image of airfoil. With exact transformation of the curves, the ice shape can be determined.
试验验证表明本文模型可以获得准确的分割结果，模拟试验的误差分析表明算法具有较高的精度。
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