本论文探讨了一种非接触式快速获取三维物体外形的检测方法——面结构光投影三角测量法。
It presents a method named surface Structured Light Projection Triangle Measurement, by which we can capture the surface topography of a three-dimensional object without any contact.
本文采用第二代低阶面元法给出了一种高升力外形下机翼的位流计算方法。
In this paper, based on the second generation low order panel method, a computational method of potential flow around wings under high-lift configuration is given.
本论文探讨了一种非接触式快速获取三维物体外形的检测方法——面结构光投影三角测量法。
This dissertation presents a method named surface Structured Light Projection Triangle Measurement, by which we can capture the surface topography of a 3d object without any contact.
为了提高数值计算效率和准确性，提出了基于多级响应面法的确定翼梢小翼气动外形参数的一种优化方法。
In order to improve the efficiency and accuracy of the numerical calculation for the aerodynamic design of winglets, an optimization method based on multi-level response surfaces is proposed.
为了提高数值计算效率和准确性，提出了基于多级响应面法的确定翼梢小翼气动外形参数的一种优化方法。
In order to improve the efficiency and accuracy of the numerical calculation for the aerodynamic design of winglets, an optimization method based on multi-level response surfaces is proposed.
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