A new method is presented to calculate the exact analytic solution of potential flow about multi - element airfoils.
本文给出了求解多段翼型位流准确解的一种方法。
The solution we obtained presents generality, because it contains some exact analytic solutions that are given in other papers.
这些解更具有一般性,它包含着已有文献给出的精确解析解。
And then obtain exact solution of the problem by using analytic method.
然后采用解析方法求解,得到了问题的精确解。
With the analytic solution as exact solution, a model problem with homogeneous boundary condition of derivative type is calculated.
计算实例针对二类齐次边值问题,以解析解作为精确解,研究了不同节点数时整体误差和局部误差的变化。
With the analytic solution as exact solution, a model problem with homogeneous boundary condition of derivative type is calculated.
计算实例针对二类齐次边值问题,以解析解作为精确解,研究了不同节点数时整体误差和局部误差的变化。
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