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。
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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