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本文给出了计算有分离低速粘性流中多段翼型气动特性的一种快速方法,与国内外实验结果及国外计算结果进行了比较,得到了较为一致的结果.方法和程序己用于支线飞机翼型研究中襟翼系统设计。
In this paper, a fast method for calculating the aerodynamic characteristics of multi-section airfoils with separated low-velocity viscous flow is given, which is compared with the experimental results at home and abroad and the calculated results abroad. The results are consistent. The method and program have been used in regional aircraft Flap System Design in Airfoil Research.