Abstract

Results of the aerodynamic coefficients imitation of wing airfoils and helicopter blades are presented. The modeling is carried out using the artificial neural network algorithms. The dependencies of the lift coefficient and the drag coefficient on the angle of attack are imitated for various airfoil geometries.

中文翻译：

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翼型（叶片）气动系数模拟建模适用性研究

摘要

介绍了模拟机翼翼型和直升机叶片的空气动力学系数的结果。使用人工神经网络算法进行建模。针对各种翼型几何形状模拟升力系数和阻力系数对迎角的依赖性。