俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
PARAMETRIC DESCRIPTION OF THE AIRFOIL USING COMBINED POLYNOMIAL FUNCTIONS FOR OPTIMIZATION APPLICATIONS
卷 46,
册 7, 2015,
pp. 647-656
DOI: 10.1615/TsAGISciJ.v46.i7.30
摘要
An approach for airfoil parameterization using geometric parameters is proposed. This approach is meant to be used for the analytical airfoil contours. A class of combined polynomial airfoil contours is considered. The approximation accuracy is tested using the example of certain airfoils. The pressure distributions for the original and approximated airfoils are compared. An example of the optimization of the airfoil aerodynamic characteristics is considered.
对本文的引用
-
Nikolaev Nikolay V., Optimization of Airfoils along High-Aspect-Ratio Wing of Long-Endurance Aircraft in Trimmed Flight, Journal of Aerospace Engineering, 32, 6, 2019. Crossref
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