TsAGI Science Journal
Publicou 6 edições por ano
ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604
PARAMETRIC DESCRIPTION OF THE AIRFOIL USING COMBINED POLYNOMIAL FUNCTIONS FOR OPTIMIZATION APPLICATIONS
Volume 46,
Edição 7, 2015,
pp. 647-656
DOI: 10.1615/TsAGISciJ.v46.i7.30
RESUMO
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.
CITADO POR
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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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