Experimental study of aerodynamic characteristics of closed parabolic wing

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Date

2016

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Publisher

International Collection of scientific proceedings «European Cooperation» – Warsaw, Poland

Abstract

The article presents the results of experiment model with closed parabolic wing in the wind tunnel Т-5 of the National Aerospace University – Kharkov Aviation Institute (KhAI), made in order to assess its overall effectiveness. Performed comparison of results obtained in wind tunnel T-5, with the results and the panel-vortex method and finite element method.

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Keywords

aircraft

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