Experimental study of aerodynamic characteristics of closed parabolic wing

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/24026

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DC Field	Value	Language
dc.contributor.author	Rahmati, Ahmad	en
dc.contributor.author	Рахмати, Ахмад	ru
dc.date.accessioned	2017-01-02T16:39:32Z	-
dc.date.available	2017-01-02T16:39:32Z	-
dc.date.issued	2016	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/24026	-
dc.description.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.	en
dc.language.iso	en	en
dc.publisher	International Collection of scientific proceedings «European Cooperation» – Warsaw, Poland	en
dc.subject	aircraft	en
dc.title	Experimental study of aerodynamic characteristics of closed parabolic wing	en
Appears in Collections:	Наукові статті кафедри аеродинаміки та безпеки польотів літальних апаратів

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Статья №5.pdf	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.	1.37 MB	Adobe PDF	View/Open