Please use this identifier to cite or link to this item: http://er.nau.edu.ua:8080/handle/NAU/24026
Title: Experimental study of aerodynamic characteristics of closed parabolic wing
Authors: Rahmati, Ahmad
Рахмати, Ахмад
Keywords: aircraft, closed parabolic wing, panel-vortex method, finite element method.
Issue Date: 2016
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.
URI: http://er.nau.edu.ua:8080/handle/NAU/24026
Appears in Collections:Наукові статті кафедри АД та БПЛА

Files in This Item:
File Description SizeFormat 
Статья №5.pdfThe 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 MBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.