Aerodynamic performances of complex shape wings

<p><em> The task of calculation of optimum circulation distribution along wingspan of complex shape wings is considered. For solving this problem Glauert-Trefts’s equation and its modifications are used. Calculations are carried out for both sweptback and forward-swept wings. It is shown...

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Main Author: О.О. Кім
Format: Article
Language:English
Published: National Aviation University 2005-04-01
Series:Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
Online Access:http://jrnl.nau.edu.ua/index.php/visnik/article/view/1248
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spelling doaj-71b1da069e7648878b75a1001286915f2020-11-25T02:30:49ZengNational Aviation UniversityVìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu1813-11662306-14722005-04-0126410410810.18372/2306-1472.26.12481221Aerodynamic performances of complex shape wingsО.О. Кім0НАУ, Аерокосмічний інститут<p><em> The task of calculation of optimum circulation distribution along wingspan of complex shape wings is considered. For solving this problem Glauert-Trefts’s equation and its modifications are used. Calculations are carried out for both sweptback and forward-swept wings. It is shown that optimum circulation distribution depends on the sweep angle χ and  on the chord b(z) distribution along wingspan. Some aerodynamic coefficients such as induced drag coefficient C<sub>Di</sub> and pitching moment coefficient C<sub>mZ</sub> are calculated for wings of different shape. The comparison of wings </em><br /><em>performances is done. In order to obtain the minimum wing induced drag with the given lift force it is very important to determine how the circulation should change along the wingspan. Results obtained by E. K. Karafoli G.F. Burago and others are used. A set of theoretical generalizations and modifications of formulas for aerodynamic coefficients are </em><br /><em>obtained. These results permit to compare aerodynamic performances of sweptback and forward-swept wings. Modified Glauert-Trefts’s integral-differential equation is formulated for wings of complex shape.</em></p>http://jrnl.nau.edu.ua/index.php/visnik/article/view/1248
collection DOAJ
language English
format Article
sources DOAJ
author О.О. Кім
spellingShingle О.О. Кім
Aerodynamic performances of complex shape wings
Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
author_facet О.О. Кім
author_sort О.О. Кім
title Aerodynamic performances of complex shape wings
title_short Aerodynamic performances of complex shape wings
title_full Aerodynamic performances of complex shape wings
title_fullStr Aerodynamic performances of complex shape wings
title_full_unstemmed Aerodynamic performances of complex shape wings
title_sort aerodynamic performances of complex shape wings
publisher National Aviation University
series Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
issn 1813-1166
2306-1472
publishDate 2005-04-01
description <p><em> The task of calculation of optimum circulation distribution along wingspan of complex shape wings is considered. For solving this problem Glauert-Trefts’s equation and its modifications are used. Calculations are carried out for both sweptback and forward-swept wings. It is shown that optimum circulation distribution depends on the sweep angle χ and  on the chord b(z) distribution along wingspan. Some aerodynamic coefficients such as induced drag coefficient C<sub>Di</sub> and pitching moment coefficient C<sub>mZ</sub> are calculated for wings of different shape. The comparison of wings </em><br /><em>performances is done. In order to obtain the minimum wing induced drag with the given lift force it is very important to determine how the circulation should change along the wingspan. Results obtained by E. K. Karafoli G.F. Burago and others are used. A set of theoretical generalizations and modifications of formulas for aerodynamic coefficients are </em><br /><em>obtained. These results permit to compare aerodynamic performances of sweptback and forward-swept wings. Modified Glauert-Trefts’s integral-differential equation is formulated for wings of complex shape.</em></p>
url http://jrnl.nau.edu.ua/index.php/visnik/article/view/1248
work_keys_str_mv AT ookím aerodynamicperformancesofcomplexshapewings
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