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...
Main Author: | |
---|---|
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 |
id |
doaj-71b1da069e7648878b75a1001286915f |
---|---|
record_format |
Article |
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 |
_version_ |
1724827695547678720 |