DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING
The numerical method of calculation of aerodynamic characteristics of a profile is stated on the basis of the experiment of aerodynamic characteristics of a rectangular wing of a final lengthening. The problem is solved by a method consecutive approximation with the use of a matrix of private deriva...
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| Format: | Article |
| Language: | Russian |
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Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Научный вестник МГТУ ГА |
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| Online Access: | https://avia.mstuca.ru/jour/article/view/6 |
| _version_ | 1797883161090195456 |
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| author | B. L. Artamonov |
| author_facet | B. L. Artamonov |
| author_sort | B. L. Artamonov |
| collection | DOAJ |
| description | The numerical method of calculation of aerodynamic characteristics of a profile is stated on the basis of the experiment of aerodynamic characteristics of a rectangular wing of a final lengthening. The problem is solved by a method consecutive approximation with the use of a matrix of private derivative factors of elevating force and aerodynamic resistance of a wing under the appropriate characteristics of a profile. |
| first_indexed | 2024-04-10T03:46:16Z |
| format | Article |
| id | doaj.art-8092ed2074ac461d87d8fe8d7db3c2f2 |
| institution | Directory Open Access Journal |
| issn | 2079-0619 2542-0119 |
| language | Russian |
| last_indexed | 2024-04-10T03:46:16Z |
| publishDate | 2016-11-01 |
| publisher | Moscow State Technical University of Civil Aviation |
| record_format | Article |
| series | Научный вестник МГТУ ГА |
| spelling | doaj.art-8092ed2074ac461d87d8fe8d7db3c2f22023-03-13T07:19:11ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-01020028356DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WINGB. L. Artamonov0МАИ (НИУ)The numerical method of calculation of aerodynamic characteristics of a profile is stated on the basis of the experiment of aerodynamic characteristics of a rectangular wing of a final lengthening. The problem is solved by a method consecutive approximation with the use of a matrix of private derivative factors of elevating force and aerodynamic resistance of a wing under the appropriate characteristics of a profile.https://avia.mstuca.ru/jour/article/view/6численный методрасчет аэродинамических характеристикпрофиль |
| spellingShingle | B. L. Artamonov DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING Научный вестник МГТУ ГА численный метод расчет аэродинамических характеристик профиль |
| title | DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING |
| title_full | DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING |
| title_fullStr | DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING |
| title_full_unstemmed | DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING |
| title_short | DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING |
| title_sort | definition of aerodynamic characteristics of the profile under the drag polar of the finite wing |
| topic | численный метод расчет аэродинамических характеристик профиль |
| url | https://avia.mstuca.ru/jour/article/view/6 |
| work_keys_str_mv | AT blartamonov definitionofaerodynamiccharacteristicsoftheprofileunderthedragpolarofthefinitewing |