Application of boundary estimation method for determining aircraft aerodynamic parameters

<span lang="EN-US">Described is boundary estimation method of aircraft aerodynamic parameters which allows to determine with sufficient accuracy aerodynamic coefficients, necessary for diagnosis of available aeronautical engineering and for prediction of new real speciments</span&...

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Main Authors:	M. B. Миронович, А. Н. Сильвестров, A. A. Стенин, Р. Ф. Хотячук
Format:	Article
Language:	English
Published:	National Aviation University 2000-09-01
Series:	Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
Online Access:	http://jrnl.nau.edu.ua/index.php/visnik/article/view/9769

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spelling	doaj-f61bc999d129452ba523ea91b44ef23b2020-11-25T03:26:58ZengNational Aviation UniversityVìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu1813-11662306-14722000-09-0161-227628210.18372/2306-1472.6.97699445Application of boundary estimation method for determining aircraft aerodynamic parametersM. B. Миронович0А. Н. Сильвестров1A. A. Стенин2Р. Ф. Хотячук3National Aviation UniversityNational Aviation UniversityNational Aviation UniversityNational Aviation University<span lang="EN-US">Described is boundary estimation method of aircraft aerodynamic parameters which allows to determine with sufficient accuracy aerodynamic coefficients, necessary for diagnosis of available aeronautical engineering and for prediction of new real speciments</span>http://jrnl.nau.edu.ua/index.php/visnik/article/view/9769
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	M. B. Миронович А. Н. Сильвестров A. A. Стенин Р. Ф. Хотячук
spellingShingle	M. B. Миронович А. Н. Сильвестров A. A. Стенин Р. Ф. Хотячук Application of boundary estimation method for determining aircraft aerodynamic parameters Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
author_facet	M. B. Миронович А. Н. Сильвестров A. A. Стенин Р. Ф. Хотячук
author_sort	M. B. Миронович
title	Application of boundary estimation method for determining aircraft aerodynamic parameters
title_short	Application of boundary estimation method for determining aircraft aerodynamic parameters
title_full	Application of boundary estimation method for determining aircraft aerodynamic parameters
title_fullStr	Application of boundary estimation method for determining aircraft aerodynamic parameters
title_full_unstemmed	Application of boundary estimation method for determining aircraft aerodynamic parameters
title_sort	application of boundary estimation method for determining aircraft aerodynamic parameters
publisher	National Aviation University
series	Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
issn	1813-1166 2306-1472
publishDate	2000-09-01
description	<span lang="EN-US">Described is boundary estimation method of aircraft aerodynamic parameters which allows to determine with sufficient accuracy aerodynamic coefficients, necessary for diagnosis of available aeronautical engineering and for prediction of new real speciments</span>
url	http://jrnl.nau.edu.ua/index.php/visnik/article/view/9769
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Application of boundary estimation method for determining aircraft aerodynamic parameters

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