Computer modeling of exhaust jet flux interaction with deflecting shield

Method of exhaust jet flux interaction with deflecting shield computer modeling is proposed in this article. The article is devoted to concrete ecological task - to decrease the noise influence on ground maintenance stuff and passengers in the airports. The method is based on the Reynolds equation s...

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Main Author: O. A. Kartishev
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/325
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author O. A. Kartishev
author_facet O. A. Kartishev
author_sort O. A. Kartishev
collection DOAJ
description Method of exhaust jet flux interaction with deflecting shield computer modeling is proposed in this article. The article is devoted to concrete ecological task - to decrease the noise influence on ground maintenance stuff and passengers in the airports. The method is based on the Reynolds equation system solution obtained with the help of control volume method. Calculation results give an opportunity to choose main deflecting shield parameters according to concrete airport conditions.
format Article
id doaj-art-c2bcc90132e64c699a908c44d81cb7b7
institution Kabale University
issn 2079-0619
2542-0119
language Russian
publishDate 2016-11-01
publisher Moscow State Technical University of Civil Aviation
record_format Article
series Научный вестник МГТУ ГА
spelling doaj-art-c2bcc90132e64c699a908c44d81cb7b72025-08-20T03:56:28ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-0102085459325Computer modeling of exhaust jet flux interaction with deflecting shieldO. A. Kartishev0ГосНИИ ГАMethod of exhaust jet flux interaction with deflecting shield computer modeling is proposed in this article. The article is devoted to concrete ecological task - to decrease the noise influence on ground maintenance stuff and passengers in the airports. The method is based on the Reynolds equation system solution obtained with the help of control volume method. Calculation results give an opportunity to choose main deflecting shield parameters according to concrete airport conditions.https://avia.mstuca.ru/jour/article/view/325jet fluxdeflecting shieldcomputer flow modelingmethod of definite volume
spellingShingle O. A. Kartishev
Computer modeling of exhaust jet flux interaction with deflecting shield
Научный вестник МГТУ ГА
jet flux
deflecting shield
computer flow modeling
method of definite volume
title Computer modeling of exhaust jet flux interaction with deflecting shield
title_full Computer modeling of exhaust jet flux interaction with deflecting shield
title_fullStr Computer modeling of exhaust jet flux interaction with deflecting shield
title_full_unstemmed Computer modeling of exhaust jet flux interaction with deflecting shield
title_short Computer modeling of exhaust jet flux interaction with deflecting shield
title_sort computer modeling of exhaust jet flux interaction with deflecting shield
topic jet flux
deflecting shield
computer flow modeling
method of definite volume
url https://avia.mstuca.ru/jour/article/view/325
work_keys_str_mv AT oakartishev computermodelingofexhaustjetfluxinteractionwithdeflectingshield