APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS
Applicability of the open source package OpenFOAM for numerical modeling different separated flows have been considered in the cases studies of the influence of vortices and their interaction with lifting surfaces, features of the flow field of rapidly rotating aerial vehicles at presence of separat...
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Format: | Article |
Language: | Russian |
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Moscow State Technical University of Civil Aviation
2017-01-01
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Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/961 |
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author | V. T. Kalugin A. G. Golubev A. S. Epikhin A. A. Michkin |
author_facet | V. T. Kalugin A. G. Golubev A. S. Epikhin A. A. Michkin |
author_sort | V. T. Kalugin |
collection | DOAJ |
description | Applicability of the open source package OpenFOAM for numerical modeling different separated flows have been considered in the cases studies of the influence of vortices and their interaction with lifting surfaces, features of the flow field of rapidly rotating aerial vehicles at presence of separation flow and study of supersonic separated flow field in flight controls. |
first_indexed | 2024-04-10T03:44:26Z |
format | Article |
id | doaj.art-b8259442c2434024b6b07219af2ffa2c |
institution | Directory Open Access Journal |
issn | 2079-0619 2542-0119 |
language | Russian |
last_indexed | 2024-04-10T03:44:26Z |
publishDate | 2017-01-01 |
publisher | Moscow State Technical University of Civil Aviation |
record_format | Article |
series | Научный вестник МГТУ ГА |
spelling | doaj.art-b8259442c2434024b6b07219af2ffa2c2023-03-13T07:19:17ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192017-01-0101992330961APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDSV. T. Kalugin0A. G. Golubev1A. S. Epikhin2A. A. Michkin3МГТУ им. Н.Э. БауманаМГТУ им. Н.Э. БауманаМГТУ им. Н.Э. БауманаМГТУ им. Н.Э. БауманаApplicability of the open source package OpenFOAM for numerical modeling different separated flows have been considered in the cases studies of the influence of vortices and their interaction with lifting surfaces, features of the flow field of rapidly rotating aerial vehicles at presence of separation flow and study of supersonic separated flow field in flight controls.https://avia.mstuca.ru/jour/article/view/961пакет openfoamотрывное течениеобтекание тел с излом образующейбыстровращающиеся летательные аппаратысверхзвуковое отрывное обтекание |
spellingShingle | V. T. Kalugin A. G. Golubev A. S. Epikhin A. A. Michkin APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS Научный вестник МГТУ ГА пакет openfoam отрывное течение обтекание тел с излом образующей быстровращающиеся летательные аппараты сверхзвуковое отрывное обтекание |
title | APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS |
title_full | APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS |
title_fullStr | APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS |
title_full_unstemmed | APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS |
title_short | APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS |
title_sort | applicability of the open source package openfoam for numerical modeling separated flow around an aircraft at subsonic and supersonic speeds |
topic | пакет openfoam отрывное течение обтекание тел с излом образующей быстровращающиеся летательные аппараты сверхзвуковое отрывное обтекание |
url | https://avia.mstuca.ru/jour/article/view/961 |
work_keys_str_mv | AT vtkalugin applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds AT aggolubev applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds AT asepikhin applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds AT aamichkin applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds |