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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Main Authors: V. T. Kalugin, A. G. Golubev, A. S. Epikhin, A. A. Michkin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2017-01-01
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.
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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
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AT asepikhin applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds
AT aamichkin applicabilityoftheopensourcepackageopenfoamfornumericalmodelingseparatedflowaroundanaircraftatsubsonicandsupersonicspeeds