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...
| Main Authors: | , , , |
|---|---|
| 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 |
| _version_ | 1826564006923468800 |
|---|---|
| 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 | 2025-03-14T10:13:00Z |
| publishDate | 2017-01-01 |
| publisher | Moscow State Technical University of Civil Aviation |
| record_format | Article |
| series | Научный вестник МГТУ ГА |
| spelling | doaj.art-b8259442c2434024b6b07219af2ffa2c2025-03-02T11:13:35ZrusMoscow 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/961open source package openfoamseparated flowflow past bodies with a break generatrixrapidly rotating aerial vehiclesupersonic separated flow field |
| 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 open source package openfoam separated flow flow past bodies with a break generatrix rapidly rotating aerial vehicle supersonic separated flow field |
| 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 | open source package openfoam separated flow flow past bodies with a break generatrix rapidly rotating aerial vehicle supersonic separated flow field |
| 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 |