CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE
The ballistic missile model analysed in this paper presents a stringer type fuselage having 10 control surfaces, 8 directional surfaces to execute turns and 2 to execute manoeuvers for changing the angle of attack, but also 4 direction stabilisers. In this paper a CFD simulation was carried out on b...
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Format: | Article |
Language: | English |
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SORGING
2016-11-01
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Series: | Journal of Industrial Design and Engineering Graphics |
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Online Access: | http://sorging.ro/jideg/index.php/jid/article/view/305 |
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author | ZAHARIA Sebastian Marian ȘTEFĂNEANU Rareș Ioan |
author_facet | ZAHARIA Sebastian Marian ȘTEFĂNEANU Rareș Ioan |
author_sort | ZAHARIA Sebastian Marian |
collection | DOAJ |
description | The ballistic missile model analysed in this paper presents a stringer type fuselage having 10 control surfaces, 8 directional surfaces to execute turns and 2 to execute manoeuvers for changing the angle of attack, but also 4 direction stabilisers. In this paper a CFD simulation was carried out on ballistic missile with a new structure for determining the flight performance and the aerodynamic configuration. It was also performed a finite element analysis of the ballistic missile and the results obtained allowed to precisely determine the areas where the stress is greatest and where is necessary to provide several measures to increase the structure’s rigidity, to protect it from temperature and pressure. |
first_indexed | 2024-03-12T08:24:31Z |
format | Article |
id | doaj.art-4b61e29f996b493caedb078ad74df056 |
institution | Directory Open Access Journal |
issn | 1843-3766 2344-4681 |
language | English |
last_indexed | 2024-03-12T08:24:31Z |
publishDate | 2016-11-01 |
publisher | SORGING |
record_format | Article |
series | Journal of Industrial Design and Engineering Graphics |
spelling | doaj.art-4b61e29f996b493caedb078ad74df0562023-09-02T18:10:33ZengSORGINGJournal of Industrial Design and Engineering Graphics1843-37662344-46812016-11-0111CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILEZAHARIA Sebastian Marian0ȘTEFĂNEANU Rareș Ioan1PhD., Transilvania University of Braşov, Department of Manufacturing EngineeringNuarb Training Academy & Nuarb AerospaceThe ballistic missile model analysed in this paper presents a stringer type fuselage having 10 control surfaces, 8 directional surfaces to execute turns and 2 to execute manoeuvers for changing the angle of attack, but also 4 direction stabilisers. In this paper a CFD simulation was carried out on ballistic missile with a new structure for determining the flight performance and the aerodynamic configuration. It was also performed a finite element analysis of the ballistic missile and the results obtained allowed to precisely determine the areas where the stress is greatest and where is necessary to provide several measures to increase the structure’s rigidity, to protect it from temperature and pressure.http://sorging.ro/jideg/index.php/jid/article/view/305ballistic missile, CFD, finite element analysis, pressure, stress. |
spellingShingle | ZAHARIA Sebastian Marian ȘTEFĂNEANU Rareș Ioan CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE Journal of Industrial Design and Engineering Graphics ballistic missile, CFD, finite element analysis, pressure, stress. |
title | CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE |
title_full | CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE |
title_fullStr | CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE |
title_full_unstemmed | CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE |
title_short | CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILE |
title_sort | cfd simulation and fea analysis of a ballistic missile |
topic | ballistic missile, CFD, finite element analysis, pressure, stress. |
url | http://sorging.ro/jideg/index.php/jid/article/view/305 |
work_keys_str_mv | AT zahariasebastianmarian cfdsimulationandfeaanalysisofaballisticmissile AT stefaneanuraresioan cfdsimulationandfeaanalysisofaballisticmissile |