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://www.sorging.ro/jideg/index.php/jideg/article/view/190 |
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author | Sebastian Marian Zaharia Rares Ioan Stefanescu |
author_facet | Sebastian Marian Zaharia Rares Ioan Stefanescu |
author_sort | Sebastian Marian Zaharia |
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 | 2024-03-12T11:04:06Z |
format | Article |
id | doaj.art-0da568d4da4e4ff1a1508c13aec319ac |
institution | Directory Open Access Journal |
issn | 1843-3766 2344-4681 |
language | English |
last_indexed | 2024-03-12T11:04:06Z |
publishDate | 2016-11-01 |
publisher | SORGING |
record_format | Article |
series | Journal of Industrial Design and Engineering Graphics |
spelling | doaj.art-0da568d4da4e4ff1a1508c13aec319ac2023-09-02T04:15:37ZengSORGINGJournal of Industrial Design and Engineering Graphics1843-37662344-46812016-11-01112CFD SIMULATION AND FEA ANALYSIS OF A BALLISTIC MISSILESebastian Marian Zaharia0Rares Ioan Stefanescu1Transilvania University of BrasovNuarb 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://www.sorging.ro/jideg/index.php/jideg/article/view/190ballistic missileCFDfinite element analysispressurestress |
spellingShingle | Sebastian Marian Zaharia Rares Ioan Stefanescu 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://www.sorging.ro/jideg/index.php/jideg/article/view/190 |
work_keys_str_mv | AT sebastianmarianzaharia cfdsimulationandfeaanalysisofaballisticmissile AT raresioanstefanescu cfdsimulationandfeaanalysisofaballisticmissile |