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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Main Authors: ZAHARIA Sebastian Marian, ȘTEFĂNEANU Rareș Ioan
Format: Article
Language:English
Published: SORGING 2016-11-01
Series:Journal of Industrial Design and Engineering Graphics
Subjects:
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.
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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
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