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: Sebastian Marian Zaharia, Rares Ioan Stefanescu
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/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.
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spelling doaj.art-39d4ebd2c6144dfd9ace00cb3749cb4b2023-09-02T08:32:02ZengSORGINGJournal 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://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://sorging.ro/jideg/index.php/jideg/article/view/190
work_keys_str_mv AT sebastianmarianzaharia cfdsimulationandfeaanalysisofaballisticmissile
AT raresioanstefanescu cfdsimulationandfeaanalysisofaballisticmissile