COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191

The main objective of this work was to accomplish the computational simulation in the software CadWind® of a filament winding for an applied pressure vase to motor rocket. The adopted simulation was of a non-geodesic helical winding, varying the winding angle in the cylindrical part of the pressure...

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Main Authors: Rafael F. Heitkoetter, Sérgio Frascino M. Almeida, Luís E. V. Loures da Costa
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2011-07-01
Series:Journal of Aerospace Technology and Management
Subjects:
Online Access:https://www.jatm.com.br/jatm/article/view/23
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author Rafael F. Heitkoetter
Sérgio Frascino M. Almeida
Luís E. V. Loures da Costa
author_facet Rafael F. Heitkoetter
Sérgio Frascino M. Almeida
Luís E. V. Loures da Costa
author_sort Rafael F. Heitkoetter
collection DOAJ
description The main objective of this work was to accomplish the computational simulation in the software CadWind® of a filament winding for an applied pressure vase to motor rocket. The adopted simulation was of a non-geodesic helical winding, varying the winding angle in the cylindrical part of the pressure vessel, due the polar holes be different and the vessel long. Also simulations were accomplished varying the winding pattern. The results indicate that a more substantial winding pattern provides increased fiber deposition and distribution on the outer region of the domes.
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spelling doaj.art-2c61c15f249846929c06f05f124b143c2022-12-22T02:14:10ZengInstituto de Aeronáutica e Espaço (IAE)Journal of Aerospace Technology and Management2175-91462011-07-0112COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191Rafael F. Heitkoetter0Sérgio Frascino M. Almeida1Luís E. V. Loures da Costa2Institute of Aeronautics and Space São José dos Campos/ SPTechnological Institute of Aeronautics São José dos Campos/SPInstitute of Aeronautics and Space São José dos Campos/ SPThe main objective of this work was to accomplish the computational simulation in the software CadWind® of a filament winding for an applied pressure vase to motor rocket. The adopted simulation was of a non-geodesic helical winding, varying the winding angle in the cylindrical part of the pressure vessel, due the polar holes be different and the vessel long. Also simulations were accomplished varying the winding pattern. The results indicate that a more substantial winding pattern provides increased fiber deposition and distribution on the outer region of the domes.https://www.jatm.com.br/jatm/article/view/23Filament windingNon-geodesic windingPressure vesselMotor caseRocket.
spellingShingle Rafael F. Heitkoetter
Sérgio Frascino M. Almeida
Luís E. V. Loures da Costa
COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
Journal of Aerospace Technology and Management
Filament winding
Non-geodesic winding
Pressure vessel
Motor case
Rocket.
title COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
title_full COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
title_fullStr COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
title_full_unstemmed COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
title_short COMPUTATIONAL SIMULATION OF NON-GEODESIC FILAMENT WINDING OF PRESSURE VESSEL OF ROCKET MOTOR. doi: 10.5028/jatm.2009.0102185191
title_sort computational simulation of non geodesic filament winding of pressure vessel of rocket motor doi 10 5028 jatm 2009 0102185191
topic Filament winding
Non-geodesic winding
Pressure vessel
Motor case
Rocket.
url https://www.jatm.com.br/jatm/article/view/23
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AT sergiofrascinomalmeida computationalsimulationofnongeodesicfilamentwindingofpressurevesselofrocketmotordoi105028jatm20090102185191
AT luisevlouresdacosta computationalsimulationofnongeodesicfilamentwindingofpressurevesselofrocketmotordoi105028jatm20090102185191