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...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Instituto de Aeronáutica e Espaço (IAE)
2011-07-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | https://www.jatm.com.br/jatm/article/view/23 |