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Computational simulation of non-geodesic filament winding of pressure vessel of rocket motor

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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Autores principales: Rafael F. Heitkoetter, Sérgio Frascino M. Almeida, Luís E. V. Loures da Costa
Formato: Artigo
Lenguaje:Inglês
Publicado: Instituto de Aeronáutica e Espaço (IAE) 2009-06-01
Colección:Journal of Aerospace Technology and Management
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Acceso en línea:http://www.jatm.com.br/papers/vol1_n2/JATMv1n2_p185-191_Computational_simulation_of_non-geodesic_filament_winding_of_pressure_vessel_of_rocket_motor.pdf
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