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Quantification of Processing Effects on Filament Wound Pressure VesselsA computational simulation procedure is described which is designed specifically for the modeling and analysis of filament wound pressure vessels. Cylindrical vessels with spherical or elliptical end caps can be generated automatically. End caps other than spherical or elliptical may be modeled by varying circular sections along the x-axis according to the end cap shape. The finite element model generated is composed of plate type quadrilateral shell elements on the entire vessel surface. This computational procedure can also be used to generate grid, connectivity and material cards (bulk data) for component parts of a larger model. These bulk data are assigned to a user designated file for finite element structural/stress analysis of composite pressure vessels. The procedure accommodates filament wound pressure vessels of all types of shells-of -revolution. It has provisions to readily evaluate initial stresses due to pretension in the winding filaments and residual stresses due to cure temperature.
Document ID
20020061253
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Aiello, Robert A.
(Modern Technologies Corp. Middleburg Heights, OH United States)
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2002
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-1999-209434/REV1
NAS 1.15:209434/REV1
E-11899-1/REV1
Funding Number(s)
PROJECT: RTOP 523-22-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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