A finite element cure model and cure cycle optimization for composite structures
A one-dimensional cylindrical cure model was developed to describe the curing process of an axisymmetric filament wound composite structure. For a specified cure cycle, the cure model can be used to calculate the temperature distribution, the degree of cure of the resin, and the resin viscosity insi...
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ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-423342021-05-22T05:27:18Z A finite element cure model and cure cycle optimization for composite structures Somanath, Nagendra Engineering Mechanics LD5655.V855 1987.S622 Composite materials Fibrous composites A one-dimensional cylindrical cure model was developed to describe the curing process of an axisymmetric filament wound composite structure. For a specified cure cycle, the cure model can be used to calculate the temperature distribution, the degree of cure of the resin, and the resin viscosity inside the composite case. Solutions to the cylindrical cure model were obtained numerically using the finite element technique. The cylindrical cure model was verified by measuring the temperature distribution in a small 5.75 inch graphite - epoxy test bottle. The data were compared with the results calculated with the computer code for conditions employed in the tests. Good agreement was found between the data and the results of the computer code. The error between the experimental data and the results of the computer code was less than 10 %. A cure cycle optimization problem is formulated for the curing process using a calculus of variations approach. The optimum cure cycle should tailor the temperature in the composite such that a uniform temperature and degree of cure distribution is achieved in the composite while minimizing the reaction exotherms and thermal lag. Cure simulations of an one inch thick graphite - epoxy composite case predict a minimization of the reaction exotherms and the thermal lag. The the final process time needed to achieve uniform degree of cure and uniform temperature distribution in the composite is also predicted. The resultant cure cycle appears to approach the boundary temperatures specified as limits on the cure cycle temperature. Master of Science 2014-03-14T21:34:59Z 2014-03-14T21:34:59Z 1987 2010-04-27 2010-04-27 2010-04-27 Thesis Text etd-04272010-020304 http://hdl.handle.net/10919/42334 http://scholar.lib.vt.edu/theses/available/etd-04272010-020304/ OCLC# 17604767 LD5655.V855_1987.S622.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ xii, 191 leaves BTD application/pdf application/pdf Virginia Tech |
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LD5655.V855 1987.S622 Composite materials Fibrous composites |
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LD5655.V855 1987.S622 Composite materials Fibrous composites Somanath, Nagendra A finite element cure model and cure cycle optimization for composite structures |
description |
A one-dimensional cylindrical cure model was developed to describe the curing process of an axisymmetric filament wound composite structure. For a specified cure cycle, the cure model can be used to calculate the temperature distribution, the degree of cure of the resin, and the resin viscosity inside the composite case. Solutions to the cylindrical cure model were obtained numerically using the finite element technique.
The cylindrical cure model was verified by measuring the temperature distribution in a small 5.75 inch graphite - epoxy test bottle. The data were compared with the results calculated with the computer code for conditions employed in the tests. Good agreement was found between the data and the results of the computer code. The error between the experimental data and the results of the computer code was less than 10 %.
A cure cycle optimization problem is formulated for the curing process using a calculus of variations approach. The optimum cure cycle should tailor the temperature in the composite such that a uniform temperature and degree of cure distribution is achieved in the composite while minimizing the reaction exotherms and thermal lag.
Cure simulations of an one inch thick graphite - epoxy composite case predict a minimization of the reaction exotherms and the thermal lag. The the final process time needed to achieve uniform degree of cure and uniform temperature distribution in the composite is also predicted. The resultant cure cycle appears to approach the boundary temperatures specified as limits on the cure cycle temperature. === Master of Science |
author2 |
Engineering Mechanics |
author_facet |
Engineering Mechanics Somanath, Nagendra |
author |
Somanath, Nagendra |
author_sort |
Somanath, Nagendra |
title |
A finite element cure model and cure cycle optimization for composite structures |
title_short |
A finite element cure model and cure cycle optimization for composite structures |
title_full |
A finite element cure model and cure cycle optimization for composite structures |
title_fullStr |
A finite element cure model and cure cycle optimization for composite structures |
title_full_unstemmed |
A finite element cure model and cure cycle optimization for composite structures |
title_sort |
finite element cure model and cure cycle optimization for composite structures |
publisher |
Virginia Tech |
publishDate |
2014 |
url |
http://hdl.handle.net/10919/42334 http://scholar.lib.vt.edu/theses/available/etd-04272010-020304/ |
work_keys_str_mv |
AT somanathnagendra afiniteelementcuremodelandcurecycleoptimizationforcompositestructures AT somanathnagendra finiteelementcuremodelandcurecycleoptimizationforcompositestructures |
_version_ |
1719405515838062592 |