Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites

Autoclave processing of large scale, one-piece structural parts made of carbon fiber-reinforced polymer composite materials is the key to decreasing manufacturing costs while at the same time increasing quality. Nonetheless, even in manufacturing simple flat parts, residual strains and stresses are...

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Main Author: Osooly, Amir
Format: Others
Language:English
Published: University of British Columbia 2008
Subjects:
Online Access:http://hdl.handle.net/2429/747
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spelling ndltd-UBC-oai-circle.library.ubc.ca-2429-7472018-01-05T17:22:44Z Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites Osooly, Amir Composite material Large deformation and stain Autoclave processing of large scale, one-piece structural parts made of carbon fiber-reinforced polymer composite materials is the key to decreasing manufacturing costs while at the same time increasing quality. Nonetheless, even in manufacturing simple flat parts, residual strains and stresses are unavoidable. For structural design purposes and to aid in the assembly procedures, it is desirable to have proven numerical tools that can be used to predict these residual geometrical and material properties in advance, thus avoid the costly experimental trial and error methods. A 2-D finite element-based code, COMPRO, has previously been developed in-house for predicting autoclave process-induced deformations and residual stresses in composite parts undergoing an entire cure cycle. To simulate the tool-part interaction, an important source of residual deformations/stresses, COMPRO used a non-zero thickness elastic shear layer as its only interface option. Moreover, the code did not account for the large deformations and strains and the resulting nonlinear effects that can arise during the early stages of the cure cycle when the material is rather compliant. In the present work, a contact surface employing a penalty method formulation is introduced at the tool-part interface. Its material-dependent parameters are a function of temperature, degree of cure, pressure and so forth. This makes the stick-slip condition plus separation between the part and the tool possible. The large displacements/rotations and large shear strains that develop at the early stages of the cure cycle when the resin has a very low elastic modulus provided the impetus to include a large strain/deformation option in COMPRO. A new “co-rotational stress formulation” was developed and found to provide a robust method for numerical treatment of very large deformation/strain problems involving anisotropic materials of interest here. Several verification and validation examples are used to calibrate the contact interface parameters and to demonstrate the correctness of implementation and the accuracy of the proposed method. A number of comparisons are made with exact solutions, other methods, other experiments and the same models in other commercial codes. Finally, several interesting cases are examined to explore the results of COMPRO predictions with the added options. Applied Science, Faculty of Civil Engineering, Department of Graduate 2008-04-21T16:43:03Z 2008-04-21T16:43:03Z 2008 2008-05 Text Thesis/Dissertation http://hdl.handle.net/2429/747 eng Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/ 2877851 bytes application/pdf University of British Columbia
collection NDLTD
language English
format Others
sources NDLTD
topic Composite material
Large deformation and stain
spellingShingle Composite material
Large deformation and stain
Osooly, Amir
Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
description Autoclave processing of large scale, one-piece structural parts made of carbon fiber-reinforced polymer composite materials is the key to decreasing manufacturing costs while at the same time increasing quality. Nonetheless, even in manufacturing simple flat parts, residual strains and stresses are unavoidable. For structural design purposes and to aid in the assembly procedures, it is desirable to have proven numerical tools that can be used to predict these residual geometrical and material properties in advance, thus avoid the costly experimental trial and error methods. A 2-D finite element-based code, COMPRO, has previously been developed in-house for predicting autoclave process-induced deformations and residual stresses in composite parts undergoing an entire cure cycle. To simulate the tool-part interaction, an important source of residual deformations/stresses, COMPRO used a non-zero thickness elastic shear layer as its only interface option. Moreover, the code did not account for the large deformations and strains and the resulting nonlinear effects that can arise during the early stages of the cure cycle when the material is rather compliant. In the present work, a contact surface employing a penalty method formulation is introduced at the tool-part interface. Its material-dependent parameters are a function of temperature, degree of cure, pressure and so forth. This makes the stick-slip condition plus separation between the part and the tool possible. The large displacements/rotations and large shear strains that develop at the early stages of the cure cycle when the resin has a very low elastic modulus provided the impetus to include a large strain/deformation option in COMPRO. A new “co-rotational stress formulation” was developed and found to provide a robust method for numerical treatment of very large deformation/strain problems involving anisotropic materials of interest here. Several verification and validation examples are used to calibrate the contact interface parameters and to demonstrate the correctness of implementation and the accuracy of the proposed method. A number of comparisons are made with exact solutions, other methods, other experiments and the same models in other commercial codes. Finally, several interesting cases are examined to explore the results of COMPRO predictions with the added options. === Applied Science, Faculty of === Civil Engineering, Department of === Graduate
author Osooly, Amir
author_facet Osooly, Amir
author_sort Osooly, Amir
title Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
title_short Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
title_full Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
title_fullStr Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
title_full_unstemmed Development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
title_sort development and implementation of robust large deformation and contact mechanics capabilities in process modelling of composites
publisher University of British Columbia
publishDate 2008
url http://hdl.handle.net/2429/747
work_keys_str_mv AT osoolyamir developmentandimplementationofrobustlargedeformationandcontactmechanicscapabilitiesinprocessmodellingofcomposites
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