materiais compósitos laminados computational project school … · computational project –...
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G 1 Aluno Nº 73872 Nome: Inês Filipa de Castro Machado Sales D´Ávila
Aluno Nº 74325 Nome: Inês Catarino Pereira Sapata
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 0º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 2 Aluno Nº 72924 Nome: Ana Mónica Carvalho Fidalgo
Aluno Nº 73769 Nome: Maria Margarida Malveiro Bento das Dores Cheira
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 5º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 3 Aluno Nº 76781 Nome: Miguel Ruiz Calle Lucas
Aluno Nº 76964 Nome: João Miguel Andrade Tudela Martins
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 10º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 4 Aluno Nº 75441 Nome: José Augusto Mendes Ribeiro
Aluno Nº 77025 Nome: Nuno de Sousa Mendes Moita
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 15º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 5 Aluno Nº 75195 Nome: João Maria de Afonseca Portela Roseira Muralha
Aluno Nº 76250 Nome: André Miguel Correia de Sousa
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 20º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 6 Aluno Nº 75687 Nome: Ana Catarina Garbacz Gomes
Aluno Nº 75873 Nome: Nuno Maria Mota Paiva de Andrada
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 25º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 7 Aluno Nº 73330 Nome: Daniel Firnhaber Beckers
Aluno Nº 83377 Nome: Francisco Miguel Ribeiro Mangerona
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 30º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 8 Aluno Nº 75709 Nome: Mariana Lopes Monho Nogueira Freire
Aluno Nº 75862 Nome: Marta Fernandes Pereira Bruxelas
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 35º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 9 Aluno Nº 75183 Nome: José Carlos Felismino Maia Carregado
Aluno Nº 75752 Nome: Diogo Ralha Portugal Bentes
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 40º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 10 Aluno Nº 72987 Nome: João Carlos Marques Correia
Aluno Nº 73144 Nome: Vasco Henrique Reis Franco
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 45º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 11 Aluno Nº 75497 Nome: José Pedro de Sousa Ferreira
Aluno Nº 76265 Nome: Carlos Filipe Lopes Ramos
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 50º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 12 Aluno Nº 73590 Nome: Ivo Miguel Delgado Rocha
Aluno Nº 76110 Nome: Beatriz Almeida Ferreira
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 55º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 13 Aluno Nº 73525 Nome: Pedro Miguel dos Santos Fernandes Marreiro
Aluno Nº 75463 Nome: Pedro Dinis Caseiro Jorge
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 65º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 14 Aluno Nº 85732 Nome: Javier Sánchez Bayona
Aluno Nº 85805 Nome: Ángela Lendinez Torres
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 60º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 15 Aluno Nº 85713 Nome: Simon Cartenet
Aluno Nº 85714 Nome: Francois Malestroit
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 70º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 16 Aluno Nº 85702 Nome: Giuseppe Landolfo
Aluno Nº 85744 Nome: Dario Aresta
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 75º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 17 Aluno Nº 85715 Nome: Jury Mura
Aluno Nº 85716 Nome: Emiliano Manfredonia
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 80º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 18 Aluno Nº 65224 Nome: Lourenço Rocheta de Almeida Fernandes
Aluno Nº 82122 Nome: Rui Filipe Tavares de Assis
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when 85º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 19 Aluno Nº 75393 Nome: José Miguel Matos de Araújo
Aluno Nº 75542 Nome: Marcelo António Borralho da Silveira
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -5º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 20 Aluno Nº 75194 Nome: Pedro Filipe Neves Ferreira Lobão da Cruz
Aluno Nº 75341 Nome: Ana Rita Afonso Rebelo
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -10º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 21 Aluno Nº 75345 Nome: Marta Duarte Lopes Gonçalves
Aluno Nº 75445 Nome: João Tiago Pinheiro Fernandes
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -15º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 22 Aluno Nº 68562 Nome: Valter Romeu Vunge Cachinhama
Aluno Nº 69806 Nome: Mykola Zaikin
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -20º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 23 Aluno Nº 75510 Nome: Jorge Miguel Relvas Cordeiro
Aluno Nº 75929 Nome: Eduardo Rebordão Pires
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -25º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 24 Aluno Nº 69334 Nome: Rodrigo Gaspar Pinto Ramos Correia
Aluno Nº 70416 Nome: Gonçalo Miguel Ramalho Brás Pereira
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -30º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 25 Aluno Nº 72634 Nome: Mariana Raposo Oliveira
Aluno Nº 75360 Nome: João Pedro da Fonseca Matos Pragana
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -35º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 26 Aluno Nº 64962 Nome: Diogo Carvalho Rodrigues
Aluno Nº 73480 Nome: Luís Guilherme Figueira Franco
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -40º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 27 Aluno Nº 85802 Nome: Beatriz Fernández-Criado Manjón
Aluno Nº 85946 Nome: Marius Auflem
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -45º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 28 Aluno Nº 85936 Nome: Federico Chueca Azlor
Aluno Nº 86062 Nome: Marvin Javier Angeles Loredo
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -50º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 29 Aluno Nº 67187 Nome: David de Almeida Correia Rodrigues de Melo
Aluno Nº 73643 Nome: Márcio Daniel Rosa Silva
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -55º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 30 Aluno Nº 75886 Nome: Gonçalo da Veiga França Rocha e Castro
Aluno Nº 85730 Nome: Sergio Fontestad Gómez
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -60º/10 and the
RVE is subjected to deformation boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.
G 31 Aluno Nº 73369 Nome: Carlos Francisco Libório Barreira
Aluno Nº 76325 Nome: Pedro Miguel Rodrigues da Costa Simões
Gonçalves
Materiais Compósitos Laminados
Computational project – School year 2016/2017
Consider the composite laminated plate used in the experimental project. Assume that each lamina of the laminated plate
is reinforced by long fibers, with the same volume fraction as in the experimental project, and can be modeled with the
cubic RVE whose cross section is shown in the figure.
Figure 1
1. Compute the equivalent properties using the classical simple expressions of Micro-Mechanics.
2. Using a Finite element program, compute the equivalent material properties assuming that the elastic strain
energy stored in the RVE is the same as the energy stored in the equivalent material, when -65º/10 and the
RVE is subjected to stress boundary conditions
3. Using the same analysis, compute the equivalent material properties using the relation between average stress
and average strain.
4. For the same RVE compute the same properties using PREMAT software.
5. For the laminated plate and for the different sets of properties, using a finite element code obtain:
a. The static solution for the same load situations as the experimental work. Compare the obtained results
with the experimental ones, both in deformation, stress and strain aspects. Find the maximum loading
that you can apply for any of the cases, using the same criteria as in the experimental work. Comment
and discuss the obtained results.
b. For the same loading cases, do a natural frequency analysis (first 10 frequencies) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
c. For the same loading cases, do a buckling load analysis (first 10 buckling loads) for each set of
equivalent properties. Compare and discuss the results. Whenever possible, compare with analytical
solutions.
Submit a report (2 students per group) with a maximum of 12 pages, where you show the formulations of the problems
to solve, figures and/or tables of all issues that you think are relevant to address. Comment all results, and present some
conclusions and a reference list. The first page of the report must be this page.