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.

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Page 1: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 2: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 3: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 4: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 5: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 6: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 7: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 8: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 9: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 10: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 11: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 12: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 13: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 14: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 15: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 16: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 17: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 18: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 19: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 20: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 21: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 22: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 23: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 24: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 25: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 26: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 27: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 28: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 29: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 30: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.

Page 31: Materiais Compósitos Laminados Computational project School … · Computational project – School year 2016/2017 Consider the composite laminated plate used in the experimental

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.