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Modeling and Optimization of Materials and Structures

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This is an author-deposited version published in: http://oatao.univ-toulouse.fr/ Eprints ID: 13846

To cite this version:

Karama, Moussa and Borouchaki, Houman and Cherouat, Abel and El Hami, Abdelkhalak Modeling and Optimization of Materials and

Structures. (2015) In: Modeling and Optimization of Materials and

Structures. Trans Tech Publications. ISBN 978-3-03935-424-6

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OATAO is an open access repository that collects the work of Toulouse researchers and makes it freely available over the web where possible.

Any correspondence concerning this service should be sent to the repository administrator: staff-oatao@listes-diff.inp-toulouse.fr

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Modeling and Optimization

of Materials and Structures

Edited by M. Karama H. Borouchaki A. Cherouat A. EL Hami

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Modeling and Optimization of

Materials and Structures

Special topic volume with invited peer reviewed papers only

Edited by

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Preface

The current economic and ecological context requires different industries towards the optimization of structures. One of the most striking examples is the soaring price of oil, which launched the major aircraft manufacturers Airbus and Boeing in a race to relief structures, to reduce their consumption. Therefore, the need of competitive products, both in terms of reliability, performance or operating cost, is pervasive and growing, aviation and elsewhere. Thus, work on the material parts by offering innovative solutions to reduce their weight and improve their performance (new materials, new processes, etc.) is essential and becomes more than ever a major industrial challenge. One way of increasing the selected aircraft is use of composite materials. Indeed, their high ratio mechanical / density properties and excellent resistance to environmental significantly improve the structural performance of the aircraft while generating a significant weight gain (20 to 30% weight of a structure). They were originally implemented in the design of secondary structures of aircraft, but improving their manufacturing processes and a better understanding of their mechanical properties and their degradation mechanisms are they now used for the manufacture of primary structures, such as the fuselage or the central box of an aircraft wing. If applications were rather the military origin, composites now particularly interested in civil aviation, the constraints are much stricter certification, which requires predictability of behavior and life of structures much finer Thus, at present, they account for over 50% of the mass of newer aircraft such as the Airbus A350, the Airbus A380 or the Boeing 787.

The potential of composite materials is important, but will speak only on one condition: work not only on the basic constituents of the material (fibers, resin, ...) on the injection preparation conditions (methods,

thermal cycle, shaped in the mold, ...) but also and above all on the function of the material in the structure. Indeed, the material is a component of a more complex system, consisting of parts, assemblies, subassemblies and the structure itself. This vision system involves understanding the material as parameters, not data, an overall optimization of the structure. This link between material and structure is evident for composites where fiber orientation, or reinforcements in a more general way, in the direction of efforts can greatly increase the performance / weight ratio. We understand that optimizing the structure requires, among other things, a design material to locally respond to the "just need" structural.

The main objectives of this special issue (consisting mainly of a selection of papers presented at 5th

International Symposium on AirCraft MAterials ACMA 2014) are, by means of modeling strategies and simulation out with conventional strategies, pushing the current limits in modeling and computation in response industrial and societal challenges. It is also to control the calculations and models in a framework that takes into account the major sources of uncertainty to optimize materials and structures. Particular attention is made to the modeling and validation of composite materials and structures.

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Table of Contents

Preface v

Fatigue Behavior of Aerospace Al-Cu, Al-Li and Al-Mg-Si Sheet Alloys

N.D. Alexopoulos, V. Migklis, S.K. Kourkoulis and Z. Marioli-Riga ... 1

Experimental and Numerical Study of Interfacial Fracture Parameters of a Brazed Joints

A. Baazaoui, T. Fourcade, O. Dalverny, J. Alexis and M. Karama ... 9

3D Remeshing Simulation of Aluminum Foams Behavior under Static Load

S.J. Zhu, A. Cherouat, H. Borouchaki and X.L. Gong ... 17

Numerical Simulation of Composite Hemp Fibers Behavior for Aircraft Application

A. Cherouat, G. Montay and F. Ilczyszyn ... 25

Modeling the Residual Stress in Woven Thermoset Composites Parts for Aerospace Applications Using Finite Element Methods

Y. Nawab, C.H. Park, A. Saouab, R. Agogué and P. Beauchêne ... 32

Concept of the Tip Effect in Single Walled Carbon Nanotube

K. El-Hami and A. El-Hami... 37

Nanocomposite Based Carbon Nanotubes for Electromechanical Application

K. El-Hami and A. El-Hami... 41

Numerical Modeling of the Flow of Particle-Filled Resin through a Dual Scale Fibrous Media

H. Haji and A. Saouab ... 44

Analysis of the Hydroforming Process Using Metamodels

A. El Hami and B. Radi ... 52

Weldability of Superalloys Hastelloy X by Yb: YAG Laser

J. Graneix, J.D. Beguin, J. Alexis and T. Masri ... 61

A New Parameter Identification Approach by Experimental Design and Multiple Regressions Method: Application to the Elastoplastic Damage Constitutive Law of a Steel Thin Parts

M.T. Nasri, S. Faouzi, M.A. Rezgui, M. Ayadi and A. Cherouat ... 71

Thermo-Viscoelastic Modeling of the Aircraft Tire Cornering

I. Rosu, L. Elias-Birembaux and F. Lebon ... 80

Reliability Study of a Coupled Three-Dimensional System with Uncertain Parameters

R. El Maani, B. Radi and A. El Hami ... 87

Reliability Based Design Optimization Framework for Boat Propeller

A. Makhloufi, M. Mansouri, B. Radi and A. El Hami ... 94

Hybrid Evolutionary Optimization Algorithm for Structures

N. El Hami, M. Itmi and A. El Hami ... 102

Simulation and Optimization of an Actuator

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Thick Composite Structures under a Load Pinch

M. Karama ... 120

Stress Reduction in Bone/Dental Implant Interface Using Elastomeric Stress Absorbers

A. Belarbi, B. Mansouri, G. Mehdi, M. Belhouari and Z. Azari ... 129

A New Reverse Engineering Method for the 3D Surface Reconstruction without Contact

L. Giraud-Moreau, R. Slysz and H. Borouchaki ... 140

Keyword Index ... 147 Author Index ... 149

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