Anisotropic tertiary creep damage formulations have become an increasingly important prediction technique for high temperature components due to drives in the gas turbine industry for increased combustion chamber exit pressures, temperature, and the use of anisotropic materials such as metal matrix composites and directionally-solidified (DS) Ni-base superalloys. Typically, isotropic creep damage formulations are implemented for simple cases involving a uniaxial state of stress; however, these formulations can be further developed for multiaxial states of stress where materials are found to exhibit induced anisotropy. In addition, anisotropic materials necessitate a fully-developed creep strain tensor. This thesis describes the development of a new anisotropic tertiary creep damage formulation implemented in a general-purpose finite element analysis (FEA) software. Creep deformation and rupture tests are conducted on L, T, and 45°-oriented specimen of subject alloy DS GTD-111. Using the Kachanov-Rabotnov isotropic creep damage formulation and the optimization software uSHARP, the damage constants associated with the creep tests are determined. The damage constants, secondary creep, and derived Hill Constants are applied directly into the improved formulation. Comparison between the isotropic and improved anisotropic creep damage formulations demonstrates modeling accuracy. An examination of the off-axis creep strain terms using the improved formulation is conducted. Integration of the isotropic creep damage formulation provides time to failure predictions which are compared with rupture tests. Integration of the improved anisotropic creep damage produces time to failure predictions at intermediate orientations and any state of stress. A parametric study examining various states of stress, and materials orientations is performed to verify the flexibility of the improved formulation. A parametric exercise of the time to failure predictions for various levels of uniaxial stress is conducted.

La méthode d’imagerie la plus répandue dans l’industrie pétrolière est la RTM (Reverse Time Migration) qui repose sur la simulation de la propagation des ondes dans le sous-sol. Nous nous sommes concentrés sur un propagateur d'ondes élastiques 3D en milieu anisotrope de type TTI (Tilted Transverse Isotropic). Nous avons directement travaillé dans le code de recherche de Total DIVA (Depth Imaging Velocity Analysis), basé sur une discrétisation par la méthode de Galerkin Discontinue et le schéma Leap-Frog, et développé pour le calcul parallèle intensif – HPC (High Performance Computing). Nous avons ciblé plus particulièrement deux contributions possibles qui, si elles supposent des compétences très différentes, ont la même finalité : réduire les coûts de calculs requis pour la simulation. D'une part, les conditions aux limites classiques de type PML (Perfectly Matched Layers) ne sont pas stables dans des milieux TTI. Nous avons proposé de formuler une CLA (Conditions aux Limites Absorbantes) stable dans des milieux anisotropes. La méthode de construction repose sur les propriétés des courbes de lenteur, ce qui donne à notre approche un caractère original. D'autre part, le parallélisme initial, basé sur une décomposition de domaine et des communications par passage de messages à l'aide de la bibliothèque MPI, conduit à un déséquilibrage de charge qui détériore son efficacité parallèle. Nous avons corrigé cela en remplaçant le paradigme parallélisme par l'utilisation de la programmation à base de tâches sur support d'exécution. Cette thèse a été réalisée dans le cadre de l'action de recherche DIP (Depth Imaging Partnership) qui lie la compagnie pétrolière Total et Inria. / The most common method of Seismic Imaging is the RTM (Reverse Time Migration) which depends on wave propagation simulations in the subsurface. We focused on a 3D elastic wave propagator in anisotropic media, more precisely TTI (Tilted Transverse Isotropic). We directly worked in the Total code DIVA (Depth Imaging Velocity Analysis) which is based on a discretization by the Discontinuous Galerkin method and the Leap-Frog scheme, and developed for intensive parallel computing – HPC (High Performance Computing). We choose to especially target two contributions. Although they required very different skills, they share the same goal: to reduce the computational cost of the simulation. On one hand, classical boundary conditions like PML (Perfectly Matched Layers) are unstable in TTI media. We have proposed a formulation of a stable ABC (Absorbing Boundary Condition) in anisotropic media. The technique is based on slowness curve properties, giving to our approach an original side. On the other hand, the initial parallelism, which is based on a domain decomposition and communications by message passing through the MPI library, leads to load-imbalance and so poor parallel efficiency. We have fixed this issue by replacing the paradigm for parallelism by the use of task-based programming through runtime system. This PhD thesis have been done in the framework of the research action DIP (Depth Imaging Partnership) between the Total oil company and Inria.

The topic of this thesis is the numerical simulation of transversely isotropic 3D structures and laminates by means of the adaptive finite element method. To achieve this goal, the theoretical background of elastic deformation problems, transverse isotropy, plate theory, and the classical laminate theory is recapitulated. The classical laminate theory implies a combination of the membrane problem and the plate problem with additional coupling terms. The focus of this work is the adjustment of two integral parts of the adaptive FE algorithm according to the classical laminate theory. One of these parts is the solution of the FE system; a good preconditioner is needed in order to use the conjugate gradient method efficiently. It is shown via a spectral equivalence bound that the combination of existing preconditioners for the membrane and plate problems poses a capable preconditioner for the combined laminate problem. The other part is the error estimation process; the error estimator determines where the current mesh has to be refined for the next step. Existing results on residual error estimators for the elasticity problem, the biharmonic problem, and the plate problem are combined and extended to obtain a posteriori local residual error indicators for the classical laminate theory problem. The effectiveness of both results is demonstrated by numerical examples.

The topic of this thesis is the numerical simulation of transversely isotropic 3D structures and laminates by means of the adaptive finite element method. To achieve this goal, the theoretical background of elastic deformation problems, transverse isotropy, plate theory, and the classical laminate theory is recapitulated. The classical laminate theory implies a combination of the membrane problem and the plate problem with additional coupling terms. The focus of this work is the adjustment of two integral parts of the adaptive FE algorithm according to the classical laminate theory. One of these parts is the solution of the FE system; a good preconditioner is needed in order to use the conjugate gradient method efficiently. It is shown via a spectral equivalence bound that the combination of existing preconditioners for the membrane and plate problems poses a capable preconditioner for the combined laminate problem. The other part is the error estimation process; the error estimator determines where the current mesh has to be refined for the next step. Existing results on residual error estimators for the elasticity problem, the biharmonic problem, and the plate problem are combined and extended to obtain a posteriori local residual error indicators for the classical laminate theory problem. The effectiveness of both results is demonstrated by numerical examples.:1 Introduction 1.1 Motivation 1.2 Organisation of this work 1.3 Notation and basic definitions 2 Basic theory of 3D simulation 2.1 Differential geometry 2.1.1 Initial and deformed domain 2.1.2 Strain tensor 2.2 Energy functional 2.2.1 Linearly elastic material law 2.2.2 Equilibrium of forces 2.2.3 Large deformations 2.2.4 Small deformations 2.3 Voigt notation and elasticity matrix 3 Transversely isotropic material law 3.1 Elasticity tensor 3.2 Conversion of the material constants 3.3 Elasticity matrix 3.4 Eigenvalues 3.5 State of plane strain 3.6 State of plane stress 4 Plate theory and classical laminate theory 4.1 The Kirchhoff–Love hypothesis 4.2 Constitutive law and bilinear form of the laminated plate 4.3 Definition of resultants 4.4 Boundary conditions 4.5 From the equilibrium conditions to the weak formulation 4.5.1 Membrane equilibrium 4.5.2 Plate equilibrium 4.5.3 Combined weak formulation 4.5.4 The CLT problem in Voigt notation 5 Discretisation 5.1 Short introduction to FEM 5.2 Adaptive FEM 5.3 Finite elements for 3D elasticity problems 5.4 Finite elements for plates 5.4 Finite elements for plates 5.4.1 BFS rectangles 5.4.2 rHCT triangles 5.5 CLT elements 5.5.1 Rectangles 5.5.2 Triangles 6 Solver and preconditioner 6.1 The preconditioned conjugate gradient method 6.2 Hierarchical basis and BPX preconditioners 6.3 Preconditioning of CLT problems 6.3.1 General laminates 6.3.2 Some special cases and examples 7 A posteriori residual error estimation 7.1 Residual error estimator for 3D elements 7.2 Residual error estimator for plate and CLT elements 7.2.1 Auxiliary definitions and assumptions on the mesh 7.2.2 Interpolation operators 7.2.3 Important inequalities 7.2.4 Cut-off functions 7.2.5 Definition of the error 7.2.6 Reliability inequality 7.2.7 Efficiency inequality 8 Some details of the implementation 8.1 The adaptive FE package SPC-PM 8.2 Remarks on some added features 8.2.1 Capability of the current code 8.2.2 Cuntze’s failure mode concept 8.3 Coordinate transformation of higher-order derivatives 8.3.1 Mapping of coordinates 8.3.2 Transformation of derivatives of up to the third-order 8.3.3 Recursive construction of transformation matrices 8.3.4 Simplification for axis-parallel rectangles 9 Numerical examples 9.1 A three-dimensional example from eniPROD 9.2 Example problems for laminates 9.2.1 Rectangular plate under in-plane load 9.2.2 Rectangular plate under vertical load 9.2.3 L-shaped plate with inhomogeneous natural boundary conditions 10 Conclusion and outlook Bibliography Acknowledgements List of main symbols Theses