The fatigue life prediction of high pressure turbine blades may require a damage tolerance approach based on the study of possible crack propagation. The nonlinear behavior of the material under complex nonproportional loadings and the high cost of running long and expensive elastic-plastic FE computations on complex 3D structures over millions of cycles are some major issues that may encounter this type of approach.Within this context, an incremental model was proposed based on plasticity as a main mechanism for fatigue crack growth.A model reduction strategy using the Proper Orthogonal Decomposition (POD) was used to reduce the cost of FEA. Based on a set of hypotheses, the number of the degrees of freedom of the problem is reduced drasti...
This PhD project aims at assessing the capabilities associated with the local approach to fracture t...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
This work aims to propose a method to estimate plasticity from two structural analyses in elasticity...
The fatigue life prediction of high pressure turbine blades may require a damage tolerance approach ...
Les aubes des turbines à haute pression des réacteurs d'avion subissent des chargements complexes da...
Single crystal components operating at elevated temperatures are subjected to severe thermomechanica...
The field of mechanics, particularly micromechanics, has undergone great developments. It is well kn...
The AM1 superalloy blades of aeronautical High Pressure turbines are cooled by a complex system of m...
The main goal of this dissertation was to develop a model to simulate the processes of crack bifurca...
International audienceIn the aeronautical field, fatigue crack propagation analysis is commonly perf...
The blade-disc fixings of an aircraft engine are subjected to complex loadings composed by a high pr...
Maître de thèse : Pierre-Olivier BouchardThe aim of this thesis is to develop an accurate numerical ...
High pressure turbine blades in aerojet engines are component that undergo severe thermo-mechanical ...
Il est connu depuis des décennies que la propagation des fissures de fatigue dans les matériaux élas...
Predicting the growth of fatigue cracks under multi-axial loading conditions still remains very diff...
This PhD project aims at assessing the capabilities associated with the local approach to fracture t...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
This work aims to propose a method to estimate plasticity from two structural analyses in elasticity...
The fatigue life prediction of high pressure turbine blades may require a damage tolerance approach ...
Les aubes des turbines à haute pression des réacteurs d'avion subissent des chargements complexes da...
Single crystal components operating at elevated temperatures are subjected to severe thermomechanica...
The field of mechanics, particularly micromechanics, has undergone great developments. It is well kn...
The AM1 superalloy blades of aeronautical High Pressure turbines are cooled by a complex system of m...
The main goal of this dissertation was to develop a model to simulate the processes of crack bifurca...
International audienceIn the aeronautical field, fatigue crack propagation analysis is commonly perf...
The blade-disc fixings of an aircraft engine are subjected to complex loadings composed by a high pr...
Maître de thèse : Pierre-Olivier BouchardThe aim of this thesis is to develop an accurate numerical ...
High pressure turbine blades in aerojet engines are component that undergo severe thermo-mechanical ...
Il est connu depuis des décennies que la propagation des fissures de fatigue dans les matériaux élas...
Predicting the growth of fatigue cracks under multi-axial loading conditions still remains very diff...
This PhD project aims at assessing the capabilities associated with the local approach to fracture t...
The creep of high pressure turbine blades is a critical issue for the certification of a helicopter ...
This work aims to propose a method to estimate plasticity from two structural analyses in elasticity...