• Aucun résultat trouvé

Advanced damage tolerance and risk assessment methodology and tool for aircraft structures containing MSD/MED

N/A
N/A
Protected

Academic year: 2021

Partager "Advanced damage tolerance and risk assessment methodology and tool for aircraft structures containing MSD/MED"

Copied!
11
0
0

Texte intégral

Loading

Figure

Fig. 1. CC-130 centre wing box
Fig. 2. β-factors of a crack growing in an  infinite plate with arbitrarily located stringers  2.3 NRC Generic FE-based Beta Tool
Fig. 3. Screenshot of the generic FE-base beta  tool for a stiffened panel configuration
Fig. 5. MSD crack scenario
+6

Références

Documents relatifs

The model predicts the evolutions of the plastic intensity factor under variable amplitude and non-proportional mixed mode conditions, and the plasticity rates pre- dicted by

The initial size of the fine scale region in the AMM boundaries is decided based on the following conditions: The refinement algorithm is activated sufficiently often such that a

For examples, two-dimensional (2D) Green functions for a magnetoelectro- elastic anisotropic medium with an elliptical cavity or rigid inclusion (Chung and Ting, 1995),

The author’s experience was concerning a calculus required by a method for determining the thermal diffusivity, based on the measurement of the thermal expansion of a

According to the size effect, small cap securities generally generate greater returns than those of large cap securities.. Recent studies have however suggested that for

To be in line with the new development agenda the identification criteria relating to structural handicaps could take into account not only the economic vulnerability as presently

Thirdly, our results illustrate the importance of so-called nonspecific binding events, and the importance of taking care of them as was indeed recognized by other investigators

In order to analyse the burst dynamics of the interfacial crack propagation and define rupture quakes, the fracture front lines extracted from image processing are added to form