Numerical Modeling of Inverse Problems under Uncertainty for Damage Detection in Aircraft Structures
Abstract
Structural health monitoring (SHM) is a competitive approach for damage detection, wherein online information is collected, compared with an existing database for the undamaged structure, and from this comparison, real-time information about the presence of damage is obtained, its location, length, speed of propagation, and, ultimately, the remaining operational life of the structural component. This study explores numerical models of inverse problems for damage detection under uncertainty in aircraft structures, which can later be part of an on-board system for structural health monitoring. The research includes modeling of the direct and inverse problems, and the related uncertainties.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 2013
- Accession Number
- ADA587627
Entities
People
- Ariosto B. Jorge
Organizations
- Federal University of Itajubá