Damage Diagnostics Utilizing Sensor Data Fusion

Poster (2020)

Authors

Agnes A.R. Broer Structural Integrity & Composites - Aerospace Engineering
D. Zarouchas Structural Integrity & Composites - Aerospace Engineering
R. Benedictus Structural Integrity & Composites - Aerospace Engineering
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
Copyright: © 2020 Agnes A.R. Broer, D. Zarouchas, R. Benedictus
More Info
expand_more

Published Date

2020

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites

Abstract

Experimental campaign to develop a multi-sensing structural health monitoring (SHM) framework in order to diagnose impact damage in stiffened composite aircraft structures on all four SHM levels, namely 1) detection, 2) localisation, 3) type, and 4) severity.

Poster_Broer.jpg

Poster_Broer.jpg

Files

Poster_Broer.jpg
(jpg | 1.12 Mb)
Unknown license