Real-Time Damage Detection in an Airplane Wing During Wind Tunnel Testing Under Realistic Flight Conditions
Yoav Ofir, Uri Ben-Simon, Shay Shoham, Iddo Kressel, Bernardino Galasso, Umberto Mercurio, Antonio Concilio, Gianvito Apuleo, Jonathan Bohbot, Moshe Tur
TL;DR
A system detects airplane wing damage in real time during wind tunnel tests using fiber-optic sensors and statistical analysis.
Contribution
The novelty lies in real-time damage detection using FBG sensors and statistical methods in a realistic wind tunnel setting.
Findings
The Q measure successfully identified damage initiation and extent in real time.
Hotelling’s T-squared measure provided limited outcomes compared to the Q measure.
Adjustable damage was simulated by loosening lockable fasteners on the composite wing.
Abstract
A real-time structural health monitoring (SHM) system of an airplane composite wing with adjustable damage is reported, where testing under realistic flight conditions is carried out in the controllable and repeatable environment of an industrial wind tunnel. An FBG-based sensing array monitors a debonded region, whose compromised structural strength is regained by a set of lockable fasteners. Damage tunability is achieved by loosening some of or all these fasteners. Real-time analysis of the data collected involves Principal Component Analysis, followed by Hotelling’s T-squared and Q measures. With previously set criteria, real-time data collection and processing software can declare the structural health status as normal or abnormal. During testing, the system using the Q measure successfully identified the initiation of the damage and its extent, while the T-squared one returned…
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Taxonomy
TopicsStructural Health Monitoring Techniques · Ultrasonics and Acoustic Wave Propagation · Non-Destructive Testing Techniques