Shay Shoam

Mr. Shay Shoam


Research Focus & Metrics

Academic Career Length

4Years (2023-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 January 2023 in Sensors
Verified
Journal Article
Open access
PDF file
Monica CiminelloMonica Ciminello
Monica Ciminello
BSBogdan Sikorski
Bogdan Sikorski
BGBernardino Galasso
Bernardino Galasso
LPLorenzo Pellone
Lorenzo Pellone
UMUmberto Mercurio
Umberto Mercurio
MTMoshe Tur
Moshe Tur
The present paper reports the outcomes of activities concerning a real-time SHM system for debonding flaw detection based on ground testing of an aircraft structural component as a basis for condition-based maintenance. In this application, a damage detection method unrelated to structural or load models is investigated. In the reported application, the system is applied for real-time detection of two flaws, kissing bond type, artificially deployed over a full-scale composite spar under the action of external bending loads. The proposed algorithm, local high-edge onset (LHEO), detects damage as an edge onset in both the space and time domains, correlating current strain levels to next strain levels within a sliding inner product proportional to the sensor step and the acquisition time interval, respectively. Real-time implementation can run on a consumer-grade computer. The SHM algorithm was written in Matlab and compiled as a Python module, then called from a multiprocess wrapper code with separate operations for data reception and data elaboration. The proposed SHM system is made of FBG arrays, an interrogator, an in-house SHM code, an original decoding software (SW) for real-time implementation of multiple SHM algorithms and a continuous interface with an external operator.

16 July 2025 in Sensors
Verified
Journal Article
Open access
PDF file
YOYoav Ofir
Yoav Ofir
UBUri Ben-Simon
Uri Ben-Simon
SSShay Shoam
Shay Shoam
IKIddo Kressel
Iddo Kressel
BGBernardino Galasso
Bernardino Galasso
MTMoshe Tur
Moshe Tur
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 limited outcomes.