STRUCTURAL HEALTH MONITORING IN AEROSPACE STRUCTURES: CURRENT INSPECTION METHODS, TECHNOLOGIES, AND FUTURE TRENDS
in: International Research in the Field of Aerospace Engineering, ASSOC. PROF. DR. HAŞIM KAFALI, Editor, Eğitim Yayınevi, İstanbul, pp.15-39, 2025
- Publication Type: Book Chapter / Chapter Research Book
- Publication Date: 2025
- Publisher: Eğitim Yayınevi
- City: İstanbul
- Page Numbers: pp.15-39
- Editors: ASSOC. PROF. DR. HAŞIM KAFALI, Editor
- Eskisehir Osmangazi University Affiliated: Yes
Abstract
1. INTRODUCTION
1.1 Damage and Safety Requirements in Aerospace Structures
Aerospace structures are subjected to variable and strenuous loading conditions throughout their
operational lifespans (Boller, 2008; Payne, 1976) Cyclic mechanical loads during flight, thermal
cycling, humidity, and corrosive environments can lead to critical defects, particularly in
metallic and composite structures. These include fatigue cracks, delamination, fastener
failures, and Barely Visible Impact Damage (BVID). (Diamanti & Soutis, 2010a; Qinetiq, 2012) Such
damage types pose significant risks to flight safety by directly compromising structural
integrity.(Seneviratne & Tomblin, 2010)
Traditional aviation maintenance philosophy relies on periodic inspections performed at specific
flight hour intervals or cycle counts (Aviation Rulemaking Advisory Committee (ARAC), 2024; “New
Materials for Next-Generation Commercial Transports,” 1996). However, the increasing use of
composite materials in modern aircraft, coupled with complex geometries and high operational
tempos, has highlighted the limitations of conventional maintenance in terms of cost, time, and
accessibility. (Muñoz, n.d.) This shift has necessitated the development of more continuous,
automated, and real-time monitoring approaches (Cusati
et al., 2022; Diamanti & Soutis, 2010b)