Ultrasonic Characterization of the Fiber-Matrix Interfacial Bond in Aerospace Composites
Joint Authors
Aggelis, D.
Kleitsa, D.
Matikas, Theodore E.
Source
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-8, 8 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-06-27
Country of Publication
Egypt
No. of Pages
8
Main Subjects
Medicine
Information Technology and Computer Science
Abstract EN
The properties of advanced composites rely on the quality of the fiber-matrix bonding.
Service-induced damage results in deterioration of bonding quality, seriously compromising the load-bearing capacity of the structure.
While traditional methods to assess bonding are destructive, herein a nondestructive methodology based on shear wave reflection is numerically investigated.
Reflection relies on the bonding quality and results in discernable changes in the received waveform.
The key element is the “interphase” model material with varying stiffness.
The study is an example of how computational methods enhance the understanding of delicate features concerning the nondestructive evaluation of materials used in advanced structures.
American Psychological Association (APA)
Aggelis, D.& Kleitsa, D.& Matikas, Theodore E.. 2013. Ultrasonic Characterization of the Fiber-Matrix Interfacial Bond in Aerospace Composites. The Scientific World Journal،Vol. 2013, no. 2013, pp.1-8.
https://search.emarefa.net/detail/BIM-1032581
Modern Language Association (MLA)
Aggelis, D.…[et al.]. Ultrasonic Characterization of the Fiber-Matrix Interfacial Bond in Aerospace Composites. The Scientific World Journal No. 2013 (2013), pp.1-8.
https://search.emarefa.net/detail/BIM-1032581
American Medical Association (AMA)
Aggelis, D.& Kleitsa, D.& Matikas, Theodore E.. Ultrasonic Characterization of the Fiber-Matrix Interfacial Bond in Aerospace Composites. The Scientific World Journal. 2013. Vol. 2013, no. 2013, pp.1-8.
https://search.emarefa.net/detail/BIM-1032581
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1032581