Damage Detection Analysis Using Lamb Waves in Restricted Geometry for Aerospace Applications - Softcover

Underwood, Roman T

Softcover

ISBN 10: 1288397194 ISBN 13: 9781288397198

Publisher: BiblioBazaar, LLC, 2012

Synopsis

A goal of structural health monitoring (SHM) is to increase aircraft readiness through condition based maintenance (i.e. servicing an aircraft only when it is known to be necessary). The lead ziconate titanate (PZT) is a commonly used piezoelectric transducer that has shown potential to detect damage in aircraft structures without time consuming manual inspections. But many locations identified by the USAF for SHM have restricted geometries, presenting difficulties using the PZT transducers successfully. One known fatigue location in an aircraft bulkhead has been selected as a basis to evaluate some of the challenges of using PZT transducers for SHM. The goal of this research is use analytical and experimental investigations to detect fatigue cracks in plates representing the restricted geometry of the aircraft bulkhead. This research shows that detecting closed fatigue cracks can be more challenging than detecting open cracks, but that opening the cracks using an applied static load presents new challenges.

Edition details

• Publisher: BiblioBazaar, LLC
• Publication date: 2012
• Language: English
• ISBN 10: 1288397194
• ISBN 13: 9781288397198
• Binding: Paperback
• Number of pages: 84