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

Underwood, Roman T.

 
9781288397198: Damage Detection Analysis Using Lamb Waves in Restricted Geometry for Aerospace Applications
Tapa blanda
ISBN 10: 1288397194 ISBN 13: 9781288397198
Editorial: BiblioScholar, 2012

Sinopsis

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.

"Sinopsis" puede pertenecer a otra edición de este libro.

Reseña del editor

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.

"Sobre este título" puede pertenecer a otra edición de este libro.

Editorial
BiblioScholar
Año de publicación
2012
Idioma
Inglés
ISBN 10 
1288397194
ISBN 13 
9781288397198
Encuadernación
Tapa blanda
Número de páginas
86
Contacto del fabricante
no disponible
Persona responsable
no disponible