The paper presents real-time non-destructive evaluation (NDE) of fatigue crack damage using ultrasonic sensing. The damage sensing system is suitable for health monitoring and residual life prediction in both aging and new aircraft structures.
Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction
20th DASC. 20th Digital Avionics Systems Conference (Cat. No.01CH37219) ; 1 ; 3D5/1-3D5/12 vol.1
01.01.2001
762904 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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