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
2001-01-01
762904 byte
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2001
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