Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction

AIAA/IEEE Digital Avionics Systems Conference - Proceedings

Volumn 1, Issue , 2001, Pages

  Keller, E ^a   Ray, A ^a  

^a The Pennsylvania State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; AIRCRAFT MODELS; CRACKS; FATIGUE OF MATERIALS; NONDESTRUCTIVE EXAMINATION; NUCLEAR ENERGY; ULTRASONIC DEVICES;

HEALTH MONITORING;

AIRFRAMES;

EID: 18144433976     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Compensation of ultrasonic transducers response by adapting excitation signals, application to defects evaluation
2. Inverse methods and imaging
3. State-Space modelling of fatigue crack growth in ductile alloys
4. Stochastic modelling of fatigue crack damage for risk analysis and remaining life prediction
5. An ultrasonic method for measurement of size and opening behaviour of small fatigue cracks