Damage detection and identification in composite aircraft components

IEEE Aerospace Conference Proceedings

Volumn 6, Issue , 2000, Pages 263-270

  Edmonds, Jack ^a   Hickman, Gail A ^a  

^a Innovative Dynamics Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; ALGORITHMS; COMPOSITE MATERIALS; DELAMINATION; FAILURE ANALYSIS; FATIGUE TESTING; INTELLIGENT STRUCTURES; LIFE CYCLE; MILITARY AIRCRAFT; PATTERN RECOGNITION; STATISTICAL METHODS; STRESSES;

CATASTROPHIC PART FAILURE; COMPOSITE AIRCRAFT COMPONENTS; DAMAGE DETECTION; FATIGUE TEST FACILITY; HEALTH MONITOR SYSTEM; VIBRATION SIGNATURE ANALYSIS;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0034431812     PISSN: 1095323X     EISSN: None     Source Type: Journal    
DOI: 10.1109/AERO.2000.877902     Document Type: Article

References (11)

1. Vibration techniques in nondestructive testing
2. The predicted and experimental natural modes of free-free CFRP plates
3. A vibration technique for nondestructive testing of fibre composite structures
4. Influence of damage on the vibration response of composite laminates
5. Local area damage detection incomposite structures using piezoelectric transducers
6. Active damage interrogation system for structural health monitoring
7. Ground and flight test results of a PZT health monitoring system
8. Neural network health monitoring system for composite structures
9. Method and apparatus for structural integrity monitoring
10. Application of smart structures to aircraft health monitoring
11. Health monitoring system for aircraft