Characterization of the damage process in GLARE® 2 using an eddy current technique based on HTS-SQUID magnetometer

Superconductor Science and Technology

Volumn 20, Issue 1, 2007, Pages 51-56

  Bonavolonta C ^a,b   Valentino, M ^b,c   Pepe, G P ^b,c  

^a IMAST   (Italy)

^b CNR   (Italy)

^c UNIVERSITY OF NAPLES FEDERICO II   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

EDDY CURRENT TESTING; LAMINATES; MAGNETIC FIELD EFFECTS; MAGNETOELECTRIC EFFECTS; MAGNETOMETERS;

DAMAGE PROCESS; FIBRE METALLIC LAMINATES; MAGNETIC FIELD RESPONSE; MECHANICAL DAMAGING;

SQUIDS;

EID: 33947627160     PISSN: 09532048     EISSN: 13616668     Source Type: Journal    
DOI: 10.1088/0953-2048/20/1/009     Document Type: Article

References (4)

1. Roebroeks G H J J 1991 Towards GLARE, the development of fatigue insensitive and damage tolerant aircraft material Int. Report Delft University of Technology, The Netherlands
2. Lariviere S G and Thompson J 1998 Development of reliable NDI procedures for airframe inspection NATO RTO Mtg Proc. 10: Airframe Inspection Reliability under Field/Depot Conditions paper 7
3. Valentino M, Ruosi A, Pepe G and Peluso G 2002 Structural health monitoring of materials by high critical temperature SQUID Physica C 201 372-6
4. Bonavolont C, Pepe G P, Peluso G, Valentino M, Caprino G and Lopresto V 2005 Electromagnetic non-destructive evaluation of fibreglass/aluminium laminates by using HTS SQUID magnetometers IEEE Trans. Appl. Supercond. 15 (2)