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Open Circuit Resonant Sensors for Composite Damage Detection and DiagnosisUnder the Integrated Vehicle Health Management (IVHM) program work was begun to investigate the feasibility of sensor systems for detecting and diagnosing damage to aircraft composite structures and materials. Specific interest for this study was in damage initiated by environmental storm hazards and the direct effect of lightning strikes on the material structures of a composite aircraft in flight. A series of open circuit resonant sensors was designed, fabricated, characterized, and determined to be a potentially viable means for damage detection and diagnosis of composite materials. The results of this research and development effort are documented in this report.
Document ID
20110004280
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Mielnik, John J., Jr.
(Lockheed Martin Corp. Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2011
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA/CR-2011-216884
NF1676L-11914
Funding Number(s)
WBS: WBS 648987.02.04.07.20
TASK: NNL10AM25T
Distribution Limits
Public
Copyright
Public Use Permitted.
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