NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Combined investigation of Eddy current and ultrasonic techniques for composite materials NDEAdvanced composites are not without trade-offs. Their increased designability brings an increase in the complexity of their internal geometry and, as a result, an increase in the number of failure modes associated with a defect. When two or more isotropic materials are combined in a composite, the isotropic material failure modes may also combine. In a laminate, matrix delamination, cracking and crazing, and voids and porosity, will often combine with fiber breakage, shattering, waviness, and separation to bring about ultimate structural failure. This combining of failure modes can result in defect boundaries of different sizes, corresponding to the failure of each structural component. This paper discusses a dual-technology NDE (Non Destructive Evaluation) (eddy current (EC) and ultrasonics (UT)) study of graphite/epoxy (gr/ep) laminate samples. Eddy current and ultrasonic raster (Cscan) imaging were used together to characterize the effects of mechanical impact damage, high temperature thermal damage and various types of inserts in gr/ep laminate samples of various stacking sequences.
Document ID
19950020358
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Davis, C. W.
(Army Aviation Systems Command Hampton, VA., United States)
Nath, S.
(Analytic Services and Materials, Inc. Hampton, VA., United States)
Fulton, J. P.
(Analytic Services and Materials, Inc. Hampton, VA., United States)
Namkung, M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NAS 1.15:110599
NASA-TM-110599
Accession Number
95N26778
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available