NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Determination of Flaw Size from Thermographic DataConventional methods for reducing the pulsed thermographic responses of delaminations tend to overestimate the size of the flaw. Since the heat diffuses in the plane parallel to the surface, the resulting temperature profile over the flaw is larger than the flaw. A variational method is presented for reducing the thermographic data to produce an estimated size for the flaw that is much closer to the true size of the flaw. The size is determined from the spatial thermal response of the exterior surface above the flaw and a constraint on the length of the contour surrounding the flaw. The technique is applied to experimental data acquired on a flat bottom hole composite specimen.
Document ID
20150001522
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Winfree, William P.
(NASA Langley Research Center Hampton, VA, United States)
Howell, Patricia A.
(NASA Langley Research Center Hampton, VA, United States)
Zalameda, Joseph N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 10, 2015
Publication Date
July 20, 2014
Subject Category
Aircraft Design, Testing And Performance
Quality Assurance And Reliability
Composite Materials
Report/Patent Number
NF1676L-19743
Meeting Information
Meeting: Annual Quantitative Nondestructive Evaluation Conference
Location: Boise, ID
Country: United States
Start Date: July 20, 2014
End Date: July 25, 2014
Sponsors: Iowa State Univ.
Funding Number(s)
WBS: WBS 432938.11.01.07.43.30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available