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NASA airframe structural integrity programNASA has initiated a research program with the long-term objective of supporting the aerospace industry in addressing issues related to the aging commercial transport fleet. The interdisciplinary program combines advanced fatigue crack growth prediction methodology with innovative nondestructive examination technology with the focus on multi-site damage (MSD) at riveted connections. A fracture mechanics evaluation of the concept of pressure proof testing the fuselage to screen for MSD has been completed. Also, a successful laboratory demonstration of the ability of the thermal flux method to detect disbonds at riveted lap splice joints has been conducted. All long-term program elements have been initiated and the plans for the methodology verification program are being coordinated with the airframe manufacturers.
Document ID
19930061785
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Structural integrity of aging airplanes (A93-45772 19-01)
Publisher: Springer-Verlag
Subject Category
Structural Mechanics
Accession Number
93A45782
Distribution Limits
Public
Copyright
Other

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