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Recent fracture mechanics results from NASA research related to the aging commercial transport fleetNASA is conducting the Airframe Structural Integrity Program in support of the aging commercial transport fleet. This interdisciplinary program is being worked in cooperation with the U.S. airframe manufacturers, airline operators, and the FAA. Advanced analysis methods are under development to predict the fatigue crack growth in complex built-up shell structures. Innovative nondestructive examination technologies are also under development to provide large area inspection capability to detect corrosion, disbonds, and fatigue cracks. Recent fracture mechanics results applicable to predicting the growth of cracks initiating at the rivets of fuselage splice joints are reviewed.
Document ID
19920009347
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
December 1, 1991
Publication Information
Publication: AGARD, Fatigue Management
Subject Category
Aircraft Design, Testing And Performance
Accession Number
92N18589
Distribution Limits
Public
Copyright
Other
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