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An overview of NASA research related to the aging commercial transport fleetThis paper describes the research activities of the NASA Airframe Structural Integrity Program for the aging commercial transport fleet. Advanced analysis methods are under development to predict the fatigue crack growth in complex built-up shell structures. Innovative nondestructive examination technologies are under development to provide large area inspection capability to detect corrosion, disbonds, and fatigue cracks. The ultimate goal of this interdisciplinary program is to develop and transfer advanced technology to the airline operators and airframe manufacturers. The program is being conducted cooperatively with the FAA and the U.S. industry.
Document ID
19910047378
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Heyman, Joseph S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Aeronautics (General)
Report/Patent Number
AIAA PAPER 91-0952
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Baltimore, MD
Country: United States
Start Date: April 8, 1991
End Date: April 10, 1991
Accession Number
91A32001
Distribution Limits
Public
Copyright
Other

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