NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage ToleranceInternational technical experts in durability and damage tolerance of metallic airframe structures were assembled to present and discuss recent research findings and the development of advanced design and analysis methods, structural concepts, and advanced materials. The symposium focused on the dissemination of new knowledge and the peer-review of progress on the development of advanced methodologies. Papers were presented on: structural concepts for enhanced durability, damage tolerance, and maintainability; new metallic alloys and processing technology; fatigue crack initiation and small crack effects; fatigue crack growth models; fracture mechanics failure, criteria for ductile materials; structural mechanics methodology for residual strength and life prediction; development of flight load spectra for design and testing; and advanced approaches to resist corrosion and environmentally assisted fatigue.
Document ID
19950008039
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Harris, Charles E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CP-3274-PT-1
NAS 1.55:3274-PT-1
L-17432-PT-1
Report Number: NASA-CP-3274-PT-1
Report Number: NAS 1.55:3274-PT-1
Report Number: L-17432-PT-1
Accession Number
95N14453
Funding Number(s)
PROJECT: RTOP 538-02-10-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available