Methodology for predicting the onset of widespread fatigue damage in lap-splice joints /

Bibliographic Details
Main Author: Newman, J. C. (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1998.
Series:NASA technical memorandum ; 1998-208975.
Subjects:
Online Access:https://purl.fdlp.gov/GPO/gpo83872

MARC

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245 1 0 |a Methodology for predicting the onset of widespread fatigue damage in lap-splice joints /  |c J.C. Newman, Jr. [and three others]. 
264 1 |a Hampton, Virginia :  |b National Aeronautics and Space Administration, Langley Research Center,  |c December 1998. 
300 |a 1 online resource (15 pages) :  |b illustrations. 
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490 1 |a NASA/TM ;  |v 1998-208975 
500 |a "December 1998." 
500 |a "Performing organization: NASA Langley Research Center"--Report documentation page. 
504 |a Includes bibliographical references (pages 10-11). 
513 |a Technical memorandum. 
536 |a Sponsored by the National Aeronautics and Space Administration  |d WU 522-18-11-01  |d L-17799 
588 |a Description based on online resource; title from PDF title page (NASA, viewed Aug. 17, 2017). 
650 7 |a Crack propagation.  |2 nasat 
650 7 |a Crack tips.  |2 nasat 
650 7 |a Airframes.  |2 nasat 
650 7 |a Stress analysis.  |2 nasat 
650 7 |a Lap joints.  |2 nasat 
650 7 |a Fuselages.  |2 nasat 
650 7 |a Finite element method.  |2 nasat 
650 7 |a Fatigue tests.  |2 nasat 
650 7 |a Fatigue (materials)  |2 nasat 
710 2 |a Langley Research Center,  |e issuing body. 
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