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Some factors that affect the inspection of aircraft for fatigue damageFatigue crack length relationship with aircraft inspection intervals and structural reinforcement, high strength materials, and aircraft usage effects
Document ID
19710021307
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Leybold, H. A. (NASA Langley Research Center Hampton, VA, United States)
Poe, C. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971
Subject Category
Structural Mechanics
Accession Number
71N30783
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19710021280Collected WorksNASA Aircraft Safety and Operating Problems, Volume 1Collected Works19710021280Collected WorksNASA Aircraft Safety and Operating Problems, Volume 1N71-30756 18-02Collected Works
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