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Reliability after inspectionFlaws are occasionally overlooked during non-destructive inspections, and consequently the products are not 100 percent reliable. The quantitative relationships among the probability of having manufacturing defects, the probability of detecting a flaw, and final reliability are established. Several specific situations are considered: where a flaw might be present; where a random number of flaws are randomly scattered throughout the piece; where some parts of the product are not accessible for inspection; and a general case where various portions are more easily inspected than others, more or less likely to contain flaws than others, or are not inspectable while other portions are.
Document ID
19740018871
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davidson, J. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-TM-X-71969
Report Number: NASA-TM-X-71969
Meeting Information
Meeting: ASTM Symp. on the Fatigue of Composite Mater.
Location: Bal Harbour, FL
Country: United States
Start Date: December 2, 1973
End Date: December 7, 1973
Accession Number
74N26984
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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