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Crack growth under spectrum loading: A crack closure modelA concept based on the crack-closure phenomenon was developed to replace random load spectra with constant amplitude loading in both analysis and tests. The maximum load and the crack opening load in the constant amplitude loading are chosen to be equal to those for the spectrum, so that both crack growth mode and the crack length at failure are equivalent to those under random load spectra. The number of cycles of constant- amplitude loading is chosen so that the amount of crack growth is equal to that due to a given sequence or block of the random spectrum loading. The concept was tested experimentally after predicting the equivalent number of constant-amplitude cycles for six different random load sequences. The agreement between predictions and test results was good.
Document ID
19750017149
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Elber, W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-72708
Report Number: NASA-TM-X-72708
Meeting Information
Meeting: Symp. of Fatigue Crack Growth Under Spectrum Loading, 78th Ann. ASTM Meeting
Start Date: January 1, 1975
Accession Number
75N25221
Funding Number(s)
PROJECT: RTOP 505-02-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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