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Microstructurally based model of fatigue initiation and growthA model to calculate fatigue life is developed based on the assumption that fatigue life is entirely composed of crack growth from an initial microstructural inhomogeneity. Specifically, growth is considered to start from either an ellipsoidal void, a cracked particle, or a debonded particle. The capability of predicting fatigue life from material microstructure is based on linear elastic fracture mechanics principles, the sizes of the crack-initiating microstructural inhomogeneities, and an initiation parameter that is proportional to the cyclic plastic zone size. A key aspect of this modeling approach is that it is linked with a general purpose probability program to analyze the effect of the distribution of controlling microstructural features within the material. This enables prediction of fatigue stress versus life curves for various specimen geometries using distributional statistics obtained from characterizations of the microstructure. Results are compared to experimental fatigue data from an aluminum alloy.
Document ID
19950008045
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brockenbrough, J. R.
(Aluminum Co. of America Alcoa Center, PA, United States)
Hinkle, A. J.
(Aluminum Co. of America Alcoa Center, PA, United States)
Magnusen, P. E.
(Aluminum Co. of America Alcoa Center, PA, United States)
Bucci, R. J.
(Aluminum Co. of America Alcoa Center, PA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
Subject Category
Structural Mechanics
Accession Number
95N14459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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