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A probabilistic fatigue analysis of multiple site damageThe variability in initial crack size and fatigue crack growth is incorporated in a probabilistic model that is used to predict the fatigue lives for unstiffened aluminum alloy panels containing multiple site damage (MSD). The uncertainty of the damage in the MSD panel is represented by a distribution of fatigue crack lengths that are analytically derived from equivalent initial flaw sizes. The variability in fatigue crack growth rate is characterized by stochastic descriptions of crack growth parameters for a modified Paris crack growth law. A Monte-Carlo simulation explicitly describes the MSD panel by randomly selecting values from the stochastic variables and then grows the MSD cracks with a deterministic fatigue model until the panel fails. Different simulations investigate the influences of the fatigue variability on the distributions of remaining fatigue lives. Six cases that consider fixed and variable conditions of initial crack size and fatigue crack growth rate are examined. The crack size distribution exhibited a dominant effect on the remaining fatigue life distribution, and the variable crack growth rate exhibited a lesser effect on the distribution. In addition, the probabilistic model predicted that only a small percentage of the life remains after a lead crack develops in the MSD panel.
Document ID
19950013060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rohrbaugh, S. M.
(Purdue Univ. West Lafayette, IN, United States)
Ruff, D.
(Purdue Univ. West Lafayette, IN, United States)
Hillberry, B. M.
(Purdue Univ. West Lafayette, IN, United States)
Mccabe, G.
(Purdue Univ. West Lafayette, IN, United States)
Grandt, A. F., Jr.
(Purdue Univ. West Lafayette, IN, 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, Part 2
Subject Category
Structural Mechanics
Accession Number
95N19476
Funding Number(s)
CONTRACT_GRANT: F49620-93-1-0377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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