Abstract
Reliability inspections of structures for fatigue cracks are traditionally conducted at equispaced intervals because, it is assumed, the average slope of the hazard function following an inspection does not change from one inspection to the next. This study examines the common case where fatigue cracks nucleate continually over time. In such cases it is found that the slope of the hazard function after inspection may tend to increase from one inspection to the next, suggesting that inspection intervals should decrease with increasing service life. A formalism is introduced that allows calculation of the hazard function from microcrack data.
Issue Section:
Research Papers
References
1.
Chen
, E. Y.
, Lawson
, L.
, and Meshii
, M.
, “The Distribution of Fatigue Microcracks in an Aluminum-Matrix Silicon Carbide Whisker Composite
,” Scripta Metallurgica et Materialia
, Vol. 30
, No. 6
, 1993
, pp. 737
-742
.2.
Chen
, E. Y.
, Lawson
, L.
, and Meshii
, M.
, “Fatigue of Discontinuous Reinforced Aluminum Metal Matrix Composites: Challenges for Nondestructive Evaluation
,” Proceedings for the Dedicated Conference on New and Alternative Materials for Transportation Industries
, 27th International Symposium on Automotive Technology and Automation
, Aachen, Germany
, 1994
, pp. 115
-122
.3.
Chen
, E. Y.
, Lawson
, L.
, and Meshii
, M.
, “The Effects of Fatigue Microcracks on Rapid Catastrophic Failure in Al-SiC Composites
,” Materials Science and Engineering A
, in press.4.
Sasaki
, M.
, Lawson
, L.
, and Meshii
, M.
, “Low-Cycle Fatigue Properties of a SiC Whisker-Reinforced 2124 Aluminum Alloy
,” Metallurgical and Materials Transactions A
, Vol. 25A
, 1994
, pp. 2265
-2274
.5.
Williams
, D. R.
, Ph.D. thesis, Northwestern University
, Evanston, IL, 1985
.6.
Lukas
, P.
, “Mechanisms of Crack Nucleation in Fatigued Materials
,” Gefuge und Bruch
, Materialkundlich-Technische Reihe, Vol. 9
, Maurer
K. L.
and Pohl
M.
, Eds., Gebruder Borntraeger
, Berlin-Stuttgart
, 1990
, pp. 125
-139
.7.
Chen
, E. Y.
, Lawson
, L.
, and Meshii
, M.
, “Statistics of Fatigue Crack Initiation in 304 Stainless Steel
,” paper presented in Fatigue Crack Initiation Symposium, Materials Week '93
, Pittsburgh, PA
, 1993
.8.
Magnin
, T.
, Courdreuse
, L.
, and Lardon
, J. M.
, “A Quantitative Approach to Fatigue Damage Evolution in FCC and BCC Stainless Steels
,” Scripta Metallurgica
, Vol. 19
, 1985
, pp. 1487
-1490
.9.
Parkins
, R. N.
and Singh
, P. M.
, “Stress Corrosion Coalescence
,” Corrosion
0010-9312, Vol. 46
, No. 6
, 1990
, pp. 485
-499
.10.
Kitagawa
, H.
, Fujita
, T.
, and Miyazawa
, K.
, “Small Randomly Distributed Cracks in Corrosion Fatigue
,” Corrosion Fatigue Technology
ASTM STP 642, Craig
, H. L.
Jr., Crooker
T. W.
, and Hoeppner
D. W.
, Eds., American Society for Testing and Materials
, Philadelphia
, 1978
, pp. 98
-114
.11.
Suh
, C. M.
, Lee
, J. J.
, and Kang
, Y. G.
, “Fatigue Microcracks in Type 304 Stainless Steel at Elevated Temperature
,” Fatigue and Fracture of Engineering Materials and Structures
, Vol. 13
, No. 5
, 1990
, pp. 487
-496
.12.
Berens
, A. P.
, Burns
, J. G.
, and Rudd
, J. L.
, “Risk Analysis for Aging Aircraft Fleets
,” Structural Integrity of Aging Airplanes
, Althuri
S. N.
, Sampath
S. G.
, and Tong
P.
, Eds., Springer-Verlag
, New York
, 1991
, pp. 28
-51
.13.
Chen
, E. Y.
, Lawson
, L.
, and Meshii
, M.
, “Fatigue of Discontinuous Reinforced Aluminum Metal Matrix Composites: Requirements for New Technologies
,” Composites X, Proceedings of the 10th Annual Advanced Composites Conference-Exhibition
, Detroit MI, ASM, Materials Park
, Ohio
(in press).14.
Sobczyk
, K.
and Spencer
, B. F.
, Jr., Random Fatigue
, Academic Press
, New York
, 1991
.
This content is only available via PDF.
All rights reserved. This material may not be reproduced or copied, in whole or in part, in any printed, mechanical, electronic, film, or other distribution and storage media, without the written consent of ASTM International.
You do not currently have access to this content.