Reliability of Structures Containing Short Cracks
Author:
Affiliation:
1. Department of Aerospace Engineering, Applied Mechanics and Aviation, The Ohio State University, 2036 Neil Avenue, Room 328 BOLZ Hall, Columbus, OH 43210-1276
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Ocean Engineering
Link
http://asmedigitalcollection.asme.org/offshoremechanics/article-pdf/121/3/153/5681798/153_1.pdf
Reference22 articles.
1. Elber, W., 1971, “The Significance of Fatigue Crack Closure,” Damage Tolerance in Aircraft Structures, STP 486, American Society for Testing and Materials, Philadelphia, PA, pp. 230–242.
2. Fu B. , HaswellJ. V., and BettessP., 1993, “Weld Magnification Factors for Semi-Elliptical Surface Cracks in Fillet Welded T-Butt Joint Models,” International Journal of Fracture, Vol. 63, pp. 155–171.
3. El Haddad M. H. , SmithK. N., and TopperT. H., 1979, “Fatigue Crack Propagation of Short Cracks,” ASME Journal of Engineering Materials and Technology, Vol. 101, Jan., pp. 42–46.
4. Hasofer A. M. , and LindN. C., 1971, “Exact and Invariant Second-Moment Code Format,” Journal of Engineering Mechanics, Vol. 100, pp. 111–121.
5. Lanning Jr., D. B., and Shen, M.-H. H., 1996, “Reliability of Welded Structures Containing Fatigue Cracks,” to appear in ASME JOURNAL OF OFFSHORE MECHANICS AND ARCTIC ENGINEERING.
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