Affiliation:
1. Mitsubishi Heavy Industries, Ltd., Nagoya Aerospace Systems Works, Nagoya 455-8515, Japan
Abstract
The coalescence conditions of plastic zones are calculated for multiple cracks in a riveted stiffened sheet using a strip yield model. The multiple cracks and their plastic zones are treated as a fictitious crack, and algebraic equations are formulated on compatibility of displacements, no stress singularity at the fictitious crack tips, and zero displacement at the coalesced points of plastic zones. These equations are iteratively solved, and critical values of remote stress, fastener forces, plastic zone sizes, and crack tip opening displacements are calculated. Some numerical results are presented for two cracks in a sheet with and without stiffeners.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Reference10 articles.
1. Bloom
J. M.
, and SandersJ. L., 1966, “The Effect of a Riveted Stringer on the Stress in a Cracked Sheet,” ASME Journal of Applied Mechanics, Vol. 33, pp. 561–570.
2. Isida
M.
, and TsunadaT., 1979, Transactions of the Japan Society of Mechanical Engineers, Ed. A, Vol. 45, pp. 346–354 (in Japanese).
3. Low, M. C., and Cartwright, D. J., 1985, “Fracture Diagrams for Stiffened Aircraft Structures: Effects of Material Non-Linearity, Durability and Damage Tolerance in Aircraft Design,” Engineering Materials Advisory Services, pp. 551–583.
4. Nishimura
T.
, 1991, “Stress Intensity Factors of Multiple Cracked Sheet with Riveted Stiffeners,” ASME JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY, Vol. 113, pp. 280–284.
5. Nishimura
T.
, 1993, “Strip Yield Analysis for Multiple Cracked Sheet with Riveted Stiffeners,” ASME JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY, Vol. 115, pp. 398–403.
Cited by
9 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献