On Displacement Fields in Orthotropic Laminates Containing an Elliptical Hole
Author:
Affiliation:
1. Civil Engineering Department, Chung-Cheng Institute of Technology, Tahsi, Taoyuan 33509, Taiwan
2. Mechanical Engineering Department, University of Washington MS 352600, Seattle, WA 98195
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/67/3/527/5467097/527_1.pdf
Reference19 articles.
1. Green, A. E., and Taylor, G. I., 1945, “Stress Systems in Aeolotropic Plates III,” Proc. R. Soc. London, Ser. A, 184, pp. 181–195;
2. pp. 218–219.
3. Bonora, N., Costanzi, M., and Marchetti, M., 1993, “On Closed Form Solution for the Elastic Stress Field Around Holes in Orthotropic Composite Plates Under in-Plane Stress Conditions,” Composite Structures,25, pp. 139–156.
4. Sampath, S. G., and Hulbert, L. E., 1975, “Analysis of Multiholed Orthotropic Laminated Plates by the Boundary-Point-Squares Methods,” ASME J. Pressure Vessel Technol., 75, pp. 118–122.
5. Hayashi, T., 1986, “Stress Analysis of the Anisotropic Plate With a Hole Under the Uniaxial Loading,” Composite ’86: Recent Advances in Japan and the United States, Proc. Japan-U.S. CCM-III, K. Kawata, S. Umekawa, and A. Kobayashi, eds., Japan Society of Composite Materials, Tokyo, pp. 197–204.
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