|
Sign In to gain access to subscriptions and/or personal tools.
|
Effect of T-stress on Damage Zone Size Predictions of Notched Laminated Composites
Hsien-Yang Yeh
Department of Mechanical and Aerospace Engineering California State University Long Beach, CA 90840, USA; hyyeh{at}csulb.edu
Hina Naz Rashid
Department of Mechanical and Aerospace Engineering California State University Long Beach, CA 90840, USA
Hsien-Liang Yeh
Department of Civil and Ecological Engineering I-Shou University Kaohsiung County, Taiwan, China
In this article, the influence of T-stress on the plastic/damage zone size of a precracked isotropic/composite plate is studied by using various failure criteria under tensile loading conditions. The results of this study indicate that the stress field with T-stress always yields a larger damage zone than the field without T-stress. Using experimental data for a symmetrical, generally orthotropic graphiteepoxy laminate, the damage zone sizes predicted by the average stress criterion and point stress criterion as well as the D-criterion are compared. Experimental measurements of crack-tip damage zone size are used to establish a physical reference point by which all the theories are compared.
Key Words: T-stress damage zone size notched laminated composites
References
- Anderson, T. L. (1995). Fracture Mechanics, 2nd edn, CRC Press, USA.
- Yeh, Hsien-Yang, Kevin Berryhill, R. and Yeh, Hsien-Liang (2004). Analytical Damage Zone Size Predictions for Notched Laminated Composites, Journal of Reinforced Plastics and Composites, 23(18): 20812100.[Abstract]
- Williams, M. L. (1957). On the Stress at the Base of a Stationary Crack, Journal of Applied Mechanics, 24: 111114.
- Larsson, S. G. and Carlsson, A. J. (1973). Influence of Non-Singular Stress and Specimen Geometry on Small-scale Yielding at Each Tip in Elastic-Plastic Materials, Journal of Mechanics of Physics and Solids, 21: 263277.[CrossRef]
- Rice, J. R. (1974). Limitations to the Small Scale Yielding Approximation for Crack-Tip Plasticity, Journal of Mechanics of Physics and Solids, 22: 1726.
- Leevers, P. S. and Radon, J. C. (1981). Inherent Stress Biaxiality in Various Fracture Specimen Geometries, International Journal of Fracture, 19: 311325.
- Sih, G. C., Paris, P. C. and Irwin, G. R. (Dec 1971). On Cracks in Rectilinearly Anisotropic Bodies, International Journal of Fracture Mechanics, 1(3): 223237.
- Yuan, F. G. (May 2001). Fracture Behavior of a Stitched Wrap-Knit Carbon Fabric Composite, NASA/ TM2001-210868.
- Yuan, F. G. (October 1998). Determination of Stress Coefficient Terms in Cracked Solids for Monoclinic Materials with Plane Symmetry at x3 1/4 0, NASA CR-1998-208729.
- Tan, S. C. (1994). Stress Concentrations in Laminated Composites, Technomic Publishing Co., USA.
- Whitney, J. M. and Nuismer, R. J. (1975). Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations, Journal of Composite Materials, 8: 253265.
- Nuismer, R. J. and Whitney, J. M. (1975). Uniaxial Failure of Composite Laminates Containing Stress Concentrations, ASTM STP-593, pp. 117142.
- Zhen, S. (1983). The D Criterion Theory in Notched Composite Materials, Journal of Reinforced Plastics and Composites, 2: 98110.[Abstract]
- Yeh, H.-L. and Yeh, H.-Y. (2002). Stress Concentration in Symmetric Single-Ply Laminates Studied by the Quadric Surface Criterion, Journal of Reinforced Plastics and Composites, 21(18): 16711683.[Abstract/Free Full Text]
- Yeh, H.-L. and Yeh, H.-Y. (2003). A Sequential Fiber Failure Criterion for the Tensile Fracture in Notched Fiber Reinforced Composites, Journal of Reinforced Plastics and Composites, 22(5): 463478.[Abstract/Free Full Text]
- Yeh, H.-Y. and Kim, C. H. (1984). The Yeh-Stratton Criterion for Composite Materials, Journal of Composite Materials, 28: 926939.
- Irwin, G. R., Kies, J. A. and Smith, H. L. (1958). Fracture Strengths Relative to Onset and Arrest of Crack Propagation, Proceedings of the American Society for Testing Materials, 58: 640657.
- Coats, T. W. and Harrs, C. E. (1998). A Progressive Damage Methodology for Residual Strengths Predictions of Notched Composites Panels, National Aeronautics and Administration Technical Memorandum 207646.
Journal of Reinforced Plastics and Composites, Vol. 25, No. 1,
89-98 (2006)
DOI: 10.1177/0731684406055458

CiteULike Complore Connotea Del.icio.us Digg Reddit Technorati Twitter What's this?
|
|