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TECHNICAL PAPERS

Assessment of the Fracture Behavior of an Asymmetrically Loaded Cantilever Composite Structure

[+] Author and Article Information
Baoxiang Shan, Assimina A. Pelegri

Rutgers, The State University of New Jersey, Department of Mechanical and Aerospace Engineering, 98 Brett Road, Piscataway, NJ 08854-8058 USA

J. Eng. Mater. Technol 125(4), 353-360 (Sep 22, 2003) (8 pages) doi:10.1115/1.1605108 History: Received January 21, 2003; Revised June 17, 2003; Online September 22, 2003
Copyright © 2003 by ASME
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References

Sanford, R. J., 1997, Foundations of Linear Elastic Fracture Mechanics, SPIE Optical Engineering Press, Bellingham, Washington, pp. 161–363.
Sanford, R. J., 1997, Crack Tip Stress Fields, SPIE Optical Engineering Press, Bellingham, Washington, pp. 3–215.
Sheinman,  I., Kardomateas,  G. A., and Pelegri,  A. A., 1998, “Delamination Growth During Pre- and Post-Buckling Phases of Delaminated Composite Laminates,” Int. J. Solids Struct., 35(1–2), pp. 19–31.
Sheinman,  I., and Soffer,  M., 1991, “Post-Buckling Analysis of Composite Delaminated Beams,” Int. J. Solids Struct., 27(5), pp. 639–646.
Simitses,  G. J., Sallam,  S., and Yin,  W. L., 1985, “Effect of Delamination of Axially Loaded Homogeneneous Laminated Plates,” AIAA J., 23(4), pp. 1437–1444.
Yin,  W. L., Sallam,  S. N., and Simitses,  G. J., 1986, “Ultimate Axial Load Capacity of a Delaminated Beam-Plate,” AIAA J., 24(1), pp. 123–128.
Kardomateas,  G. A., 1989, “Large Deformation Effect in the Postbuckling Behavior of Composite With Thin Delaminations,” AIAA J., 27(5), pp. 624–631.
Suemasu,  H., 1993, “Effect of Multiple Delaminations on Compressive Buckling Behaviors of Composite Panels,” J. Compos. Mater., 27, pp. 1172–1192.
Suemasu,  T., Kumagai,  T., and Gozu,  K., 1998, “Compressive Behavior of Rectangular Composite Laminates With Multiple Circular Delaminations,” AIAA J., 36, pp. 1279–1285.
Comninou,  M., and Dundurs,  J., 1979, “On the Frictional Contact in Crack Analysis,” Eng. Fract. Mech., 12, pp. 117–123.
Comninou,  M., and Dundurs,  J., 1979, “An Example for Frictional Slip Progressing Into a Contact Zone of a Crack,” Eng. Fract. Mech., 12, pp. 191–197.
Antipov,  Y. A., 1995, “An Interface Crack Between Elastic Materials When There is Dry Friction,” J. Appl. Math. Mech., 59(2), pp. 273–287.
Audoly,  B., 2000, “Asymptotic Study of the Interfacial Crack With Friction,” J. Mech. Phys. Solids, 48(9), pp. 1851–1864.
Whitcomb,  J. D., 1981, “Finite Element Analysis of Instability Related Delamination Growth,” J. Compos. Mater., 15, pp. 403–426.
Moradi,  S., and Taheri,  F., 1999, “Postbuckling Analysis of Delaminated Composite Beams by Differential Quadrature Method,” Compos. Struct., 46, pp. 33–39.
Yeh,  M. K., and Fang,  L. B., 1999, “Contact Analysis and Experiments of Delaminated Cantilever Composite Beam,” Composites, Part B, 30(4), pp. 407–414.
Yeh,  M. K., Fang,  L. B., and Kao,  M. H., 1997, “Bending Behavior of Delaminated Composite Plates With Contact Effects,” Compos. Struct., 39(3–4), pp. 347–356.
ANSY Smanual, at http://www.cesup.ufrgs.br/ansys/elem_55/chapter4/ES4-2.htm
Timoshenko, S., 1934, Theory of Elasticity, McGraw-Hill, New York, New York, pp. 33–38.
Brush, D. O., and Almroth, B. O., 1975, Buckling of Bars, Plates, and Shells, McGraw-Hill, New York, New York, p. 22.
Yin,  W. L., and Wang,  T. S., 1984, “The Energy-Release Rate in the Growth of a One-Dimensional Delamination,” ASME J. Appl. Mech., 51, pp. 939–941.
Pelegri, A. A., and Chen, I., 2000, “Mixed Mode Fatigue of Fiber Reinforced Composites Using a Modified MMB Fixture,” 41st AIAA/ASME/ASCE/AHS/ASC SDM (Structures) Atlanta, AIAA-2000-1404.

Figures

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Geometry of the delaminated cantilever
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Singular elements at concentrated point
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Situation around the end of delamination: (a) penetration of the delamination flanks without contact analysis; and (b) contact of the delamination flanks with contact analysis.
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Relation of load and displacement: Line 1—model for h/T=6/24, without contact zone; Line 2—model for h/T=6/24, with contact zone; Line 3—model for h/T=3/24, without contact zone; Line 4—model for h/T=3/24, with contact zone; and Line 5—model without delamination.
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Distribution of contact force along the delamination: P—applied load; Delamination length here is 50 mm.
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Procedure of solution to simple geometric model
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Variation of energy release rate with applied loading: solid line—ratio of energy release rate with contact zone to that without contact zone; dash line—energy release rate with contact zone.
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Applied load, P, versus displacement, δ, at the free end of cantilever beam: solid line—geometric model; dashed line—finite element analysis; and circle—experimental data.
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Ratio of stress intensity factors in mode II to mode I: (a) inner end for h/T=3/24 with contact zone; (b) outer end for h/T=3/24 with contact zone; (c) inner end for h/T=3/24 without contact zone; (d) outer end for h/T=3/24 without contact zone; (e) inner end for h/T=6/24 with contact zone; (f) outer end for h/T=6/24 with contact zone; (g) inner end for h/T=6/24 without contact zone; and (h) outer end for h/T=6/24 without contact zone.
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The variation of stress intensity factor in mode I with loading: (a) mode I, KI; and (b) mode II, KII.
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Trajectory of crack propagation in IM7/8552 graphite/epoxy. Kinking from the 6th /7th to the 5th /6th interface is observed.
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Trajectory of crack propagation in mode I

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