Progressive damage modeling of an adhesively bonded composite single lap joint under flexural loads at the mesoscale level

Journal of Reinforced Plastics and Composites

Volumn 26, Issue 9, 2007, Pages 903-953

  Apalak, Z Gul ^a   Apalak, M Kemal ^a   Genc, M Serdar ^a  

^a ERCIYES UNIVERSITY   (Turkey)

Author keywords

Adhesive; Composite; Damage; Failure; Layered finite element; Meso volume; Single lap joint; Stress analysis

Indexed keywords

ADHESIVES; BENDING STRENGTH; DAMAGE DETECTION; DEGRADATION; STRESS ANALYSIS;

LAYERED FINITE ELEMENT; MESO VOLUME; SINGLE LAP JOINT;

COMPOSITE MATERIALS;

EID: 34547613167     PISSN: 07316844     EISSN: 15307964     Source Type: Journal    
DOI: 10.1177/0731684407079413     Document Type: Article

References (61)

1. Hashin, Z. (1980). Failure Criteria for Unidirectional Fibre Composites, Journal of Applied Mechanics, 47: 329 - 334.
2. Liu, K.S. and Tsai S.W. (1998). A Progressive Quadratic Failure Criterion for a Laminate, Composites Science and Technology, 58 (7). 1023 - 1032.
3. Lessard, L.B. and Shokrieh, M.M. (1991). Two-dimensional Modeling of Composite Pinned-joint Failure, Journal of Composite Materials, 25: 556 - 577.
4. Shokrieh, M.M. and Lessard, L.B. (2001). Progressive Fatigue Damage Modeling of Composite Materials. Part I: Modeling, Journal of Composite Materials, 34: 1056 - 1080.
5. Camanho, P.P. and Matthews, F.L. (2000). A Progressive Damage Model for Mechanically Fastened Joints in Composite Laminates, Journal of Composite Materials, 33: 906 - 27.
6. Camanho, P.P. and Matthews, F.L. (1997). Stress Analysis and Strength Prediction of Mechanically Fastened Joints in FRP: A Review, Composites: Part A, 28: 529 - 547.
7. Tserpes, K.I., Papanikos, P. and Kermanidis, T.H. (2002). A Three-dimensional Progressive Damage Model for Bolted Joints in Composite Laminates Subjected to Tensile Loading, Fatigue and Fracture Engineering Materials and Structures, 24 (10). 673 - 686.
8. Tserpes, K.I., Labeas, G., Papanikos, P. and Kermanidis, Th. (2002). Strength Prediction of Bolted Joints in Graphite/Epoxy Composite Laminates, Composites: Part B, 33: 521 - 529.
9. Tserpes, K.I., Papanikos, P., Labeas, G. and Pantelakis, Sp. (2004). Fatigue Damage Accumulation and Residual Strength Assessment of CFRP Laminates, Composite Structures, 63: 219 - 230.
10. Tan, S.C. (1991). A Progressive Failure Model for Composite Laminates Containing Openings, Journal of Composite Materials, 25: 556 - 577.
11. Tan, S.C. and Perez, J. (1993). Progressive Failure of Laminated Composites with a Hole under Compressive Loading, Journal of Reinforced Plastics and Composites, 18: 255 - 278.
12. Nuismer, R.J. and Tan S.C. (1988). Constitutive Relations of a Cracked Composite Lamina, Journal of Composite Materials, 22: 306 - 21.
13. Tan, S.C. and Nuismer, R.J. (1989). A Theory of Progressive Matrix Cracking in Composite Laminates, Journal of Composite Materials, 23: 1029 - 1047.
14. Haj-Ali, R. and Kilic, H. (2002). Non-linear Behavior of Pultruded FRP Composite, Composites: Part B, 33: 173 - 191.
15. Kilic, H. and Haj- Ali, R. (2003). Progressive Damage and Nonlinear Analysis of Pultruded Composite Structures, Composites: Part B, 34: 235 - 250.
16. Kilic, H. and Haj-Ali, R. (2003). Elastic-degrading Analysis of Pultruded Composite Structures, Composite Structures, 60: 43 - 55.
17. Haj-Ali, R. and Kilic, H. (2003). Nonlinear Constitutive Models for Pultruded FRP Composites, Mechanics of Materials, 35: 791 - 801.
18. Kwon, Y.W. and Berner, J.M. (1995). Micromechanics Model for Damage and Failure Analyses of Laminated Fibrous Composites, Engineering Fracture Mechanics, 52: 231 - 242.
19. Bogetti, T.A., Hoppel, C.P.R., Harik, V.M., Newill, J.F. and Burns B.P. (2004). Predicting the Nonlinear Response and Progressive Failure of Composite Laminates, Composite Science and Technology, 64: 329 - 342.
20. Bogetti, T.A., Hoppel, C.P.R., Harik, V.M., Newill, J.F. and Burns, B.P. (2004). Predicting the Nonlinear Response and Failure of Composite Laminates: Correlation with Experimental Results, Composite Science and Technology, 64: 477 - 485.
21. Spottswood, S.M. and Palazotto, A.N. (2001). Progressive Failure Analysis of a Composite Shell, Composite Structures, 53: 117 - 131.
22. McCarthy, C.T., McCarthy, M.A. and Lawlor, V.P. (2005). Progressive Damage Analysis of Multi-bolt Composite Joints with Variable Bolt-hole Clearances, Composites: Part B, 36: 290 - 305.
23. McCarthy, M.A., McCarthy, C.T., Lawlor, V.P. and Stanley, W.F. Three-dimensional Finite Element Analysis of Single-bolt, Single Lap Composite Bolted Joints: Part I - Model Development and Validation, Composite Structures, 71 (2). 140 - 158.
24. McCarthy, C.T. and McCarthy, M.A. Three-dimensional Finite Element Analysis of Single-bolt, Single-lap Composite Bolted Joints: Part II - Effects of Bolt-hole Clearance, Composite Structures (in press).
25. Ambur, D.R., Jaunky, N. and Hilburger M.W. (2004). Progressive Failure Studies of Stiffened Panels subjected to Shear Loading, Composite Structures, 65: 129 - 142.
26. Reedy, J.N. (1996). Mechanics of Laminated Composite Plates (Theory and Analysis), CRC Press, Boca Raton.
27. Ochoa, O.O. and Reedy, J.N. (1992). Finite Element Analysis of Composite Laminates, Kluwer Academic Publishers, Dordrecht.
28. Jones, R.M. (1999). Mechanics of Composite Materials, Taylor and Francis, New York.
29. Tsai, S.W. and Hahn, H.T. (1980). Introduction to Composite Materials, Technomic Publishing Co., Westport, Connecticut.
30. Adams, R.D. and Wake, W.C. (1984). Structural Adhesive Joints in Engineering, Elsevier Applied Science, London.
31. Kinloch, A.J. (1987). Adhesion and Adhesives, Chapman and Hall, London.
32. Volkersen, O. (1938). Die Nietkraftverteilung in Zugbeanspruchten Nieverbindungen mit Konstanten Laschenquerschnitten, Luftfahrtforschung, 15: 41 - 47.
33. Volkersen, O. (1965). Construction Metallique, 4: 3 - 13.
34. Goland, M. and Reissner, E. (1944). The stresses in Cemented Joints, Journal of Applied Mechanics, 11: A-17-27.
35. Hart - Smith, L.J. (1973). Adhesive-Bonded Single-Lap Joints, Douglas Aircraft Co., NASA Langley Report CR 112236.
36. Hart - Smith, L.J. (1973). Adhesive-Bonded Double-Lap Joints, Douglas Aircraft Co., NASA Langley Report CR 112235.
37. Hart - Smith, L.J. (1973). Adhesive-Bonded Scarf and Stepped-Lap Joints, Douglas Aircraft Co., NASA Langley Report CR 112237.
38. Hart - Smith, L.J. (1974). Analysis and Design of Advanced Composite Bonded Joints, Douglas Aircraft Co., NASA Langley Report CR-2218.
39. Reissner, E. (1945). The Effect of Transverse Shear Deformation on the Bending of Elastic Plates, Journal of Applied Mechanics, 12: A-69-77.
40. Reddy, J.N. (1984). A Refined Nonlinear Theory of Plates with Transverse Shear Deformation, International Journal of Solids Structures, 20: 881 - 896.
41. Nageswara, R.B., Sadasiva, R.Y.V.K. and Yadagiri, S. (1982). Analysis of Composite Bonded Joints, Fibre Science and Technology, 17: 77 - 90.
42. Ishii, K., Imanaka, M., Nakayama H. and Kodama H. (1998). Fatigue Failure Criterion of Adhesively Bonded CFRP/Metal Joints under Multiaxial Stress conditions, Composites: Part A, 29 (4). 415 - 422.
43. Ishii, K., Imanaka, M., Nakayama, H. and Kodama, H. (1999). Evaluation of The Fatigue Strength of Adhesively Bonded CFRP/Metal Single and Single-Step Double-Lap Joints, Composites Science and Technology, 59 (11). 1675 - 1683.
44. Kam, T.Y. and Lai, F.M. (1999). Experimental and Theoretical Predictions of First-Ply Failure Strength of Laminated Composite Plates, International Journal of Solids and Structures, 36 (16). 2379 - 2395.
45. Tong, L. (1997). An Assessment of Failure Criteria to Predict the Strength of Adhesively Bonded Composite Double Lap Joints, Journal of Reinforced Plastics and Composites, 16 (8). 698 - 713.
46. Tong, L. (1998). Strength of Adhesively Bonded Single Lap and Lap-Shear Joints, International Journal Solids and Structures, 35 (20). 2601 - 2616.
47. Tong, L., Sheppard, A., Kelly, D. and Chalkley, P. (1998). Effect of Joint Flexibility in Adhesively Bonded Composite Panel-to-Flange Joints, Composites: Part B, 29 (3). 287 - 298.
48. Sheppard, A., Kelly, D. and Tong, L. (1998). A Damage Zone Model for the Failure Analysis of Adhesively Bonded Joints, International Journal of Adhesion & Adhesives, 18 (6). 385 - 400.
49. Cheuk, P.T., Tong, L., Wang, C.H., Baker, A. and Chalkley, P. (2002). Fatigue Crack Growth in Adhesively Bonded Composite-Metal Double-Lap Joints, Composite Structures, 57 (1 - 4). 109 - 115.
50. Kim, K., Yoo, J., Yi, Y. and Kim, C. Failure Mode and Strength of Unidirectional Composite Single Lap Bonded Joints with Different Bonding Methods, Composite Structures (in press).
51. Li, G., Lee-Sullivan, P. and Thring, R.W. (1999). Nonlinear Finite Element Analysis of Stress and Strain Distributions across the Adhesive Thickness in Composite Single-lap Joints, Composite Structures, 46 (4). 395 - 403.
52. Apalak, M.K. and Engin, A. (2003). An Investigation on the Initiation and Propagation of Damaged Zones in Adhesively Bonded Lap Joints, Journal of Adhesion Science and Technology, 17 (14). 1889 - 1921.
53. Apalak, M.K. and Engin, A. (2004). Effect of Adhesive Free-end Geometry on the Initiation and Propagation of Damaged Zones in Adhesively Bonded Lap Joints, Journal of Adhesion Science and Technology, 18 (5). 529 - 560.
54. Apalak, M.K., Gunes, R., Turaman, M.O. and Cerit, A.A. (2003). Thermal and Geometrically Non-Linear Stress Analyses of an Adhesively Bonded Composite Tee Joint, Composites: Part A, 34 (2). 135 - 150.
55. Cook, R.D., Malkus, D.V. and Plesha, M.E. (1989). Concept and Applications of Finite Element Analysis, John Wiley & Sons, Canada.
56. Ahmad, S., Irons, B.M. and Zienkiewicz, O.C. (1970). Analysis of Thick and Thin Shell Structures by Curved Finite Elements, International Journal of Numerical Methods in Engineering, 2 (3). 419 - 451.
57. Yunus, S.M., Khonke, P.C. and Saigal, S. (1989). An Efficient Through-thickness Integration Scheme in an Unlimited Layer Doubly Curved Isoparametric Composite Shell Element, International Journal of Numerical Methods in Engineering, 28 (12). 2777 - 2793.
58. Apalak, M.K. and Gunes, R. (2005). Thermal Residual Stress Analysis of Ni-Al2O3, Ni-TiO2 and Ti-2-SiC Functionally Graded Composite Plates subjected to Various Thermal Fields, Journal of Thermoplastic Composite Materials, 18 (2). 119 - 152.
59. Panda, S. and Natarajan, R. (1981). Analysis of Laminated Composite Shell Structures by Finite Element Method, Computers and Structures, 14 (3 - 4). 225 - 230.
60. Kumar, W.P.P. and Palaninathan, R. (1997). Finite Element Analysis of Laminated Shells with Exact Through-thickness Integration, Computers and Structures, 63 (1). 173 - 184.
61. Apalak, M.K. and Gunes, R. (2005). Investigation of Elastic Stresses in an Adhesively Bonded Single Lap Joint with Functionally Graded Adherends in Tension, Composite Structures, 70 (4). 444 - 467.