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Finite Elements and Fracture Mechanics

Finite Elements and Fracture Mechanics. Leslie Banks-Sills The Dreszer Fracture Mechanics Laboratory Department of Solid Mechanics, Materials and Systems Tel Aviv University. ISCM-1 5 , October, 2003. Outline. Introduction to fracture mechanics (homogeneous material).

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Finite Elements and Fracture Mechanics

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  1. Finite Elements and Fracture Mechanics Leslie Banks-Sills The Dreszer Fracture Mechanics Laboratory Department of Solid Mechanics, Materials and Systems Tel Aviv University ISCM-15, October, 2003

  2. Outline • Introduction to fracture mechanics (homogeneous material). • The finite element method. • Methods for calculating stress intensity factors. • Interface fracture mechanics.

  3. Dreszer Fracture Mechanics Laboratory

  4. Liberty Ships-World War II • The hulls of Liberty Ships fractured without warning, mainly in the North Atlantic. • There were 2,751 Liberty Ships manufactured between 1941- 1945. Cracks propagated in 400 of these ships including 145 catastrophic failures; only 2 exist today which are sea- worthy.

  5. Liberty Ships-(continued) • The low temperatures of the North Atlantic caused the steel to be brittle. • These are the first ships mass produced with welds. • Fractures occurred mainly in the vicinity of stress raisers. • The problem may be prevented by employing higher quality steels and improvement of the design of the ship.

  6. The Aloha Boeing 737 Accident On April 28, 1988, part of the fuselage of a Boeing 737 failed after 19 years of service. The failure was caused by fatigue (multi-site damage).

  7. The Aloha Boeing 737 Accident

  8. m = I, II, III i, j=1, 2, 3 mode I mode II mode III Modes of Fracture

  9. Asymptotic Stress Field in Mode I

  10. units Stress Intensity Factor m = I, II, III

  11. Fracture Toughness ASTM 399 Standard compact tension specimen material parameter, depends on environment

  12. J -- integral strain energy density tractions J is a conservative integral

  13. Griffith’s Energy G

  14. J vs G

  15. The Finite Element Method For a static problem:

  16. The Element Lagrangian shape functions for a four noded element

  17. The Element (continued) isoparametric element

  18. Special Crack Tip Elements quarter-point elements Henshell and Shaw, 1975, quadrilateral elements Barsoum, 1974,1976, triangular elements

  19. Special Crack Tip Elements quarter-point elements Henshell and Shaw, 1975, quadrilateral elements Barsoum, 1974,1976, triangular elements

  20. Special Crack Tip Elements quarter-point elements Henshell and Shaw, 1975, quadrilateral elements Barsoum, 1974,1976, triangular elements

  21. Special Crack Tip Elements quarter-point elements Henshell and Shaw, 1975, quadrilateral elements Barsoum, 1974,1976, triangular elements

  22. Eight Noded Isoparametric Element shape functions

  23. Eight Noded Isoparametric Element shape functions (continued)

  24. Square-Root Singular Element Banks-Sills and Bortman (1984)

  25. Methods of Calculating KI • Direct Methods • Stress extrapolation • Displacement extrapolation • Indirect Methods • J – integral • Griffith’s energy • Stiffness derivative

  26. Displacement Extrapolation

  27. Displacement Extrapolation (continued) for plane strain

  28. Displacement Extrapolation (continued) for

  29. J -- integral strain energy density tractions J is a conservative integral

  30. J -- integral(continued)

  31. Area J -- integral

  32. Griffith’s Energy

  33. Stiffness Derivative Technique

  34. Results (central crack)

  35. Results (edge crack)

  36. Mixed modes: M – integral

  37. Auxiliary Solutions solution (2a) solution (2b)

  38. Interface Fracture Mechanics

  39. Interface Fracture Mechanics (continued) phase angle or mode mixity energy release rate

  40. Interface Fracture Mechanics (continued)

  41. (1) (2) M – integral

  42. Auxiliary Solutions solution (2a) solution (2b)

  43. Results

  44. Summary • Accurate methods have been presented for calculating stress intensity factors based on energy methods. • The best methods are the area J –integral, stiffness derivative and area M –integral for mixed modes and interface cracks. • The J and M – integrals can be extended for thermal stresses, body forces and tractions along the crack faces. • Conservative integrals have been derived for homo- geneous notches and bimaterial wedges including thermal stresses. • Student wanted for extending these methods to piezo-electric materials

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