Evaluation of plasticity-induced crack closure concept and measurement methods

ASTM Special Technical Publication

Volumn , Issue 1343, 1999, Pages 128-144

  Newman Jr , J C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; COMPUTER SIMULATION; FATIGUE OF MATERIALS; FRACTURE MECHANICS; MATHEMATICAL MODELS; PLASTICITY; STEEL; STRESS INTENSITY FACTORS;

CRACK OPENING STRESS; PLASTICITY-INDUCED CRACK CLOSURE;

CRACK PROPAGATION;

EID: 0033360275     PISSN: 10403094     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (33)

1. Elber, W., "The Significance of Fatigue Crack Closure," Damage Tolerance in Aircraft Structures, ASTM STP 486, American Society for Testing and Materials, 1971, pp. 230-242.
2. Walker, N. and Beevers, C. J., "A Fatigue Crack Closure Mechanism in Titanium," Fatigue and Fracture of Engineering Materials and Structures, Vol. 1, No. 1, 1979, pp. 135-148.
3. Paris, P. C., Bucci, R. J., Wessel, E. T., Clark, W. G., and Mager, T. R., "Extensive Study of Low Fatigue Crack Growth Rates in A533 and A508 Steels," ASTM STP 513, American Society for Testing and Materials, 1972, pp. 141-176.
4. Vasudevan, A. K. and Sadananda, K., "Classification of Fatigue Crack Growth Behavior," Metallurgical and Materials Transactions A, Vol. 26A, May 1995, pp. 1221-1234.
5. Sadananda, K. and Vasudevan, A. K., "Analysis of Fatigue Crack Closure and Thresholds," Fracture Mechanics: 25th Volume, ASTM STP 1220, F. Erdogan, Ed., American Society for Testing and Materials, 1995, pp. 484-501.
6. Chen, D. L., Weiss, B., and Stickler, R., "A New Evaluation Procedure for Crack Closure," International Journal of Fatigue, Vol. 13, No. 4, 1991, pp. 327-331.
7. Donald, J. K., Bray, G. H., and Bush, R. W., "An Evaluation of the Adjusted Compliance Ratio Technique for Determining the Effective Stress Intensity Factor," Fracture Mechanics: 29th Volume, ASTM STP 1331, T. L. Panontin and S. D. Sheppard, Eds., American Society for Testing and Materials, 1997.
8. Marci, G., "Failure Mode Below 390K with IMI 834," Fatigue '96 Proceedings of the Sixth International Fatigue Congress, Berlin, G. Lütjering and H. Nowack, Eds., Vol. I, pp. 493-498.
9. Riddell, W. and Piascik, R. S., "Stress Ratio Effects on Crack Opening Loads and Crack Growth Rates in Aluminum Alloy 2024," Fracture Mechanics: 29th Volume, ASTM STP 1331, T. L. Panontin and S. D. Sheppard, Eds., American Society for Testing and Materials, 1997.
10. Weertman, J., "Rate of Growth of Fatigue Cracks Calculated from the Theory of Infinitesimal Dislocations Distributed on a Crack Plane," International Journal of Fracture, Vol. 2, 1966, pp. 460-467.
11. Tomkins, B., "Fatigue Crack Propagation - An Analysis," Philosophical Magazine, Vol. 18, 1968, pp. 1041-1066.
12. Ogura, K., Miyoshi, Y., and Nishikawa, I., "Fatigue Crack Growth and Closure of Small Cracks at the Notch Root," Current Research on Fatigue Cracks, T. Tanaka, M. Jono, and K. Komai, Eds., Society of Materials Science, Japan, 1985, pp. 57-78.
13. Dowling, N. E. and Begley, J. A., "Fatigue Crack Growth During Gross Plasticity and the J-Integral," Mechanics of Crack Growth, ASTM STP 590, American Society for Testing and Materials, 1976, pp. 82-103.
14. Dugdale, D. S., "Yielding of Steel Sheets Containing Slits," Journal of the Mechanics and Physics of Solids, Vol. 8, 1960, pp. 100-104.
15. Newman, J. C., Jr., "A Crack-Closure Model for Predicting Fatigue Crack Growth under Aircraft Spectrum Loading," Methods and Models for Predicting Fatigue Crack Growth under Random Loading, ASTM STP 748, J. B. Chang and C. M. Hudson, Eds., American Society for Testing and Materials, 1981, pp. 53-84.
16. Newman, J. C., Jr., "FASTRAN-II - A Fatigue Crack Growth Structural Analysis Program," NASA TM 104159, Feb. 1992.
17. Blom, A. R., Wang, G. S., and Chermahini, R. G., "Comparison of Crack Closure Results Obtained by 3D Elastic-Plastic FEM and Modified Dugdale Model," Localized Damage: Computer-Aided Assessment and Control, M. H. Aliabadi et al., Eds., Computational Mechanics Publications, Springer-Verlag, Berlin, 1990, pp. 57-68.
18. Newman, J. C., Jr., "Finite-Element Analysis of Crack Growth under Monotonic and Cyclic Loading," Cyclic Stress-Strain and Plastic Deformation Aspects of Fatigue Crack Growth, ASTM STP 637, American Society for Testing and Materials, 1977, pp. 56-80.
19. Bichler, C. and Pippan, R., this volume, pp. 191-206.
20. Chermahini, R. G., Shivakumar, K. N., and Newman, J. C., Jr., "Three-Dimensional Finite-Element Simulation of Fatigue Crack Growth and Closure," Mechanics of Fatigue Crack Closure, ASTM STP 982, J. C. Newman, Jr. and W. Elber, Eds., American Society for Testing and Materials, 1988, pp. 398-413.
21. Riddell, W. T., Piascik, R. S., Sutton, M. A., Zhao, W., McNeill, S. R., and Helm, J. D., this volume, pp. 157-174.
22. Elber, W., "Crack-Closure and Crack-Growth Measurements in Surface-Flawed Titanium Alloy Ti-6A1-4V," NASA TN D-8010, National Aeronautics and Space Administration, Washington, DC, Sept. 1975.
23. Donald, J. K., "Introducing the Compliance Ratio Concept for Determining Effective Stess Intensity," First International Conference on Fatigue Damage in Structural Materials," Hyannis, MA, Sept. 22-27, 1996.
24. Broek, D., "The Propagation of Fatigue Cracks Emanating from Holes," National Aerospace Laboratory, NLR Technical Report 72134U, 1972.
25. Wu, Yisheng and Schijve, J., "Fatigue Crack Closure Measurements on 2024-T3 Sheet Specimens," Fatigue and Fracture of Engineering Materials and Structures, Vol. 18, 1995, pp. 917-921.
26. Newman, J. C., Jr., "Crack Growth under Variable Amplitude and Spectrum Loading in 2024-T3 Aluminum Alloys," Proceedings of the Symposium on High Cycle Fatigue of Structural Materials, TMS-ASM Fall Meeting, Indianapolis, IN. The Metallurgical Society-American Society for Metals, Sept. 16-18, 1997.
27. Paris, P. C. and Erdogan, F., "Critical Analysis of Crack Propagation Laws," Transactions of ASME, Journal of Basic Engineering, Vol. 85, 1963, pp. 528-534.
28. Dubensky, R. G., "Fatigue Crack Propagation in 2024-T3 and 7075-T6 Aluminum Alloys at High Stress," NASA CR-1732, National Aeronautics and Space Administration, Washington, DC, 1971.
29. Hudson, C. M., "Effect of Stress Ratio on Fatigue-Crack Growth in 7075-T6 and 2024-T3 Aluminum Alloy Specimens," NASA TN D-5390, National Aeronautics and Space Administration, Washington, DC, 1969.
30. Phillips, E. P., "The Influence of Crack Closure on Fatigue Crack Growth Thresholds in 2024-T3 Aluminum Alloy," Mechanics of Fatigue Crack Closure, ASTM STP 982, J. C. Newman, Jr. and W. Elber, Eds., American Society for Testing and Materials, 1988, pp. 505-515.
31. Newman, J. C., Jr., "Fracture Analysis of Various Cracked Configurations in Sheet and Plate Materials," Properties Related to Fracture Toughness, ASTM STP 605, American Society for Testing and Materials, 1976, pp. 104-123.
32. Piascik, R. S. and Newman, J. C., Jr., "An Extended Compact Tension Specimen for Fatigue Crack Growth and Fracture Testing," International Journal of Fracture, Vol. 76, 1996, pp. R43-R48.
33. Newman, J. C., Jr., "Effects of Constraint on Crack Growth under Aircraft Spectrum Loading," Fatigue of Aircraft Materials, A. Beukers, T. deJong, J. Sinke, A. Vlot, and L. B. Vogelesang, Eds., Delft University Press, 1992, pp. 83-109.