Evaluation of fatigue crack thresholds using various experimental methods

ASTM Special Technical Publication

Volumn , Issue 1461, 2005, Pages 203-218

  Forth, S C ^a   Forman, R G ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA JOHNSON SPACE CENTER   (United States)

Author keywords

Crack growth; Fatigue; Plasticity induced crack closure; Test methods; Threshold

Indexed keywords

ALUMINUM ALLOYS; CRACKS; DATA ACQUISITION;

PLASTICITY INDUCED CRACK CLOSURE; TEST METHODS; THRESHOLD;

FATIGUE OF MATERIALS;

EID: 33244486530     PISSN: 00660558     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (37)

1. Paris, P.C. and Erdogan, F., "A Critical Analysis of Crack Propagation Laws," Transactions of the ASME, Journal of Basic Engineering, Series D, 85, 3, 1963.
2. Barsom, J.M., "Fatigue-Crack Propagation in Steels of Various Yield Strengths," Transactions of the ASME, Journal of Engineering for Industry, Series B, 93, 4, November 1971.
3. Frost, N.E., "The Growth of Fatigue Cracks," Proceedings of the First International Conference on Fracture, Sendai, Japan, 1966, p. 1433.
4. Bucci, R.J., "Development of a Proposed ASTM Standard Test Method for Near-Threshold Fatigue Crack Growth Rate Measurement" Fatigue Crack Growth Measurement and Data Analysis, ASTMSTP 738, ASTM International, West Conshohocken, PA, 1981, pp. 5-28.
5. "Damage Tolerance and Fatigue Evaluation of Structure", Federal Aviation Regulations, Title 14 Code of Federal Regulations, Part 25, Section 571.
6. Engine Structural Integrity Program (ENSIP), MIL-STD-1783 (United States Air Force), 30, November 1984.
7. Pearson, S., "Initiation of Fatigue Cracks in Commercial Aluminum Alloys and the Subsequent Propagation of Very Short Cracks," Engineering Fracture Mechanics, 7, 2, 1975, pp. 235-247.
8. Taylor, D. and Knott, J.F., "Fatigue Crack Propagation Behavior of Short Cracks - The Effects of Microstructure," Fatigue of Engineering Materials and Structures, 4, 2, 1981, pp. 147-155.
9. Taylor, D. and Knott, J.F., "Growth of Fatigue Cracks from Casting Defects in Nickel Aluminum Bronze," Proceedings of the Metal Society Conference on Defects and Crack Initiation in Environment Sensitive Fracture, University of Newcastle-on-Tyne, 1981.
10. Smith, S.W. and Piascik, R.S., "An Indirect Technique for Determining Closure-Free Fatigue Crack Growth Behavior," Fatigue Crack Growth Thresholds, Endurance Limits, and Design, ASTM STP 1372, ASTM International, West Conshohocken, PA, 2000, pp. 109-122.
11. Herman, W.A., Hertzberg, R.W. and Jaccard, R., "A Simplified Laboratory Approach for the Prediction of Short Crack Behavior in Engineering Structures," Fatigue and Fracture of Engineering Materials and Structures, 11, 4, 1988, pp. 303-320.
12. max Test Procedure to Predict Small Crack Growth Behavior in 2090-T8E41 Aluminum-Lithium Alloy," Scripta Metallurgica, 21, 1987, pp. 1541-1546.
13. Marci, G., "Fatigue Crack Propagation Threshold: What is it and How is it Measured?" Journal of Testing and Evaluation, JTEVA, 26, 3, 1998, pp. 220-233.
14. Haddad, M.H., Topper, T.H. and Smith, K.N., "Prediction of Non Propagating Cracks," Engineering Fracture Mechanics, 11, 3, 1979, pp. 573-584.
15. Newman, Jr., J.C. and Piascik, R.S. (Eds.), Fatigue Crack Growth Thresholds, Endurance Limits, and Design, ASTM STP 1372, ASTM International, West Conshohocken, PA, 2000.
16. Wu, X.J., Wallace, W. and Koul, A.K., "A New Approach to Fatigue Threshold", Fatigue & Fracture of Engineering Materials & Structures, 18, 7/8, 1995, pp. 833-845.
17. Elber, W., "The Significance of Fatigue Crack Closure," Damage Tolerance in Aircraft Structures, ASTM STP 486, ASTM International, West Conshohocken, PA, 1971, pp. 230-242.
18. Chen, D.L., Weiss, B. and Stickler, R., "Effect of Stress Ratio and Loading Condition on the Fatigue Threshold," International Journal of Fatigue, 14, 1992, pp. 325-329.
19. Newman, Jr., J.C. and Elber, W. (Eds.), Mechanics of Fatigue Crack Closure, ASTM STP 982, ASTM International, West Conshohocken, PA, 1988.
20. Forman, R.G., "Study of Fatigue-Crack Initiation from Flaws Using Fracture Mechanics Theory," Air Force Flight Dynamics Laboratory Technical Report AFFDL-TR-68-100, Wright-Patterson Air Force Base, Dayton, Ohio, Sept. 1968.
21. Irwin, G.R., "Linear Fracture Mechanics, Fracture Transition, and Fracture Control," Engineering Fracture Mechanics, 1, 2, Aug. 1968.
22. McClintock, F.A. and Hult, J., "Elastic-Plastic Stress and Strain Distribution Around Sharp Notches in Repeated Shear," Ninth International Congress on Applied Mechanics, New York, 1956.
23. Andrews, W.R. and Shih, C.F., "Thickness and side-groove effects on J- and δ-resistance curves for A533-B steel at 93°C," Elastic-Plastic Fracture, ASTM STP 668, ASTM International, West Conshohocken, PA, 1979, pp. 426-450.
24. Shih, C.F., deLorenzi, H.G. and Andrews, W.R., International Journal of Fracture, 13, 1977, pp. 544-548. [CrossRef]
25. Topper, T.H. and Au, P., "Cyclic strain approach to fatigue in metals," AGARD lecture series 118, Fatigue Test Methodology, The Technical University of Denmark, Denmark, Oct. 19-20, 1981.
26. Conle, A. and Topper, T.H., "Evaluation of small cycle omission criteria for shortening of fatigue service histories," International Journal of Fatigue, Jan. 1979.
27. Pippan, R., Plochl, L., Klanner, F. and Stuwe, H.P., "The Use of Fatigue Specimens Precracked in Compression for Measuring Threshold Value and Crack Growth," Journal of Testing and Evaluation, JTEVA, Vol. 22, No. 2, 1994, pp. 98-103.
28. Forth, S.C., Newman, J.C., Jr., and Forman, R.G., "On Generating Fatigue Crack Growth Thresholds," International Journal of Fatigue, Vol. 25, 2003, pp. 9-15.
29. Shivakumar, K.N. and Newman, Jr., J.C., "Verification of Effective Thicknesses for Side-Grooved Compact Specimens," Engineering Fracture Mechanics, 43, 2, 1992, pp. 269-275.
30. Newman, Jr., J.C., "Stress Analysis of the Compact Specimen Including the Effects of Pin Loading," Fracture Analysis, ASTM STP 560, ASTM International, West Conshohocken, PA, 1974, pp. 105-121.
31. Feddersen, C.E., "Discussion of Plane-Strain Crack Toughness Testing of Metallic Materials," Current Status of Plane Strain Crack Toughness Testing of High-Strength Metallic Materials, ASTM STP 410, ASTM International, West Conshohocken, PA, 1967, pp. 77-79.
32. Hudak, Jr., S.J., Saxena, S.J., Bucci, A. and Malcolm, R.C., "Development of Standard Methods of Testing and Analyzing Fatigue Crack Growth Rate Data - Final Report," AFML TR 78-40, Air Force Materials Laboratory, Wright Patterson Air Force Base, OH, 1978.
33. Saxena, A., Hudak, Jr., S.J., Donald, J.K. and Schmidt, D.W., "Computer-Controlled Decreasing Stress Intensity Technique for Low Rate Fatigue Crack Growth Testing," Journal of Testing and Evaluation, 8, 1, 1980, pp. 19-24.
34. Au, P., Topper, T.H. and El Haddad, M.L., "The Effects of Compressive Overloads on the Threshold Stress Intensity for Short Cracks," Behavior of Short Cracks in Airframe Components, AGARD Conference Proceedings No. 328, pp. 11-1 to 11-7.
35. Newman, Jr., J.C., "An Evaluation of the Plasticity-Induced Crack Closure Concept and Measurement Methods," ASTM STP-1343, ASTM International, West Conshohocken, PA, 1999, pp. 128-144.
36. James, M. A., Forth, S. C., and Newman, J. A., "Load History Effects Resulting from Compression Precracking," Fatigue and Fracture Mechanics: 34th Volume, ASTM 1461, S. R. Daniewicz, J. C. Newman, Jr., and K.-H. Schwalbe, Eds., ASTM International, West Conshohocken, PA, 2004.
37. NASGRO Material Database, www.nasgro.swri.org, 2004.