Fatigue of structures and materials in the 20th century and the state of the art

International Journal of Fatigue

Volumn 25, Issue 8, 2003, Pages 679-702

  Schijve, J ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Fatigue mechanism; Fatigue properties; History; Load spectra; Prediction

Indexed keywords

CRACK INITIATION; FATIGUE OF MATERIALS; SPECTRUM ANALYSIS; STRESS ANALYSIS;

LOAD SPECTRA;

KNOWLEDGE ENGINEERING;

EID: 0038136928     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(03)00051-3     Document Type: Review

References (108)

1. Ewing J.A., Humfrey J.C.W. The fracture of metals under repeated alternations of stress. Phil Trans Roy Soc. A200:1903;241-250.
2. Peterson R.E. Discussion of a century ago concerning the nature of fatigue, and review of some of the subsequent researches concerning the mechanism of fatigue. ASTM Bulletin, 164. 1950;50-56 American Society for Testing and Materials.
3. Timoshenko S. Stress concentration in the history of strength of materials. The William M. Murray Lecture. Proc Soc Exp Stress Analysis (SESA). 12:1954;1-12.
4. Hetényi M. Handbook of experimental stress analysis. 1950;John Wiley, New York.
5. Mann J.Y. Aircraft fatigue - with particular emphasis on Australian operations and research. Proc 12th Symp of the Int Committee on Aeronautical Fatigue (ICAF):1983;Centre d'Essais Aéronautique de Toulouse.
6. Schütz W. A history of fatigue. Engng Fract Mech. 54:1996;263-300.
7. Smith R.A. Fatigue crack growth, 30 years of progress. 1986;Pergamon.
8. Sanfor R.J. Selected papers on foundations of linear elastic fracture mechanics. SEM Classic papers, Vol. CP1, SPIE Milestone series, Vol. MS 137. 1997.
9. Hanewinckel D., Zenner H. Fatigue strength, a collection of facsimile, historical papers until 1950. 1989;Technical University, Clausthal.
10. Mann J.Y. Bibliography on the fatigue of materials, components and structures. Vol. 1-4, covering 1838-1969. 1970-1990;Pergamon Press.
11. Schijve J. Fatigue of structures and materials. 2001;Kluwer Academic Publ, Dordrecht, Boston.
12. Gough H.J. Crystalline structure in relation to failure of metals, especially by fatigue. Proc ASTM, American Society for Testing and Materials. 33:1933;3-114.
13. Orowan E. Theory of the fatigue of metals. Proc Roy Soc. A171:1939;79-106.
14. Head A.K. The growth of fatigue cracks. Phil Mag. 44:1953;925-938.
15. Stroh A.N. The formation of cracks as a result of plastic flow. Proc Roy Soc. A223:1955;404.
16. Forsyth P.J.E. The application of 'fractography' to fatigue failure investigations. Roy Aircraft Est, Tech Note Met. 257:1957.
17. Ryder D.A. Some quantitative information obtained from the examination of fatigue fracture surfaces. Roy Aircraft Est, Tech Note Met. 288:1958.
18. Cottrell A.H., Hull D. Extrusion and intrusion by cyclic slip in copper. Proc Roy Soc. A242:1957;211-213.
19. Mott N.F. A theory of the origin of fatigue cracks. Acta Metall. 6:1958;195-197.
20. A discussion on work-hardening and fatigue in metals. Proc Roy Soc Math Phys Sci 1957;242:1229.
21. Averbach B.L., Felbeck D.K., Hahn G.T., Thomas D.A. Proc Int Conf on the Atomic Mechanisms of Fracture. Tech Press, MIT:1959;John Wiley & Sons.
22. Forsyth P.J.E. The physical basis of metal fatigue. 1969;Blackie and Son, London.
23. Backofen W.A. Formation of slip-band cracks in fatigue. Proc Int Conf on the Atomic Mechanisms of Fracture. Tech Press, MIT. 1959;435-449 John Wiley & Sons.
24. Suresh S. Fatigue of materials, 2nd ed. 1998;Cambridge University Press, Cambridge.
25. Fatigue crack propagation, ASTM STP 415. Philadelphia, PA: American Society for Testing and Materials; 1967. p.131-80 and 505-35.
26. Schijve J. The significance of fractography for investigations of fatigue crack growth under variable- amplitude loading. Fatigue Fract Engng Mater Struct. 22:1999;87-99.
27. Bowles CQ. The role of environment, frequency and wave shape during fatigue crack growth in aluminum alloys. Doctor Thesis, Delft University of Technology, 1978.
28. Bowles C.Q., Schijve J. Crack tip geometry for fatigue cracks grown in air and vacuum. ASTM 811. 1983;400-426 American Society for Testing and Materials, Philadelphia, PA.
29. Broek D., de Rijk P., Sevenhuysen P.J. The transition of fatigue cracks in alclad sheet, TR M2100. 1962;Nat Aerospace Laboratory NLR, Amsterdam.
30. Lindley T.C., Richards C.E. The relevance of crack closure to fatigue crack propagation. Mater Sci Eng. 14:1974;281-293.
31. Veer FA. The effect of shear lips, loading transition and test frequency on constant K and constant amplitude fatigue tests. Doctor Thesis, Delft University of Technology, 1993.
32. Zuidema J. Square and slant fatigue crack growth. Doctor Thesis, Delft University of Technology, 1995.
33. Schijve J., Arkema W.J. Crack closure and the environmental effect on fatigue crack growth, Report LR-217. 1976;Delft University of Technology.
34. Paris P.C., Gomez M.P., Anderson W.E. A rational analytical theory of fatigue. The Trend of Engineering. 13:1961;9-14.
35. Irwin G.R. Analysis of stresses and strains near the end of a crack traversing a plate. Trans ASME J Appl Mech. 24:1957;361-364.
36. Pearson S. Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks. Engng Fract Mech. 7:1975;235-247.
37. Wanhill R.J.H. Durability analysis using short and long fatigue crack growth data. Aircraft damage assessment and repair. 1991;Institute of Engineering, Barton, Australia.
38. Miller K.J. The three thresholds for fatigue crack propagation. Fatigue and Fracture Mechanics, 27th vol. ASTM STP 1296. 1997;267-286 American Society for Testing and Materials, Philadelphia, PA.
39. Schijve J. Fatigue crack closure observations and technical significance. Mechanics of fatigue crack closure. ASTM STP 982. 1988;5-34 American Society for Testing and Materials, Philadelphia, PA.
40. Elber W. Fatigue crack propagation. PhD Thesis, University New South Wales, Australia, 1968.
41. Elber W. The significance of fatigue crack closure. Damage tolerance in aircraft structures, ASTM STP 486. 1971;230-242 American Society for Testing and Materials, Philadelphia, PA.
42. Schijve J. Fatigue crack growth under variable-amplitude loading. Fatigue and fracture, ASM handbook, vol. 19. 1996;110-133 ASM International.
43. Coffin L.F. Jr. Low cycle fatigue - a review. Appl Mater Res. 1:1962;129.
44. Manson S.S., Hirschberg M.H. Fatigue behavior in strain cycling in the low- and intermediate-cycle range. Fatigue an Interdisciplinary Approach. 1964;133-178 Syracuse University Press.
45. Stanzl-Tschegg S., Mayer H. Fatigue in the very high cycle regime. Proc Int Conf, July 2001, Inst Meteorology and Physics:2001;University of Agricultural Science, Vienna.
46. Frost N.E., Marsh K.J., Pook L.P. Metal fatigue. 1974;Clarendon, Oxford.
47. A guide for fatigue testing and the statistical analysis of fatigue data. ASTM STP No.91-A. Philadelphia, PA: American Society for Testing and Materials, 1963.
48. Bellows R.S., Muju S., Nicholas T. Validation of the step test method for generating Haigh diagrams for Ti-6Al-4V. Int J Fracture. 21:1999;687-697.
49. Heywood R.B. Designing against fatigue. 1962;Chapman and Hall, London.
50. Ramsden J.M. The geriatric problem. Flight International. 22 Oct:1977;1201-1207.
51. Neuber H. Kerbspannungslehre. Berlin: Springer; 1937 Translated: Theory of Notch Stresses:1946;JW Edwards, Ann Arbor, Michigan.
52. Neuber H. Kerbspannungslehre. Berlin: Springer; 1937 Translated: Theory of Notch Stresses:1946;JW Edwards, Ann Arbor, Michigan.
53. Peterson R.E. Stress concentration factors. 1974;John Wiley & Sons, New York.
54. Kuhn P., Hardrath H.F. An engineering method for estimating notch-size effect in fatigue tests of steel. NACA TN. 2805:1952.
55. Siebel E., Stieler M. Significance of dissimilar stress distributions for cyclic loading. ZVDI. 97:1955;146-148. (in German).
56. Schijve J. Fundamental aspects of predictions on fatigue crack growth under variable-amplitude loading. Blom A.F., Beevers C.J. Theoretical concepts and numerical analysis of fatigue. Proc. Conference of the University of Birmingham:1992;111-130 EMAS.
57. Rooke D.P., Cartwright D.J. Stress intensity factors. 1976;Her Majesty's Stationery Office, London.
58. Tada H., Paris P.C., Irwin G.R. The stress analysis handbook, 2nd ed. 1985;Paris Productions Inc. St Louis.
59. Murakami Y. Stress intensity factors handbook. 1987/1993;Pergamon, Oxford.
60. Pålmgren A. The endurance of ball bearings. Z Ver Deut Ing. 68:1923;339-341. (in German).
61. Langer B.F. Fatigue failure from stress cycles of varying amplitude. J Appl Mech. 4:1937;A160-A162.
62. Miner M.A. Cumulative damage in fatigue. J Appl Mech. 12:1945;A159-A164.
63. Schijve J. Some remarks on the cumulative damage concept. Minutes 4th Conference of the Int Committee on Aero Fatigue (ICAF), Zürich, 1956. Paper 2:1956.
64. Heyer K. Multi-step tests on structural elements, 152. 1943;Lilienthal-Gesellschaft für Luftfahrtforschung, Bericht. (in German).
65. Smith C.R. Fatigue-service life prediction based on tests at constant stress levels. Proc. Soc Exp Stress Analysis (SESA). 16:(1):1958;9.
66. Martin J.F., Topper T.H., Sinclair G.M. Computer based simulation of cyclic stress-strain behavior with applications to fatigue. Mater Res Stand. 11:(23-28):1971;50.
67. Wetzel R.M. Fatigue under complex loading: Analysis and experiments. Advances in Engineering, Vol. 7. 1977;Society of Automotive Engineering.
68. Neuber H. Theory of stress concentration for shear strained prismatical bodies with arbitrary nonlinear stress-strain law. Trans ASME J Appl Mech. 28:1961;544-550.
69. Haibach E. Modified linear damage accumulation hypothesis accounting for a decreasing fatigue strength during increasing fatigue damage, Report TM Nr. 50. 1970;Laboratorium für Betriebsfestigkeit, LBF, Darmstadt. (in German).
70. European Prestandard. European Committee for Standardization, Brussels, May 1998. ENV 1999-2.
71. Hardrath H.F., Naumann E.C. Variable-amplitude fatigue tests on aluminum alloy specimens. ASTM STP 274. 1960;125-138 American Society for Testing and Materials, Philadelphia, PA.
72. Naumann E.C., Hardrath H.R., Guthrie E.C. Axial load fatigue tests of -T3 and 7075-T6 aluminum alloy sheet specimens under constant- and variable-amplitude loads, NASA Report TN D-212. 1959.
73. Schijve J. The accumulation of fatigue damage in aircraft materials and structures, AGARDograph No.157. 1972;Advisory Group for Aerospace Research and & Development.
74. Schijve J. The significance of flight simulation fatigue tests. Durability and damage tolerance in aircraft design. Proc 13th ICAF Symposium Pisa:1985;71-170 EMAS.
75. Schijve J. Fatigue crack propagation in light alloy sheet material and structures. Advances in aeronautical sciences, vol. 3. 1961;387-408 Pergamon Press.
76. Hudson C.M., Hardrath H.F. Effects of changing stress amplitude on the rate of fatigue crack propagation in two aluminum alloys. NASA TN D-960. 1961.
77. Mills W.J., Hertzberg R.W. The effect of sheet thickness on fatigue crack retardation in 2024-T3 aluminum alloy. Engng Fract Mech. 7:1975;705-711.
78. Petrak G.S. Strength level effects on fatigue crack growth and retardation. Engng Fract Mech. 6:1974;725-733.
79. Willenborg J, Engle RM, Wood HA. A crack growth retardation model using an effective stress concept. Air Force Flight Dynamic Laboratory, Dayton, Report AFFDL-TR71-1, 1971.
80. Wheeler O.E. Spectrum loading and crack growth. ASME Trans J Basic Engng. 94:1972;181-186.
81. Padmadinata UH. Investigation of crack-closure prediction models for fatigue in aluminum sheet under flight-simulation loading. Doctor Thesis, Delft University of Technology, 1990.
82. de Koning A.U. A simple crack closure model for prediction of fatigue crack growth rates under variable-amplitude loading. ASTM STP 743. 1981;63-85 American Society for Testing and Materials, Philadelphia, PA.
83. Padmadinata U.H., Schijve J. Prediction of fatigue crack growth under flight-simulation loading with the modified CORPUS model. Harris C.E. Advanced structural integrity methods for airframe durability and damage tolerance. 1994;547-562 NASA Conf Publ.
84. Dugdale D.S. Yielding of steel sheets containing slits. J Mech Phys Solids. 8:1960;100-104.
85. Dill H.D., Saff C.R. Spectrum crack growth prediction method based on crack growth surface displacement and contact analysis. ASTM STP 595. 1976;306-319 American Society for Testing and Materials, Philadelphia, PA.
86. Dill H.D., Saff C.R., Potter J.M. Effects of fighter attack spectrum and crack growth. ASTM STP 714. 1980;205-217 American Society for Testing and Materials, Philadelphia, PA.
87. Newman J.C. Jr. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. ASTM STP 748. 1981;53-84 American Society for Testing and Materials, Philadelphia, PA.
88. Dougherty D.J., de Koning A.U., Hillberry B.M. Modelling hgh crack growth rates under variable amplitude loading. ASTM STP 1122. 1992;214-233 American Society for Testing and Materials, Philadelphia, PA.
89. Wang G.S., Blom A.F. A strip model for fatigue crack growth predictions under general load conditions. Engng Fract Mech. 40:1991;507-533.
90. Gassner E. Strength experiments under cyclic loading in aircraft structures. Luftwissen. 6:1939;61-64. (in German).
91. Teichmann A. Basic consideration on fatigue durability in service (in German). Jahrbuch der Deutschen Luftfahrtforschung. 1:1941;467-471.
92. Seewald F. Measurements with a glass scratching recorder of the German Institute for Aeronautics. Maschinenbau. 10:1931;725-727. (in German).
93. Taylor J. Measurements of gust loads in aircraft. J Roy Aero Soc. 57:1953;78-88.
94. Data of the Fokker Aircraft Industry, 1980.
95. Proc. 20th Symp. Aircraft integrated monitoring systems 2000. Tech University Münich, Faculty Maschinenwesen, 2000.
96. Murakami Y. The rainflow method in fatigue, The Tatsuo Endo memorial volume. 1992;Butterworth-Heinemann, Oxford.
97. Burns A. Fatigue loadings in flight: Loads in the tailplane and fin of a Varsity. 1956;ARC Technical Report CP 256, London.
98. Standard practices for cycle counting in fatigue analysis. ASTM Standard E 1049-90. American Society for Testing and Materials 1990.
99. Branger J. The full-scale fatigue test on the DH-112 Venom. Eidgenossische Flugzeugwerk Emmen. 1964;. Report F&W S-162.
100. Schijve J. Fatigue predictions and scatter. Fatigue Fract Engng Mater Struct. 17:1994;381-396.
101. Adenstedt R. Scatter of the fatigue strength (in German). Doctor Thesis, Technical University of Clausthal, 2001.
102. Radai D. Review of fatigue strength assessment of nonwelded and welded structures based on local parameters. Int J Fatigue. 18:1996;153-170.
103. Skorupa M. Load interaction effects during fatigue crack growth under variable amplitude loading - A literature review. Part I: Empirical trends, Part II: Qualitative interpretation. Fatigue Fract Engng Mater Struct. 21/22:2001;987-1006.
104. Goranson U.G. Continuous airworthiness of aging aircraft. Proc 2nd Annual International Conference on Aging Aircraft:1989;61-89 Federal Aviation Adm US Dept of Trans, Baltimore.
105. Saff C.R., Holloway D.R. Evaluation of crack growth gages for service life tracking. Fracture mechanics. 13th Conf, ASTM STP 743:1981;623-640 American Society for Testing and Materials.
106. Wanhill R.J.H., de Graaf E.A.B., Delil A.A.M. Significance of a rotor blade failure for fleet operation, inspection, maintenance, design and certification. Fifth European rotorcraft and powered lift aircraft forum, Amsterdam, 4-7 September:1979;. Paper 38.
107. Flatau A.G., Chong K.P. Dynamic smart material and structural systems. Engng Struct. 24:2002;261-270.
108. Miller KJ. Structural integrity - whose responsibility? The Institution of Mechanical Engineers, The 36th John Player Memorial Lecture, 2001.