105
4.2.7. Analysis of crack growth data
The two major aspects of FCGR test analysis are to ensure suitability of the test data and
to calculate growth rates from the data. The analysis also may require the calculation of
fatigue crack closure level and the analysis of fracture surface and metallography. It is
essential that computer-controlled tests generate records of
a
vs.
N
and FCGR. It is
prescribed
to ensure the validity of the test data and make corrections to the crack length,
if necessary (ASTM E 647).
At the end of the test, the final crack length is measured on both sides of the specimen.
The error between the final measured and predicted crack size is linearly distributed over
the crack extension range. If periodic optical measurements were made during the test,
other more appropriate correction procedures can be used.
REFERENCES
1.
D.W. Cameron, and D.W. Hoeppner,
"Fatigue and Fracture"
, ASM Handbook Vol. 19, 2005.
2.
A. Wöhler, Versuche über die Festigkeit der Eisenbahnwagenachsen, Zeitschrift für Bauwesen,
1860.
3.
"Dynamically Loaded Structures"
, AWS Structural Welding Code, ANSI/AWS D1.1-92, American
Welding Society, 1992, p 185-201.
4.
C. Lipson, G.C. Noll, and L.S. Clock,
"Stress and Strength of Manufactured Parts"
, McGraw-Hill,
1950.
5.
J.E. Shigley and L.D. Mitchell, Mechanical Engineering Design, McGraw-Hill, 4th ed., 1983.
6.
H.O. Fuchs and R.I. Stephens, Metal Fatigue in Engineering, John Wiley and Sons, 1980.
7.
J.A. Bannantine, J.J. Comer, and J.L. Handrock,
"Fundamentals of Metal Fatigue Analysis"
,
Prentice-Hall, 1990.
8.
Fatigue Design Handbook, Society of Automotive Engineers, 2nd ed., 1988.
9.
ASTM E 468-90,
"Standard Practice for Presentation of Constant Amplitude Fatigue Test
Results for Metallic Materials"
, Annual Book of ASTM Standards, Vol 03.01, ASTM, 1995.
10. M. Burzić, MSc Thesis, Faculty of Technology and Metallugry, Belgrade, 2001.
11. R.C. Juvinall,
"Engineering Considerations of Stress, Strain, and Strength"
, McGraw-Hill,
1967, p 274.
12. MIL-HDBK-5D,
"Military Standardization Handbook"
, Metallic Materials and Elements for
Aerospace Vehicle Structures, 1983, p 3-164.
13. ASTM D 671-93,
"Test Method for Flexural Fatigue of Plastics by Constant-Amplitude-of-
Force"
, Annual Book of ASTM Standards, Vol 08.01, ASTM, 1995.
14. A. Moet and H. Aglan,
"Fatigue Failure, Engineering Plastics"
, Vol 2, Engineered Materials
Handbook, ASM International, 1988, p 742.
15. D. Broek,
"The Practical Use of Fracture Mechanics"
, Kluwer Academic Publishers, 1989, p
52.
16. M. Burzić, PhD Thesis, University of Novi Sad, Faculty of Technical Sciences, Serbia, 2008.
17. M. Burzić, R. Prokić-Cvetković, B. Grujić, I. Atanasovska, Ž. Adamović,
"Safe Operation of
Welded Structure with Cracks at Elevated Temperature"
, Strojniški Vestnik - Journal of
Mechanical Engineering, 2008, Vol. 54, No. 11, pp. 807-816.
18. P.C. Paris, and F. Erdogan, J. Basic Eng. (TRANS. ASME), Series D,Vol. 85,1963, p.528-534.
19. P.C. Paris, Proc. 10th Sagamore Conf., Syracuse University Press, 1965, p. 107-132.
20. J.R. Griffits and C.E. Richards, Mater. Sci. Eng., Vol. 11, 1973, p. 305-315.
21. M. Burzić, Ž. Adamović,
"Experimental Analysis of Crack Initiation and Growth in Welded
Joint of Steel for Elevated Temperature"
, Materials and Tehnology, 2008, Vol .42 No. 6, pp.
263-271.