320
this is not so much at the highest level because critical crack sizes are very sensitive with
respect to the input information. At the highest level, the conservatism was mostly due to
the simplified crack model used as substitute geometry (Fig. 11).
It can be concluded that failure occurred as the consequence of inadequate design and
not of inadmissible handling, such as overloading. The failure could have been avoided
by applying fracture mechanics in the design stage. The SINTAP algorithm was shown to
be an easy, but suitable tool for this purpose.
CONCLUSIONS
The basic principle of the recently developed European SINTAP procedure has been
reviewed. The SINTAP procedure contributes towards the development of a fitness for
service standard of the European Committee for Standardization (CEN). The SINTAP
procedure was applied to
or predicting
the critical size
. Assuming the
loa
in service. The results
reases by increasing the quality of input data.
The Stress Analysis of Cracks Handbook
. ASME Press,
mechanical heterogeneity
gineering approach for elastic-plastic fracture
rt NP-1931, EPRI, Palo Alto, CA. (1981)
7.
the failure analysis of a cracked component, and f
of cracks on both sides of a bore hole in a fork of a forklift
ding by design, an overall critical crack size of 35.6 mm (including both cracks and the
hole) was predicted at the highest analysis level, whereas the real fork had fractured in
service after the overall crack size reached a length of 45.5 mm. This result has shown
that inadequate design could give a sufficient account to failure without any need to
imply further reasons such as inadmissible handling of the forklift
procedure gives reliable conservative results
of the example also showed that SINTAP
ec
where conservatism (e.g. safety factor) d
REFERENCES
1.
SINTAP: Structural Integrity Assessment Procedure. Final Report. EU-Project BE 95-1462.
(1999)
Brite Euram Programme, Brussels.
2.
R.,
Tada, H., Paris, P.C., Irwin, G.
(1998)
3.
Murakami, Y., et al. (Eds.),
Stress Intensity Factor Handbook
, Vol. 1&2 (1987), Vol. 3 (1992),
Pergamon Press, Oxford.
4.
Schwalbe, K-H., Kim, Y-J., Hao, S., Cornec, A., Koçak, M.,
EFAM, ETM-MM96: the ETM
method for assessing significance of crack-like defects in joints with
(strength mismatch)
, GKSS Report 97/E/9. (1997)
5.
Schwalbe, K-H., Zerbst, U, Kim, Y-J., Brocks, W., Cornec A., Heerens J., Amstutz H.,
EFAM
ETM 97: the ETM method for assessing crack-like defects in engineering structures
, GKSS
Report 98/E/6. (1988)
6.
Kumar, V., German, M.D., Shih, C.F.,
An en
analysis
, EPRI-Repo
SINTAP Special issue of Engineering Fracture Mechanics, Vol. 67, Issue 6, pp. 476-668, Dec.
2000
8.
Ainsworth, R.A., Bannister, A.C., Zerbst, U.,
An overview of the European flaw assessment
procedure SINTAP and its validation
, Int. J. Pres. Ves. & Piping, 77, pp. 869-876. (2001)
9.
Zerbst, U., Hamann, R., Wohlschlegel, A.,
Application of the European flaw assessment proce-
dure SINTAP to pipes
, Int. J. Pres. Ves. & Piping, 77, pp. 697-702. (2000)
10. BS 7448: Part 2: 1997:
Fracture mechanics toughness tests, Part 2. Method for determination
of K
Ic
, critical CTOD and critical J values of welds in metallic materials
, British standards
institution, London. (1997)
11. Miller, A.G.,
Review of Limit Loads of Structures Containing Defects
. Int. J. Pres. Ves. &
Piping, 32, pp. 197-327. (1988)




