The Crack Length Growth – A Fracture Parameter in a Stainless Steel Influenced by the Loading Test

Article Preview

Abstract:

The defects or micro-cracks that exist in a product mass from the elaboration phase, can extend controlled or not, because of a variable solicitation applied to a product or a sample. The Fracture Mechanics parameter that highlight the crack propagation in time is its rate growth marked as da/dN and represents the crack advancement length during a solicitation cycle. This can be studied based on some mathematical models obtained from some propose models, experimentally determined. In this paper, a propagation process analysis is made of a fracture crack by an axial-eccentric fatigue loading for a 10TiNiCr175 stainless steel. CT type flat samples were loaded with an asymmetry coefficient R= 0.3, for the solicitation temperatures: T= 293K (20°C), T= 253K (-20°C), respectively T= 213 K (-60°C). The crack growth increase was studied by three most used mathematical models: the polynomial method standardized according to ASTM E647, method proposed by Paris and method proposed by Walker.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

489-494

Citation:

Online since:

January 2016

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2016 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] J. Cardinal, et. al., Fatigue Crack Growth Equations for TC-128 B Tank Car Steel, Final Report, Sw R1 Project 18. 12240. 01. 006, Cambridge, UK, October, (2006).

Google Scholar

[2] D.M. Constantinescu, Structural integrity, University ˝Politehnica˝ Bucharest, (1998).

Google Scholar

[3] D. Cioclov, Materials fracture mechanics, Romanian Academy Publishing House, Bucharest, (1977).

Google Scholar

[4] I. Dumitru, L. Marşavina, Elements of fracture mechanics – course, University Politehnica Timişoara, (2000).

Google Scholar

[5] J.C. Jr. Newman, A Crack-Opening Stress Equation for Fatigue Crack Growth, International Journal of Fracture, 24 (1984), R131-R135.

DOI: 10.1007/bf00020751

Google Scholar

[6] J.C. Jr., Newman, Phillips, E.P., and Everet, R.A., Fatigue analyses under constant and variable amplitude loading using small-crack theory, NASA/TM-1999-209329, ARL-TR, (2001).

Google Scholar

[7] T. Pană, Şt. D. Pastramă, Mechanicals structures integrity, Fair Partners Publishing House, Bucharest, (2000).

Google Scholar

[8] V. Roşca, Contributions to the mono-axial fatigue study at low temperatures, Phd. Thesis, University Politehnica of Bucharest, (1997).

Google Scholar

[9] V. Roşca, Modern concepts regarding the mechanical structures fracture, Universitaria Publishing House, Craiova, (2002).

Google Scholar

[10] O. Rusu, M. Teodorescu, N. Laşcu-Simion, Materials fatigue, vol. 1 – Calculus bases, vol. 2 – Engineering applications, Technical Publishing House, Bucharest (1992).

Google Scholar

[11] E.K. Walker, The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7076-T6 aluminium. In: Effect of Environment and complex load history on fatigue life, ASTM STP 462, Philadelphia, American Society for Testing and Materials, (1970).

DOI: 10.1520/stp32032s

Google Scholar

[12] ASTM E647-95, Standard Test Method for Measurement of Fatigue Crack Growth Rates, American National Standard.

Google Scholar

[13] V. Roşca, C.M. Miriţoiu, M. Rădulescu, Comparisons between different models for the cracking rate, International congress Science and Management of Automotive and Transportation Engineering SMAT 2014, 2 (2014), 119-125.

Google Scholar