Fatigue Crack Growth of Alloy 7050-T7451 Plate in L-S Orientation

Article Preview

Abstract:

Experiments have been conducted to investigate the crack growth characteristics of 7050-T7451 aluminium plate in L-S orientation. Two loading conditions are selected, i.e. constant amplitude and constant stress intensity factor range (ΔK). The effects of ΔK-levels and stress ratios (R) on crack splitting are studied. Test data shows that crack splitting could result in the reverse of crack growth rate trend with the increasing R ratio at high ΔK-level. The appearance of crack splitting depends on both ΔK and R.

You might also be interested in these eBooks

Info:

Periodical:

Key Engineering Materials (Volumes 525-526)

Pages:

221-224

Citation:

Online since:

November 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Alcoa Mill Products: 7050 Aluminium Alloy Plate and Sheet; Website (accessed Aug. 2009): http: /www. alcoa. com/mill_products/catalog/pdf/alloy7050techsheetrev. pdf.

DOI: 10.1002/9780470114735.hawley00375

Google Scholar

[2] J J Schubbe. Fatigue crack propagation in 7050-T7451 plate alloy, Eng Frac Mech, 76(2009): 1037-1048.

DOI: 10.1016/j.engfracmech.2009.01.006

Google Scholar

[3] P White, S A Barter, C Wright. Small crack growth rates from simple sequences containing underloads in AA7050-T7451, Int J Fatigue, 31 (2009) 1865–1874.

DOI: 10.1016/j.ijfatigue.2009.01.014

Google Scholar

[4] J J Schubbe. Evaluation of fatigue life and crack growth rates in 7050-T7451 aluminum plate for T-L and L-S oriented failure under truncated spectra loading, Eng Fail Anal, 16(2009): 340-349.

DOI: 10.1016/j.engfailanal.2008.05.009

Google Scholar

[5] R Bao, X Zhang. Fatigue crack growth behaviour and life prediction for 2324-T39 and 7050-T7451 aluminium alloys under truncated load spectra, Int J Fatigue 32 (2010) 1180–1189.

DOI: 10.1016/j.ijfatigue.2009.12.010

Google Scholar

[6] AFGROW – US Air Force Crack Growth Software; V4. 12. 15. 0, (2009).

Google Scholar

[7] K Walker. The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum, ASTM STP 462, American Society for Testing and Materials, (1970).

DOI: 10.1520/stp32032s

Google Scholar