Title variants
Languages of publication
Abstracts
The determination of fracture toughness of aluminium alloy aviation parts, exposed to cyclic mechanical loading, is an important engineering issue. The service life and crack resistance of such unprotected metallic parts is limited under corrosive operating conditions. The resistance against fracture cracking and corrosion resistance can be increased by the surface coatings. The scientific research of fracture toughness of coated metallic parts is being carried out in a comprehensive way. In this research, fracture toughness behaviour of high velocity oxy-fuel (HVOF) spray coated and conventional hard chrome plated aluminium-zinc alloy parts were compared and the results are discussed. The fracture surfaces are investigated and fracture toughness values are calculated. Electron microscopy analysis revealed significant differences in crack growth morphology and toughness values. As a result, the fracture toughness value is higher in hard chrome plated parts.
Discipline
- 46.50.+a: Fracture mechanics, fatigue and cracks(see also 62.20.M- Structural failure of materials in mechanical properties of condensed matter)
- 81.40.Np: Fatigue, corrosion fatigue, embrittlement, cracking, fracture, and failure(see also 62.20.M- Structural failure of materials)
- 61.82.Bg: Metals and alloys
Journal
Year
Volume
Issue
Pages
926-929
Physical description
Dates
published
2017-09
Contributors
author
- Sakarya University, Technology Faculty, Metallurgy and Materials Engineering Department, Sakarya, Turkey
author
- Sakarya University, Engineering Faculty, Mechanical Engineering Department, Sakarya, Turkey
References
- [1] M.O. Lai, W.G. Ferguson, Mater. Sci. Engin. 74, 133 (1985), doi: 10.1016/0025-5416(85)90426-4
- [2] R. Clark Jr, B. Coughran, I. Traina, et al., Engin. Failure Anal. 12, 520 (2005), doi: 10.1016/j.engfailanal.2004.09.005
- [3] S. Mohan Kumar, R. Pramod, M.E. Shashi Kumar, H.K. Govindaraju, Procedia Engin. 97, 178 (2014), doi: 10.1016/j.proeng.2014.12.240
- [4] E.S. Puchi-Cabrera, et al., Int. J. Fatigue 28, 1854 (2006), doi: 10.1016/j.ijfatigue.2005.12.005
- [5] J.A. Picas, A. Forn, G. Matthau, Wear 261, 477 (2006), doi: 10.1016/j.wear.2005.12.005
- [6] Z. Bergant, U. Trdan, J. Grum, Int. J. Fatigue 87, 444 (2016), doi: 10.1016/j.ijfatigue.2016.02.027
- [7] A.Z. Zakaria, K. Shelesh-Nezhad, T.N. Chakherlou, A. Olad, Engin. Fracture Mech. 172, 139 (2017), doi: 10.1016/j.engfracmech.2017.01.004
- [8] ASTM B 645-02 Practice for plane-strain fracture toughness testing of aluminium alloys
- [9] ASTM E 399-99 Standard test method for plane-strain fracture toughness of metallic materials
Document Type
Publication order reference
Identifiers
YADDA identifier
bwmeta1.element.bwnjournal-article-app132z3-iip033kz