Abstract
The strength, fracture toughness and fatigue crack growth resistance of 7050-T7451 aluminum alloy plate with different thicknesses (35 mm and 160 mm) were investigated by means of optical microscope, scanning electron microscope and transmission electron microscope. The results show that thicker plate has lower strength and fracture toughness but higher fatigue crack growth resistance, by comparison to the thinner plate. The drop of strength is mainly attributed to grain coarsening in the thicker plate, and the increased degree of recrystallization results in the loss of K IC. However, the coarsened grains in the thicker plate make cracks deflected and closure effect enhanced due to surface roughness increased. For both of plates, in the fracture surface subjected plain strain, a transition from transgranular dimpled fracture to intergranular dimpled fracture is observed during the fracture process.
Similar content being viewed by others
References
WILLIAM C, JOHN L, JAMES T. Aluminum alloys for aircraft structure [J]. Advanced Materials and Processes, 2002, 160(12):27–29.
HEINZ A, HASZLER A, KEIDEL C. Recent development in aluminum alloys for aerospace applications [J]. Materials Science and Engineering: A, 2000, 280(1):102–107.
HATAMLEH O, SINGH P M, GARMESTANI H. Corrosion susceptibility of peened friction stir welded 7075 aluminum alloy joints [J]. Corrosion Science, 2009, 51(1):135–143.
YOU J H, LIU S D, ZHANG X M. Influence of quench transfer time on microstructure and mechanical properties of 7055 aluminum alloy [J]. Journal of Central South University of Technology, 2008, 15(2):153–158.
de CAMARGO J A M, CORNELIS H J, CIOFFI V M O H. Coating residual stress effects on fatigue performance of 7050-T7451 aluminum alloy [J]. Surface and Coatings Technology, 2007, 201(24):9448–9455.
ALRUBAIE K S, DEL GRANDE M A, TRAVESSA D N. Effect of pre-strain on the fatigue life of 7050-T7451 aluminum alloy [J]. Materials Science and Engineering: A, 2007, 464(1/2):141–150.
PRZYSTUPA M A, BUCCI R J, MAGNUSEN P E. Microstructure based fatigue life predictions for thick plate 7050-T7451 airframe alloys [J]. International Journal of Fatigue. 1997, 19(93):285–288.
SCHUBBE J J. Plate Thickness variation effects on crack growth rates in 7050-T7451 alloy thick plate [J]. Journal of Materials Engineering and Performance, 2011, 20(1):147–154.
CVIJOVIC Z, RAKIN M, VRATNICA M. Microstructural dependence of fracture toughness in high-strength 7000 forging alloys [J]. Engineering Fracture Mechanics, 2008, 75(8):2115–2129.
DU Feng-shan, YAN Liang, DAI Sheng-long, YANG Shou-jie. Study on fatigue performance of high strength aluminum alloy [J]. Journal of Aeronautical Materials, 2009, 29(1):96–100. (in Chinese)
ROBSON J D, PRANGNELL P B. Predicting recrystallised volume fraction in aluminum alloy 7050 hot rolled plate [J]. Materials Science and Technology, 2002, 18(6):607–614.
HAN N M, ZHANG X M, LIU S D. Effect of solution treatment on the strength and fracture toughness of aluminum alloy 7050 [J]. Journal of Alloys and Compounds, 2011, 509(10):4138–4145.
SATO Y S, URATA M, KOKAWA H. Hall-Petch relationship in friction stir welds of equal channel angular-pressed aluminum alloys [J]. Materials Science and Engineering: A, 2003, 354(1/2):298–305.
DUMONT D, DESCHAMPS A, BRECHET Y. On the relationship between microstructure, strength and toughness in AA7050 aluminum alloy [J]. Materials Science and Engineering: A, 2003, 356(1/2):326–336.
STARINK M J, GAO N. Relations between microstructure, precipitation, age-formability and damage tolerance of Al-Cu-Mg-Li (Mn,Zr,Sc) alloys for age forming [J]. Materials Science and Engineering: A, 2006, 418:241–249.
PEDERSEN K O, BORVIK T, HOPPERSTAD O S. Fracture mechanisms of aluminium alloy AA7075-T651 under various loading conditions [J]. Materials & Design, 2011, 32(1):97–107.
GOKHALE A, DESHPANDE N, DENZER D. Relationship between fracture toughness, fracture path, and microstructure of 7050 aluminum alloy: Part II. Multiple micromechanisms-based fracture toughness model [J]. Metallurgical and Materials Transactions A, 1998, 29(4):1203.
SURESH S. Further remarks on the micromechanisms of fatigue crack growth retardation following overloads [J]. Engineering Fracture Mechanics, 1985, 21(6):1169–1170.
BASAVAKUMAR K G, MUKUNDA P G, CHAKRABORTY M. Influence of grain refinement and modification on microstructure and mechanical properties of Al-7Si and Al-7Si-2.5Cu cast alloys [J]. Materials Characterization, 2008, 59(3):283–289.
KAMP N, GAO N, STARINK M J. Analytical modelling of the influence of local mixed mode displacements on roughness induced crack closure [J]. International Journal of Fatigue, 2007, 29(5):897–908
Author information
Authors and Affiliations
Corresponding author
Additional information
Foundation item: Project(2012CB619503) supported by State Key Fundamental Research Program of China
Rights and permissions
About this article
Cite this article
Wang, Yl., Pan, Ql., Wei, Ll. et al. Fracture toughness and fatigue crack growth analysis of 7050-T7451 alloy thick plate with different thicknesses. J. Cent. South Univ. 21, 2977–2983 (2014). https://doi.org/10.1007/s11771-014-2265-0
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11771-014-2265-0