Both standard and non-standard compact specimens were employed to experimentally study the crack growth behavior of 7075-T651 aluminum alloy in ambient air. The effects of the stress ratio (R), overloading, underloading, and high-low sequence loading on fatigue crack growth rate were investigated. S
A microscopic study of crack initiation mechanisms in 7075 aluminum alloy sheets
โ Scribed by D.L. Jones; H. Liebowitz
- Publisher
- Elsevier Science
- Year
- 1973
- Tongue
- English
- Weight
- 950 KB
- Volume
- 5
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
Ah&act-A study of the opening mode of crack initiation in 7075-T6 aluminum alloy sheets has been conducted with the aid of a scann@ electron micnxcope. Observations were made from several orientations including the top view of the specimen which showed the notch profile and the edge view of the specimen which showed the entire notch front along the specimen thickness. It was found that the edge view exhibited thefhatsifnsolpsrmMentdcformationatabout55percsntobtbebraaldaOstrroeth.Thesec~stodr theformotdeformstionbnndswhichwere~inthedirectionofthetensilesxisaadapperently&~ limiting regions of homogeneous slip. It is felt that the apptamnce of mkrocrxks at loads approaching the br+@!streagtbwf@ fundamentalimpoWnccintbeformationdthe~fRcturrsurface.ManyoftheK m were i&i&d at intermeu& particles and other met&~@cally weak qions on the notch su&ce. It was also possible to carrelate the strain in the notch with the stress intensity factor for the various loads. Very large plastic strains were observed on the notch tip as compar4 to published values of elongation at-for lmnot&dspecimens.
๐ SIMILAR VOLUMES
Three-dimensional finite element analysis of a bicrystal using a crystal plasticity constitutive theory was performed to compute the maximum plastic shear strain range Dc p max in the matrix, at the particle/matrix interface, and at the bicrystal boundary. Using the finite element analysis results,
Three-dimensional finite element analysis using a crystal plasticity constitutive theory was performed to understand and quantify various parametric effects on microstructurally small fatigue crack growth in a AA7075 aluminum alloy. Plasticity-induced crack opening stresses (S o /S max ) were comput