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Microstructurally small fatigue crack growth in thin, aluminum-alloy, pressure vessel liner

โœ Scribed by Ashley Spear; Anthony Ingraffea


Publisher
Elsevier
Year
2011
Tongue
English
Weight
719 KB
Volume
10
Category
Article
ISSN
1877-7058

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โœฆ Synopsis


Motivation to decrease weight and cost of composite-overwrapped pressure vessels used in space exploration leads to designs that challenge the current qualification standards and methods for predicting fatigue life of the structures. Namely, as thickness of the metallic, overwrapped liners is reduced (potentially to tens of grains through-thickness), plastic deformation extends to the liner bounds, and linear elastic fracture parameters become invalid for fatigue crack growth characterization. In this case, fatigue crack growth is likely governed by microstructural features of the material. Life predictions should ultimately reflect this microstructural dependence. In this work, we design a study that involves both experimental and computational modeling aspects to gain three-dimensional perspective of the microstructural features influencing fatigue crack growth in a thin aluminum alloy reminiscent of a metallic liner material. High-energy X-ray diffraction microscopy is explored as a method for characterizing microstructural morphology, including crystallographic orientations, in a volume of material containing a microstructurally small fatigue crack. Initial work involves a feasibility study of the material form (rolled sheet versus actual liner material) to be used in the proposed experimental study. An outlook on future work of the study is provided.


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Three-dimensional finite element analysi
โœ L. Wang; S.R. Daniewicz; M.F. Horstemeyer; S. Sintay; A.D. Rollett ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 520 KB

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