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Structure of the Deformed 7075 Aircraft Al - Alloy with Material Analysis Using Diffraction (MAUD) |
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PP: 267-274 |
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doi:10.18576/ijtfst/110302
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Author(s) |
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Z. Sayed,
M. Abdel-Rahman,
M. Y. A Mostafa,
M. A. Abdel-Rahman,
E. A. Badawi,
E. E. Assem,
A. Ashour,
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Abstract |
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| This work aims to study the effect of plastic deformation on the 7075 Al - alloy using Material Analyses Using Diffraction (MAUD). Plastic deformation produces dislocation defects. Using a hydraulic press, samples were deformed up to 25%. The XRD was measured for each degree of deformation. The MAUD program was used to analyze the data, and mathematical methods were deployed to understand the various behaviors observed. The lattice parameter, crystallite size, average internal stress, micro-strain, and dislocation density of the 7075Al-alloy were calculated. As the deformation degree increased, there was a progressive decline in the crystallite size as an increase in the micro-strain and dislocation density. The flow stress changes from 5.8 to 49 MPa and the stored dislocation energy varies from 2.62 to 185 kPa.
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