FE Modelling and Experimental Evaluation for the Surface Integrity of Thin-Walled Aluminum Alloy

2024-26-0429

06/01/2024

Features
Event
AeroCON 2024
Authors Abstract
Content
The present study discusses the effect of installation torque on the surface and subsurface deformations for thin-walled 7075 aluminum alloy adapters used in Aerospace applications. An FE model was constructed to predict the effect of torque-induced stresses on thin-walled geometry validated with experimentation. A detailed surface analysis was performed on 7075 aluminum to check superficial discontinuities, residual stresses, and grain deformations. The localized strain hardening resulting from increased dislocation density and its effect on surface microhardness was further studied using SEM (Scanning Electron Microscope). The predicted surface level plastic strain of .25%, on the castle nut adapter, was further validated with grain deformations measured using optical and scanning electron microscopy.
Meta TagsDetails
DOI
https://doi.org/10.4271/2024-26-0429
Pages
7
Citation
Yarolkar, M., Harish, U., Patil, S., and Patil, M., "FE Modelling and Experimental Evaluation for the Surface Integrity of Thin-Walled Aluminum Alloy," SAE Technical Paper 2024-26-0429, 2024, https://doi.org/10.4271/2024-26-0429.
Additional Details
Publisher
Published
Jun 01
Product Code
2024-26-0429
Content Type
Technical Paper
Language
English