Quantitative assessment of impact damage in stitched foam‐filled Aluminium honeycomb Sandwich panels by experimental and machine learning methods
Authors:
- 24 June 2024
- journal article
- research article
- Published by Wiley in Polymer Composites
- Vol. 45 (15) , 13663-13675
Abstract
Novel Stitched Foam‐filled Honeycomb Sandwich (SFHS) panels have been fabricated using vacuum‐assisted resin transfer molding to address the weak interfaces between the face sheets and the core in the Foam‐filled Honeycomb Sandwich (FHS) panel. The SFHS panels have shown better load‐bearing capacity and performance characteristics compared to FHS panel after Low‐Velocity Impact (LVI) tests. After the LVI test, MATLAB image processing was used to analyze the impact damage areas and failure mechanisms. In addition, Machine Learning regression algorithms were employed to predict the optimal amount of energy absorbed during low‐velocity impact testing of fabricated panels with a maximum impactor drop height of 700 mm. The results indicated that nylon yarn stitching significantly improved energy absorption and interfacial behavior compared to unstitched honeycomb panels. This research also revealed that SFHS1 panels with adjacent honeycomb cell stitching are more impact resistant, provide increased load carrying capacity, and are cost‐effective. These panels can be utilized by modern engineers to increase economy, durability, and functionality in industrial, automotive, and construction applications.Highlights: Stitched Foam Filled Honeycomb Sandwich (SFHS) panels, manufactured via resin transfer molding, and eliminates weak interfaces between the face sheets and core. SFHS panels outperformed unstitched panels in load‐bearing and energy absorption during low‐velocity impact, as confirmed by MATLAB image analysis showing reduced damage and failure. Machine learning algorithms particularly polynomial regression model predicted maximum absorption energy precisely with 99.9% accuracy, close to experimental results. SFHS panels can be used in automotive and industrial applications due to their through‐thickness stitching.Keywords
This publication has 38 references indexed in Scilit:
- Impact characterization on thin structures using machine learning approachesChinese Journal of Aeronautics, 2023
- Compression after multiple impact strength of composite laminates prediction method based on machine learning approachAerospace Science and Technology, 2023
- On the structural parameters of honeycomb-core sandwich panels against low-velocity impactComposites Part B: Engineering, 2021
- Influence of interfacial adhesive on impact and post-impact behaviors of CFRP/end-grain balsawood sandwich compositesComposites Part B: Engineering, 2021
- Low-velocity impact response and compression after impact behavior of tubular composite sandwich structuresComposites Part B: Engineering, 2020
- Damage and failure mechanism of thin composite laminates under low-velocity impact and compression-after-impact loading conditionsComposites Part B: Engineering, 2019
- Low-velocity impact tests on carbon/epoxy composite laminates: A benchmark studyComposites Part B: Engineering, 2016
- Enhanced mechanical performance of foam core sandwich composites with through the thickness reinforced coreComposites Part B: Engineering, 2015
- A digital image analysis to evaluate delamination factor for wind turbine composite laminate bladeComposites Part B: Engineering, 2012
- Effect of stitch density and stitch thread thickness on low-velocity impact damage of stitched compositesComposites Part A: Applied Science and Manufacturing, 2010