Quantitative assessment of impact damage in stitched foam-filled Aluminium honeycomb Sandwich panels by experimental and machine learning methods

被引:0
|
作者
Dhanesh, E. [1 ]
Nagarajan, V. A. [1 ]
Kumar, K. P. Vinod [2 ]
Karthik, B. [2 ]
机构
[1] Univ Coll Engn, Dept Mech Engn, Nagercoil 629004, Tamil Nadu, India
[2] Univ Coll Engn, Dept Chem, Nagercoil, India
关键词
low-velocity impact; machine learning; MATLAB; regression analysis; sandwich panels; stitching; LOW-VELOCITY IMPACT; MECHANICAL PERFORMANCE; CAI BEHAVIOR; COMPRESSION; COMPOSITES; CORE;
D O I
10.1002/pc.28726
中图分类号
TB33 [复合材料];
学科分类号
摘要
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. Process for manufacturing and testing SFHS panels. image
引用
收藏
页码:13663 / 13675
页数:13
相关论文
共 35 条
  • [21] Response of aluminium honeycomb sandwich panels under combined shock and impact loading: Experimental and numerical investigations
    Li, Lang
    Jia, Fusen
    Liu, Lu
    Yu, Runpei
    Zhang, Qiancheng
    Li, Lei
    THIN-WALLED STRUCTURES, 2023, 193
  • [22] Compression and low velocity impact response of sandwich panels with polyester pin-reinforced foam filled honeycomb core
    Jayaram, R. S.
    Nagarajan, V. A.
    Kumar, K. P. Vinod
    JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2019, 21 (06) : 2014 - 2030
  • [23] Dynamic response of Nomex honeycomb sandwich panels subjected to aluminum foam projectile impact-An experimental study
    Deng, Yunfei
    Hu, Xiaoyu
    Yang, Xiaoyue
    Huang, Ziqiang
    Wang, Yuetong
    Zhou, Chunping
    POLYMER COMPOSITES, 2023, 44 (02) : 1017 - 1037
  • [24] Experimental and numerical study on compression-after-impact behavior of composite panels with foam-filled hat-stiffener
    Liu, Da
    Bai, Ruixiang
    Lei, Zhenkun
    Guo, Jingjing
    Zou, Jianchao
    Wu, Wen
    Yan, Cheng
    OCEAN ENGINEERING, 2020, 198
  • [25] Experimental investigation of adhesive fillet size on barely visible impact damage in metallic honeycomb sandwich panels
    Kendall, Patrick
    Sun, Mengqian
    Wowk, Diane
    Mechefske, Christopher
    Kim, Il Yong
    COMPOSITES PART B-ENGINEERING, 2020, 184 (184)
  • [26] Experimental and numerical study on compression-after-impact behavior of composite panels with foam-filled hat-stiffener
    Liu, Da
    Bai, Ruixiang
    Lei, Zhenkun
    Guo, Jingjing
    Zou, Jianchao
    Wu, Wen
    Yan, Cheng
    Ocean Engineering, 2021, 198
  • [27] Low-velocity impact properties of foam-filled composite lattice sandwich beams: Experimental study and numerical simulation
    Chen, Chen
    Fang, Hai
    Zhu, Lu
    Han, Juan
    Li, Xiaolong
    Qian, Zhen
    Zhang, Xinchen
    COMPOSITE STRUCTURES, 2023, 306
  • [28] An experimental and numerical investigation of core damage size in honeycomb sandwich panels subject to low-velocity impact
    Wowk, D.
    Reyno, T.
    Yeung, R.
    Marsden, C.
    COMPOSITE STRUCTURES, 2020, 254
  • [29] High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods
    Bilgin, Mustafa
    Usta, Fatih
    Turkmen, Halit S.
    Yolum, Ugur
    2023 10TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN AIR AND SPACE TECHNOLOGIES, RAST, 2023,
  • [30] Experimental and analytical study on impact response of stainless steel-aluminium foam-alloy steel sandwich panels
    Liu, Kun
    Kang, Shao-Bo
    Gao, Shan
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2023, 179