Experimental investigation of sandwich panels with hybrid composite face sheets and embedded shape memory alloy wires under low velocity impact
This experimental study was conducted to investigate the behavior of hybrid composite sandwich panels with superelastic shape memory alloy (SMA) wires under low velocity impact (LVI). Square‐shaped sandwich panels were made few of a foam core and hybrid composite structures with carbon fiber and gla...
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Published in | Polymer composites Vol. 41; no. 11; pp. 4811 - 4829 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Hoboken, USA
John Wiley & Sons, Inc
01.11.2020
Blackwell Publishing Ltd |
Subjects | |
Online Access | Get full text |
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Abstract | This experimental study was conducted to investigate the behavior of hybrid composite sandwich panels with superelastic shape memory alloy (SMA) wires under low velocity impact (LVI). Square‐shaped sandwich panels were made few of a foam core and hybrid composite structures with carbon fiber and glass fiber, in which prestrained superelastic SMA wires were embedded between the layers. The sandwich panels had symmetrical and asymmetrical lay‐ups and SMA wires were placed between the layers with different states. LVI tests were performed by drop weight impact testing machine. Moreover, damaged areas of the panels were estimated using thermography. The experimental results showed that the impact performance of the panels improved after embedding SMA wires. The presence of the SMA within the composite sandwich structure prevented the full perforation of the samples and reduced the internal delamination area. The utilization of SMA wires embedded in front face sheet, which is subject to the direct impact, is more effective than the utilization of wire in the back face layer. It was also found that increasing the layers of the back face and asymmetrication of the structure were more effective than the use of SMA wires in the symmetric structure in improving the panel impact resistance. |
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AbstractList | This experimental study was conducted to investigate the behavior of hybrid composite sandwich panels with superelastic shape memory alloy (SMA) wires under low velocity impact (LVI). Square‐shaped sandwich panels were made few of a foam core and hybrid composite structures with carbon fiber and glass fiber, in which prestrained superelastic SMA wires were embedded between the layers. The sandwich panels had symmetrical and asymmetrical lay‐ups and SMA wires were placed between the layers with different states. LVI tests were performed by drop weight impact testing machine. Moreover, damaged areas of the panels were estimated using thermography. The experimental results showed that the impact performance of the panels improved after embedding SMA wires. The presence of the SMA within the composite sandwich structure prevented the full perforation of the samples and reduced the internal delamination area. The utilization of SMA wires embedded in front face sheet, which is subject to the direct impact, is more effective than the utilization of wire in the back face layer. It was also found that increasing the layers of the back face and asymmetrication of the structure were more effective than the use of SMA wires in the symmetric structure in improving the panel impact resistance. |
Author | Jabbari, Mohsen Masoudi Moghaddam, Seyed A. Khorshidvand, Ahmad R. Yarmohammad Tooski, Mehdi |
Author_xml | – sequence: 1 givenname: Seyed A. surname: Masoudi Moghaddam fullname: Masoudi Moghaddam, Seyed A. organization: Islamic Azad University – sequence: 2 givenname: Mehdi orcidid: 0000-0001-9712-5472 surname: Yarmohammad Tooski fullname: Yarmohammad Tooski, Mehdi email: m_yarmohammad@azad.ac.ir organization: Islamic Azad University – sequence: 3 givenname: Mohsen surname: Jabbari fullname: Jabbari, Mohsen organization: Islamic Azad University – sequence: 4 givenname: Ahmad R. surname: Khorshidvand fullname: Khorshidvand, Ahmad R. organization: Islamic Azad University |
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CitedBy_id | crossref_primary_10_1016_j_rineng_2024_103815 crossref_primary_10_1002_pc_26219 crossref_primary_10_1002_pc_29013 crossref_primary_10_1002_pc_26063 crossref_primary_10_1007_s40830_021_00355_w crossref_primary_10_1080_15376494_2021_2023921 crossref_primary_10_1002_pc_27269 crossref_primary_10_1016_j_jcomc_2025_100557 crossref_primary_10_1002_pc_27311 crossref_primary_10_1016_j_ijsolstr_2025_113223 crossref_primary_10_1515_epoly_2024_0100 |
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Snippet | This experimental study was conducted to investigate the behavior of hybrid composite sandwich panels with superelastic shape memory alloy (SMA) wires under... |
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StartPage | 4811 |
SubjectTerms | active infrared thermography Asymmetry Carbon fibers composite sandwich panel Composite structures damaged area Drop tests Embedding Glass fibers Hybrid composites Impact damage Impact resistance Impact testing machines low velocity impact Sandwich panels Sandwich structures Shape memory alloys superelastic SMA wire Superelasticity Thermography |
Title | Experimental investigation of sandwich panels with hybrid composite face sheets and embedded shape memory alloy wires under low velocity impact |
URI | https://onlinelibrary.wiley.com/doi/abs/10.1002%2Fpc.25754 https://www.proquest.com/docview/2460969973 |
Volume | 41 |
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