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Cited 15 time in webofscience Cited 17 time in scopus
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Advanced acoustic design: 3D printed thermoplastic folded core sandwich structures with porous materials and microperforations for enhanced sound absorption

Authors
Mallesh, ShanigaramHwang, JunhyeokChoi, HuncheolHong, Dong-JunSeok, ChangminKwak, ByeongsuLee, Soo-YongNam, Youngwoo
Issue Date
Oct-2024
Publisher
Elsevier BV
Keywords
3D printing; Microperforated panel; Sound absorption coefficient; Sound absorption materials; Thermoplastic folded core sandwich composite
Citation
Composite Structures, v.345
Indexed
SCIE
SCOPUS
Journal Title
Composite Structures
Volume
345
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/71205
DOI
10.1016/j.compstruct.2024.118371
ISSN
0263-8223
1879-1085
Abstract
This study introduces a novel sound-absorbing sandwich structure with a folded core, created through 3D printing technology, to address the challenge of weak sound absorption in the low-frequency range in sound absorption materials (SAMs). The structure comprises chopped carbon fiber–dispersed thermoplastic polyamide (CF-PA), continuous carbon fiber (CCF) filaments, and polyurethane (PU) foam coated with graphene oxide (GO). Simulation studies revealed that optimized structural parameters and microperforation diameters resulted in enhanced sound absorption coefficient (SAC) of 99 % or more at 1250 Hz, within the low-frequency range (160–1600 Hz). The GO-coated PU foam SAMs demonstrated excellent sound absorption performance measured in the high-frequency range (1600–6000 Hz), achieving 99 % SAC at 2400 Hz. Furthermore, the manufactured folded core structure exhibited outstanding sound absorption performance, achieving SAC of 99 % at 732 Hz measured in the low-frequency (160–1600 Hz) band and 99 % at 600 Hz, showcasing broad absorption capabilities measured in the high-frequency band (160–6000 Hz). Additionally, a flatwise compression test on the structure filled with GO-coated PU foam demonstrated a 32 % improvement in compressive load, indicating the structure's versatility for various applications. © 2024 Elsevier Ltd
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Kwak, Byeong Su
대학원 (기계항공우주공학부)
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