Nickel-coated glass/epoxy honeycomb sandwich composite for broadband RCS reduction
- Authors
- Kwak, Byeong-Su; Choi, Won-Ho; Noh, Yeong-Hoon; Jeong, Gi-Won; Yook, Jong-Gwan; Kweon, Jin-Hwe; Nam, Young-Woo
- Issue Date
- 15-Jun-2020
- Publisher
- ELSEVIER SCI LTD
- Keywords
- Radar-absorbing structure; Honeycomb sandwich structure; Radar cross-section (RCS); Electroless nickel plating
- Citation
- COMPOSITES PART B-ENGINEERING, v.191
- Indexed
- SCIE
SCOPUS
- Journal Title
- COMPOSITES PART B-ENGINEERING
- Volume
- 191
- URI
- https://scholarworks.bwise.kr/gnu/handle/sw.gnu/6488
- DOI
- 10.1016/j.compositesb.2020.107952
- ISSN
- 1359-8368
- Abstract
- In this paper, a new proposed radar-absorbing honeycomb sandwich composite with nickel-coated glass fabric, implemented via electmless plating, was applied to the leading edge of a NACA 0012 wing airfoil model to reduce the echo radar cross-section (RCS) level. The composite was designed and fabricated without dispersing conductive nanoparticles or metal magnetic micmpowders in polymer materials. The proposed composite exhibited -10 dB microwave absorption in the frequency range of 5.8-16.3 GHz, with a resonance peak of -38.1 dB at 8.2 GHz under TM mode, and an RCS reduction of 10 dB for VV polarization and 8 dB for HH polarization in the frequency range of 6.0-17.8 GHz. When the proposed absorber was applied to the leading edge of NACA 0012, the simulated echo RCS level was reduced by 10 dB from C-band to Ku-band under both horizontal and vertical polarizations. A flatwise compressive test was conducted to evaluate mechanical performance of the composite. The proposed composite can be potentially applied to the radar-absorbing structure of stealth aircrafts.
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Collections - 공학계열 > Division of Mechanical and Aerospace Engineering > Journal Articles

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