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    <responseDate>2026-10-14T14:09:11Z</responseDate>
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    <identifier>10.57760/sciencedb.13253</identifier>
    <datestamp>2024-09-12T09:52:11Z</datestamp>
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  <dc:date>2024-09-12</dc:date>
  <dc:title>Flexural properties of lightweight carbon fiber/epoxy resin composite sandwiches with different fiber directions</dc:title>
  <dc:identifier>doi:10.57760/sciencedb.13253</dc:identifier>
  <dc:language>en</dc:language>
  <dc:description> The unidirectional CFRP laminates were prepared using the carbon fiber prepreg (CF, ZFS Materials Co., Ltd) by hot-pressing method. he lightweight pumice/Mg core was fabricated by pressure-infiltration method. In short, the selected pumice particles with the size of 3&amp;ndash;4 mm were transferred into a cylindrical mould. Then, the molten magnesium was infiltrated into the gaps between pumice particles under vertical pressure. After solidification, the pumice/Mg core was processed to the required size for subsequent experiments.The length, width and thickness of the core material are 60 mm, 15 mm and 10 mm, respectively. The lightweight pumice/Mg core is between two thin CFRP skins, and the core material and CFRP skins are tightly bonded by epoxy adhesive under low pressure. After 24 h of curing, the composite sandwiches for the test were obtained. Three types of composite sandwiches with pumice/Mg core were obtained by using the CFRP skins with different fiber directions.</dc:description>
  <dc:subject>carbon fiber reinforced plastic; sandwiches; flexural properties; failure mode</dc:subject>
  <dc:creator>J A Liu</dc:creator>
  <dc:creator>X Y Zhu</dc:creator>
  <dc:rights>RESTRICTED</dc:rights>
  <dc:type>dataset</dc:type>
  <dc:relation>http://www.doi.org/10.1088/2053-1591/ac4dc5</dc:relation>
  <dc:publisher>Science Data Bank</dc:publisher>
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