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    <identifier>10.57760/sciencedb.13359</identifier>
    <datestamp>2024-09-18T21:03:43Z</datestamp>
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  <dc:date>2024-09-18</dc:date>
  <dc:title>Dataset on interlaminar fracture toughness of  mantis shrimp saddles inspired basalt fiber reinforced laminate composites</dc:title>
  <dc:identifier>doi:10.57760/sciencedb.13359</dc:identifier>
  <dc:language>en</dc:language>
  <dc:description>Mechanical test of Mode I and Mode II Interlaminar fracture toughness (IFT)The sample preparation and tests of GIC and GIIC were according to ASTM D5528-13 and HB7403-96. A standard double-cantilever beam (DCB) specimen with a size of 180 mm (length) &amp;times; 25 mm (width) &amp;times; 3.2 mm (thickness) was used to measure GIC. The pre-crack made by PTFE film was 25 mm in length. An end notch flexure (ENF) test specimen with 140 mm (length) &amp;times; 25 mm (width) &amp;times; 3.2 mm (thickness) was used to measure GIIC. The pre-crack made by PVDF film was 25 mm in length.For Mode I test, the sample was clamped on a universal testing machine and was loaded at a rate of 2 mm/min. Critical load (P), displacement of loading point (&amp;delta;) and crack length (a) were recorded during the test. Then the load-displacement curve was plotted. The recorded data was used to calculate GIC. Similarly, for the Mode II test, three-point ENF tests were carried out. The loading rate was 2 mm/min. The load-displacement curve was plotted for further analysis. At least five specimens of each kind of BFRP composites were tested.</dc:description>
  <dc:subject>Composite laminate; Interlaminar toughening; Helical structure; Interlaminar fibril structure.</dc:subject>
  <dc:creator>Binjie Zhang</dc:creator>
  <dc:creator>Shichao Niu</dc:creator>
  <dc:creator>Zhiwu Han</dc:creator>
  <dc:rights>RESTRICTED</dc:rights>
  <dc:type>dataset</dc:type>
  <dc:relation>http://www.doi.org/10.1002/adfm.202311666</dc:relation>
  <dc:publisher>Science Data Bank</dc:publisher>
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