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        <identifier>oai:www.ideals.illinois.edu:2142/21157</identifier>
        <datestamp>2023-07-10</datestamp>
        <setSpec>col_2142_5131</setSpec>
        <setSpec>col_2142_14787</setSpec>
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        <thesis xmlns="http://www.ndltd.org/standards/metadata/etdms/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/" xsi:schemaLocation="http://www.ndltd.org/standards/metadata/etdms/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdms11.xsd http://purl.org/dc/elements/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdmsdc.xsd">
          <dc:contributor>Socie, Darrell F.</dc:contributor>
          <dc:creator>Wang, Jerry Zhiqi</dc:creator>
          <dc:date>2011-05-07T13:00:02Z</dc:date>
          <dc:date>2011-05-07T13:00:02Z</dc:date>
          <dc:date>10000-01-01</dc:date>
          <dc:date>1993</dc:date>
          <dc:description>An experimental study of strength and failure behavior of orthotropic G-10 glass fiber reinforced composite laminates in an in-plane stress state has been conducted. Different types of biaxial specimens and associated test fixtures were developed and employed in the study. Standard IITRI specimens were used to determine tensile and compressive failure strengths of G-10 composite laminates in both fill and warp directions. Biaxial tension-compression (BTC) and biaxial compression-compression (BCC) flat coupon specimens with flexible end reinforcements were designed and tested to study failure behaviors and mechanisms of composite laminates under a biaxial tension-compression and biaxial compression-compression stress states. Tubular specimens loaded in axial tension, axial compression, torsion, internal pressure, and external pressure were employed to produce desired combinations of in-plane stresses and strains. Based on the biaxial failure envelopes obtained from the tests, notched BCC specimens (BCC(n)) were tested in a biaxial compression loading condition to study failure behavior of notched laminates under a biaxial stress state. Failure mechanisms of notched and unnotched composite laminates have been studied based on the test data and failure surface examination.</dc:description>
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  Previous issue date: 1993</dc:description>
          <dc:description>Item marked as restricted to the 'UIUC Users [automated]' Group (id=2) by Howard Ding (hding2@illinois.edu) on 2011-05-07T14:48:52Z
Item is restricted indefinitely.</dc:description>
          <dc:description>Restriction data tranferred 2014-07-01T11:22:10-05:00
Original Data
Group with Access UIUC Users [automated]
Release Date: none
Reason: ETDs are only available to UIUC Users without author permission</dc:description>
          <dc:description>ETDs are only available to UIUC Users without author permission</dc:description>
          <dc:description>U of I Only</dc:description>
          <dc:identifier>AAI9314957</dc:identifier>
          <dc:identifier>(UMI)AAI9314957</dc:identifier>
          <dc:identifier>http://hdl.handle.net/2142/21157</dc:identifier>
          <dc:language>eng</dc:language>
          <dc:rights>Copyright 1993 Wang, Jerry Zhiqi</dc:rights>
          <dc:subject>Applied Mechanics</dc:subject>
          <dc:subject>Engineering, Mechanical</dc:subject>
          <dc:title>Failure strength and mechanism of composite laminates under multiaxial loading conditions</dc:title>
          <dc:type>text</dc:type>
          <degree>
            <department>Mechanical Science and Engineering</department>
            <discipline>Mechanical Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Dissertation</level>
            <name>Ph.D.</name>
          </degree>
        </thesis>
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