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DTSTART:20190315T090000Z
DTEND:20190315T100000Z
SUMMARY:DCAMM Seminar - Quantification of Manufacturing Defect Severity in Composites for Failure Assessment
DESCRIPTION:<p style="margin-left: 1cm;"><span>A DCAMM seminar will be presented by</span></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Professor Ramesh Talreja</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Department of Aerospace Engineering</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Department of Materials Science and Engineering</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Texas A&amp;M University, College Station, Texas, USA</span></strong></p>\n&nbsp;\n<p style="margin: 0cm 0cm 0.0001pt 1cm; text-align: justify;"><strong><span>Abstract:</span></strong><span><br />\n<br />\n</span>Composite materials are manufactured by a variety of processes that produce microstructural compositions depending on the process histories. In spite of efforts to achieve perfect microstructures, real manufactured composites contain defects in the forms of nonuniform fiber distributions, fiber misalignment, matrix voids, etc. Such defects affect the composite&rsquo;s performance, such as structural integrity and durability, when exposed to service environments. In many cases, the early failure events are significantly affected by the defects, and inadequate account of these effects leads to inaccurate assessment of damage progression and ultimate failure. Furthermore, evaluating the goodness of the manufacturing process requires that the defects are quantified in terms of their severity with respect to the performance metric. A concept for defect severity quantification will be proposed that generalizes the geometric size characterization and allows incorporation of the parameters governing the particular failure mode under consideration. Two failure&nbsp;<span style="text-align: left;">modes in unidirectional composites will be taken to illustrate implementation of the defect severity measures: a) transverse cracking&nbsp;</span>and b) longitudinal fiber microbuckling.</p>\n<p style="margin: 0cm 0cm 0.0001pt 1cm; text-align: justify;">&nbsp;</p>\n<p style="margin-left: 1cm;"><span>Danish pastry, coffee and tea will be served 15 minutes before the seminar starts.<br />\n<br />\nAll interested persons are invited.<br />\n<br />\n</span></p>
X-ALT-DESC;FMTTYPE=text/html:<p style="margin-left: 1cm;"><span>A DCAMM seminar will be presented by</span></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Professor Ramesh Talreja</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Department of Aerospace Engineering</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Department of Materials Science and Engineering</span></strong></p>\n<p style="margin-bottom: 0.0001pt; text-align: center;"><strong><span>Texas A&amp;M University, College Station, Texas, USA</span></strong></p>\n&nbsp;\n<p style="margin: 0cm 0cm 0.0001pt 1cm; text-align: justify;"><strong><span>Abstract:</span></strong><span><br />\n<br />\n</span>Composite materials are manufactured by a variety of processes that produce microstructural compositions depending on the process histories. In spite of efforts to achieve perfect microstructures, real manufactured composites contain defects in the forms of nonuniform fiber distributions, fiber misalignment, matrix voids, etc. Such defects affect the composite&rsquo;s performance, such as structural integrity and durability, when exposed to service environments. In many cases, the early failure events are significantly affected by the defects, and inadequate account of these effects leads to inaccurate assessment of damage progression and ultimate failure. Furthermore, evaluating the goodness of the manufacturing process requires that the defects are quantified in terms of their severity with respect to the performance metric. A concept for defect severity quantification will be proposed that generalizes the geometric size characterization and allows incorporation of the parameters governing the particular failure mode under consideration. Two failure&nbsp;<span style="text-align: left;">modes in unidirectional composites will be taken to illustrate implementation of the defect severity measures: a) transverse cracking&nbsp;</span>and b) longitudinal fiber microbuckling.</p>\n<p style="margin: 0cm 0cm 0.0001pt 1cm; text-align: justify;">&nbsp;</p>\n<p style="margin-left: 1cm;"><span>Danish pastry, coffee and tea will be served 15 minutes before the seminar starts.<br />\n<br />\nAll interested persons are invited.<br />\n<br />\n</span></p>

URL:http://www.dcamm.dk/da/Kalender/2019/03/Seminar_No_736
DTSTAMP:20260925T215000Z
UID:{2C833220-E480-4006-9A9E-32957364839F}-20190315T090000Z-20190315T090000Z
LOCATION: DTU Wind Energy, Risø Campus, Meeting room 2+3, Building 228, Frederiksborgvej 228, 4000  Roskilde
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