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		<title><![CDATA[Cervenka Consulting Forums — Mesh refinement]]></title>
		<link>https://forums.cervenka.cz/viewtopic.php?id=1693</link>
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		<description><![CDATA[The most recent posts in Mesh refinement.]]></description>
		<lastBuildDate>Tue, 04 Feb 2014 06:55:40 +0000</lastBuildDate>
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			<title><![CDATA[Re: Mesh refinement]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=3073#p3073</link>
			<description><![CDATA[<p>Hello, the material law is evaluated in each integration point - see also ATENA Troubleshooting, 2.1.23 The tensile (or compressive) stresses exceed the tensile (or compressive) strength or yield stress – what is wrong?</p><p>You can not say in general if the convergence with mesh refinement is from above or below - this can differ problem from problem, model from model. </p><p>You are right large elements are more brittle once a crack starts opening. For element sizes larger than the distance between localized cracks (typically, shells), please define crack spacing to prevent unrealistic brittleness.</p>]]></description>
			<author><![CDATA[null@example.com (dpryl)]]></author>
			<pubDate>Tue, 04 Feb 2014 06:55:40 +0000</pubDate>
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			<title><![CDATA[Mesh refinement]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=3072#p3072</link>
			<description><![CDATA[<p>Hi there,</p><p>I have a RC&nbsp; pile cap with a coarse mesh. I was wondering which stress is considered for cracking criteria in FE mesh? is it the stress at element surface or the average for that element?</p><p>Does finer mesh give a higher load capacity and whilst the coarse mesh is conservative? </p><p>I guess the crack will propagate in the whole element (not partially) and with the coarse mesh it will be quicker. Please confirm if that is correct.</p><p>kind regards,<br />Siavash</p>]]></description>
			<author><![CDATA[null@example.com (siavash.hashemi)]]></author>
			<pubDate>Tue, 04 Feb 2014 00:00:50 +0000</pubDate>
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