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		<title><![CDATA[Cervenka Consulting Forums — Beam Lap-Splice Analysis]]></title>
		<link>https://forums.cervenka.cz/viewtopic.php?id=2178</link>
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		<description><![CDATA[The most recent posts in Beam Lap-Splice Analysis.]]></description>
		<lastBuildDate>Fri, 20 Mar 2020 18:11:56 +0000</lastBuildDate>
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			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4562#p4562</link>
			<description><![CDATA[<p>I understand you plan to follow MC2010 section 7.11 Verification assisted by numerical simulations, but have you already discussed the safety formats with your supervisor? </p><p>Ad 1.: Maybe you can find some publications with similar experiments, and verify / calibrate your model (modelling approach) using that? </p><p>I still do not get how you plan to compare with the design formula? The problem with partial safety factors is the failure mode can frequently be different than the real. </p><p>Regards.</p>]]></description>
			<author><![CDATA[null@example.com (dpryl)]]></author>
			<pubDate>Fri, 20 Mar 2020 18:11:56 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4562#p4562</guid>
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			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4561#p4561</link>
			<description><![CDATA[<p>Thank you for the articles </p><p>Title of my study is &quot;Numerical study of Tension Reinforcement Lap Length calculated by Model Code Using a Four-Point Beam Loading System&quot;</p><p>1) In my current study i don&#039;t have any experimental campaign. To validate my model i am trying to compare the failure load given by software with theoretical failure load calculated based on sectional analysis. </p><p>Once model gives results almost accurate with theoretical in terms of failure load, I will carry out further study which is actually variation of splice length. </p><p>Regards</p>]]></description>
			<author><![CDATA[null@example.com (ali)]]></author>
			<pubDate>Fri, 20 Mar 2020 16:19:19 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4561#p4561</guid>
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			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4560#p4560</link>
			<description><![CDATA[<p>If you explain us your plans, we may be able to help you find a way... </p><p>What kind of theoretical prediction do you wish to compare to?</p><p>What are the questions to be answered by your analysis (see also ATENA Troubleshooting, 2.1.1)? </p><p>I recommend the following articles on the safety formats topic: </p><p><a href="https://www.cervenka.cz/assets/files/papers/11th_IPW_Cervenka.pdf">https://www.cervenka.cz/assets/files/pa … rvenka.pdf</a></p><p><a href="https://www.researchgate.net/publication/324389439_Evaluation_of_Safety_Formats_for_Structural_Assessment_Based_on_Nonlinear_Analysis">https://www.researchgate.net/publicatio … r_Analysis</a></p><p>Regards.</p>]]></description>
			<author><![CDATA[null@example.com (dpryl)]]></author>
			<pubDate>Fri, 20 Mar 2020 16:02:14 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4560#p4560</guid>
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		<item>
			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4559#p4559</link>
			<description><![CDATA[<p>Thanks</p><p>I am using design option in ATENA, direct comparison with theoretical predictions could not be possible ?</p>]]></description>
			<author><![CDATA[null@example.com (ali)]]></author>
			<pubDate>Fri, 20 Mar 2020 15:31:20 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4559#p4559</guid>
		</item>
		<item>
			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4558#p4558</link>
			<description><![CDATA[<p>Dear Ali,<br />1. please make clear how you plan to compare the calculate results with design formulas? <br />The most typical approaches with nonlinear FEM is working with mean properties and directly comparing to average measurements, or applying a global safety factor to prove safety. </p><p>2. Trying to constrain a nonexistant degree of freedom is a problem - please correct.</p><p>3. You may need a bond law for your model. The statement that you usually do not need it for ribbed reinforcement and fine meshes (Troubleshooting, 2.2.11) is mainly valid for 3D models - one can simply say in 2D, one dimension of your elements is the thickness, and this is usually much larger than the bar diameter. </p><p>Regards.</p>]]></description>
			<author><![CDATA[null@example.com (dpryl)]]></author>
			<pubDate>Fri, 20 Mar 2020 15:17:34 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4558#p4558</guid>
		</item>
		<item>
			<title><![CDATA[Re: Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4557#p4557</link>
			<description><![CDATA[<p>Recently hasnat1947 was working on a very similar problem. You can find his posts on this forum.</p>]]></description>
			<author><![CDATA[null@example.com (pavlo)]]></author>
			<pubDate>Fri, 20 Mar 2020 14:22:05 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4557#p4557</guid>
		</item>
		<item>
			<title><![CDATA[Beam Lap-Splice Analysis]]></title>
			<link>https://forums.cervenka.cz/viewtopic.php?pid=4556#p4556</link>
			<description><![CDATA[<p>Dear All</p><p>I am analyzing my beam under four pint bending. I failed to reach my desired results. I tried to figure out where i am doing something wrong but couldn&#039;t achieve. </p><p>Theoretical Failure Load = 54.9 KN</p><p>I need to validate my model in term of theoretical failure load.</p><p>I am attaching my model in below link</p><p><a href="https://drive.google.com/open?id=1rPUjWKyAXujtPqhvz1lUnPf9t5335VFS">https://drive.google.com/open?id=1rPUjW … f9t5335VFS</a></p><p>Regards</p>]]></description>
			<author><![CDATA[null@example.com (ali)]]></author>
			<pubDate>Fri, 20 Mar 2020 14:10:22 +0000</pubDate>
			<guid>https://forums.cervenka.cz/viewtopic.php?pid=4556#p4556</guid>
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