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<?xml-stylesheet type="text/xsl" href="https://communities.bentley.com/cfs-file/__key/system/syndication/rss.xsl" media="screen"?><rss version="2.0" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:slash="http://purl.org/rss/1.0/modules/slash/" xmlns:wfw="http://wellformedweb.org/CommentAPI/"><channel><title>Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/products/ram-staad/f/ram-staad-forum/217862/bolt-group-tool-tension-calculation</link><description>In RAM Connection Standalone v13 update 3 (13.03.00.33), how is the Bolt Group tool calculating the tension per bolt? It looks like the program is using case I for eccentricity normal to the plane of the faying surface from part 7 of AISC 360, however</description><dc:language>en-US</dc:language><generator>Telligent Community 12</generator><item><title>RE: Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/thread/667832?ContentTypeID=1</link><pubDate>Mon, 23 Aug 2021 11:56:55 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:b3d16139-1bcc-42ef-8cdb-5d1df069978c</guid><dc:creator>Quinton Sweitzer</dc:creator><description>&lt;p&gt;Thanks for the response. I actually discovered that regardless of how you enter the bolt matrix parameters and direction of the eccentric shear, RAM calculates the neutral axis based on the axis corresponding to the bolt columns.&amp;nbsp;&lt;/p&gt;
&lt;p&gt;I tested this out with a 2 column x 3 row bolt matrix with an out of plane shear force at 0&amp;deg; vs. a 3 column by 2 row bolt matrix with an out of plane shear force at 90&amp;deg;. The results should be identical but were not.&amp;nbsp;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>RE: Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/thread/666691?ContentTypeID=1</link><pubDate>Mon, 16 Aug 2021 14:44:51 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:10fa8a89-f0ac-47a9-898e-4dad0569ed4b</guid><dc:creator>Seth Guthrie</dc:creator><description>&lt;p&gt;&amp;nbsp;For out-of-plane analysis we are following the Eccentricity Normal to the Plane of the Faying Surface procedure. AISC360 15th Edition page 7-10.&lt;/p&gt;
&lt;p&gt;&amp;nbsp;Where we found the equilibrium/neutral axis using a bisection method.&lt;/p&gt;
&lt;p&gt;&amp;nbsp;&lt;img alt=" " src="/resized-image/__size/500x350/__key/communityserver-discussions-components-files/5932/boltdiagram.png" /&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>RE: Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/thread/665356?ContentTypeID=1</link><pubDate>Mon, 09 Aug 2021 16:19:50 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:cdfc5fc9-b3e7-4e2c-8314-eb7471fc0048</guid><dc:creator>Seth Guthrie</dc:creator><description>&lt;p&gt;I&amp;#39;ll double check with the developers, but this is what the Limcon manual indicated and the Ram Connection methods are similar.&amp;nbsp;&lt;/p&gt;
&lt;p&gt;&lt;strong&gt;Out of Plane Bending&lt;/strong&gt;&lt;/p&gt;
&lt;p&gt;Out-of-plane moments on bolt groups are always analyzed using a plastic method in which all tension bolts are assumed to resist the ultimate bolt tension. Using the Ref.&amp;nbsp;6 method with the neutral axis at the bolt group centroid there can be only one non-zero out-of-plane moment. Behavior is not defined for biaxial out-of-plane bending.&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>RE: Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/thread/665332?ContentTypeID=1</link><pubDate>Mon, 09 Aug 2021 14:52:26 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:03b5840a-c42c-4b9b-9df5-057fc2533d2d</guid><dc:creator>Quinton Sweitzer</dc:creator><description>&lt;p&gt;My question is in regard to the tension force calculation. E&lt;span&gt;ccentricity normal to the plane of the faying surface and getting the tension per bolt.&lt;/span&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>RE: Bolt Group Tool Tension Calculation</title><link>https://communities.bentley.com/thread/665331?ContentTypeID=1</link><pubDate>Mon, 09 Aug 2021 14:49:43 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:3e2881b6-d536-4c2a-aabd-df6f6cfb4114</guid><dc:creator>Seth Guthrie</dc:creator><description>&lt;p&gt;If you click on the Analysis Method and show the help you will get some details. Copied below:&amp;nbsp;&lt;/p&gt;
&lt;div class="mainbody"&gt;
&lt;h1&gt;Analysis method&lt;/h1&gt;
&lt;div class="body conbody"&gt;
&lt;p class="shortdesc"&gt;Option that allows to define the analysis method to determine the bolt group capacity when subjected to eccentric loads.&lt;/p&gt;
&lt;div class="section" id="GUID-9181305D-D445-44D8-86FA-1992C383FF8E__GUID-FB23C74E-CEAC-4B98-9A0D-36CA9603F02F"&gt;
&lt;ul class="ul"&gt;
&lt;li class="li"&gt;Elastic Method
&lt;p class="p"&gt;The elastic method uses basic mechanics and superposition to estimate the shear stress in each bolt. The load is considered at the center of gravity of the bolt group and a moment added to account for the eccentricity. The stresses for each case are then determined and vectorially added together.&lt;/p&gt;
&lt;/li&gt;
&lt;li class="li"&gt;Instantaneous Center Method
&lt;p class="p"&gt;The instantaneous center method considers that the translational and rotational events occur simultaneously about an instantaneous center of rotation that is located near a line that is perpendicular to the applied force and passes near the original center of gravity of the bolt group. The method also accounts for the ductility of the bolt group and the potential for load redistribution.&lt;/p&gt;
&lt;/li&gt;
&lt;/ul&gt;
&lt;/div&gt;
&lt;/div&gt;
&lt;/div&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item></channel></rss>