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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/"><channel><title>Bashar Seraphim's Activities</title><link>https://communities.bentley.com/members/e577b5cb_2d00_21e6_2d00_472d_2d00_be79_2d00_5b394b3323ce</link><description>Bashar Seraphim's recent activity</description><dc:language>en-US</dc:language><generator>Telligent Community 12</generator><item><title>MSTower</title><link>https://communities.bentley.com/products/ram-staad/f/ram-staad-forum/178183/mstower</link><pubDate>Sun, 14 Apr 2019 21:18:40 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:7fd4335d-efbb-4c44-b6cc-e4a379c3f19e</guid><dc:creator>Charles Ononye</dc:creator><description>&lt;p&gt;I am trying to create RF panel for tower loading. I am finding it quite difficult to do. I can load the Dishes but I can&amp;#39;t find the RF panels in the Ms_anc.lib can any one assist me in getting a comprehensive ancillary library file or teach me how to create one?&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Curve Selection for Effective slenderness factor (K) in Mstower</title><link>https://communities.bentley.com/products/ram-staad/f/ram-staad-forum/242459/curve-selection-for-effective-slenderness-factor-k-in-mstower</link><pubDate>Thu, 06 Apr 2023 15:35:57 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:9cdf97bc-d5df-4b65-ae47-33eda246fe22</guid><dc:creator>Bashar Seraphim</dc:creator><description>&lt;p&gt;Hello&amp;nbsp;&lt;/p&gt;
&lt;p&gt;I&amp;#39;m a bit confused about the way MsTower depends to determine buckling curve to calculate effective slenderness factor (K) according to TIA-222-G table 4-4&amp;nbsp;&amp;nbsp;&lt;/p&gt;
&lt;p&gt;According to Mstower manual P56 &amp;quot;&amp;nbsp;If the number of bolts is not specified MStower will assume that all members are single-bolted except for legs, face bracing, and horizontals that are assumed to have two or more bolts&amp;quot;&lt;/p&gt;
&lt;p&gt;In attached summary file there are X Bracing listed with number of bolts nb=2 bu the selected curve is No.4 which correspond with the case of &amp;quot;both ends are unrestrained&amp;quot;( one bolt )&lt;/p&gt;
&lt;p&gt;May I get clarification about the calculation logic please&lt;/p&gt;
&lt;p&gt;Thanks&lt;/p&gt;
&lt;p&gt;Bashar&amp;nbsp;&lt;/p&gt;
&lt;p&gt;&lt;a href="https://communities.bentley.com/cfs-file/__key/communityserver-discussions-components-files/5932/example_5F00_1.rar"&gt;communities.bentley.com/.../example_5F00_1.rar&lt;/a&gt;&lt;a href="https://communities.bentley.com/cfs-file/__key/communityserver-discussions-components-files/5932/example1.rar"&gt;communities.bentley.com/.../example1.rar&lt;/a&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Mstower XH1 discontinuous bracing</title><link>https://communities.bentley.com/products/ram-staad/f/ram-staad-forum/243167/mstower-xh1-discontinuous-bracing</link><pubDate>Tue, 21 Mar 2023 09:54:14 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:ec455227-d2b7-494a-b1b5-f7de4c6a4e1a</guid><dc:creator>Bashar Seraphim</dc:creator><description>&lt;p&gt;Hello,&lt;/p&gt;
&lt;p&gt;I have modeled a tower with one panel configuration of XH1 and discontinuous X bracing (XDISC)&amp;nbsp;&lt;/p&gt;
&lt;p&gt;Upon reveiwing the detailed report, the results shows cross brace capacity being checked taking the tension in the other member into consideration and based on that the total length L=L1+L2 checked (paragraph below)&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;May I get some explanation why total length checked for the discontinuous braing case ?&amp;nbsp;&lt;/p&gt;
&lt;p&gt;Thanks in advance&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;Members: 1205 1206&lt;br /&gt; Intersecting X brace: 1207 1208 at node: 1204&lt;br /&gt; &lt;span style="color:#0000ff;"&gt;Braces not continuous&lt;/span&gt;&lt;br /&gt; Section: 63X5EA Y fy: 355.0 fu: 480.0 Hot rolled &lt;br /&gt; D B Tf Tw: 63.00 63.00 5.00 5.00&lt;br /&gt; Ag An rx ry rv: 611.65 521.65 19.34 19.34 12.42&lt;br /&gt; No. bolts: 1 BH: 18.00 L &lt;br /&gt; Bolts: 1 M16-8 8.8 Ac: 201.0 fy: 620.0 fv: 496.0 fu: 827.0 No. shear planes: 1&lt;br /&gt; Ply th: 5.00 fyp: 355.00 fup: 480.00 X: 0.00 Y: 0.00 Z: 0.00 Cap: 73.7&lt;br /&gt; &lt;br /&gt; Total member length: 4120.8&lt;br /&gt; Rotational stiffness ratios (restraint/member): &lt;br /&gt; my: 0.0 0.0 0.0&lt;br /&gt; mz: 0.0 0.0 0.0&lt;br /&gt; Case: 3000&lt;br /&gt; Axial force range: 0.1c 0.4c&lt;br /&gt; Memb Curve L L/rx L/ry L/rv KL/r fy&amp;#39; Fcr &amp;iacute;Pnt &amp;iacute;Pnc&lt;br /&gt; 1205 b4 1982 102.5 102.5 159.5 159.5 355.0 68.0 140.8 37.4 &lt;br /&gt; 1206 b4 2139 110.6 110.6 172.2 172.2 355.0 58.4 140.8 32.1 &lt;br /&gt; &lt;span style="color:#ff6600;"&gt;check cross brace capacities:&lt;/span&gt;&lt;br /&gt;&lt;span style="color:#ff6600;"&gt; Pb1 Pb2 Pb L1 L2: 0.11c 0.36c 0.36c 1981.75 2139.03&lt;/span&gt;&lt;br /&gt;&lt;span style="color:#ff6600;"&gt; Px1 Px2 Px : 0.01t 0.26c 0.26c&lt;/span&gt;&lt;br /&gt;&lt;span style="color:#ff6600;"&gt; Tension/compr. in X brace &amp;lt; 0.2, L = L1 + L2 = 4120.8&lt;/span&gt;&lt;br /&gt;&lt;span style="color:#993366;"&gt;&lt;strong&gt; 1205 b4 4121 0.0 213.1 0.0 213.1 355.0 38.1 140.8 21.0 &amp;nbsp;&lt;/strong&gt;&lt;/span&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Ask A Question I</title><link>https://communities.bentley.com/achievements/460ac7df-7ccc-4c42-a204-9e05eef3be09</link><pubDate>Sat, 04 Mar 2023 09:04:30 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:ca6c2438-a541-45f9-bb1b-0caebb42019f</guid><dc:creator /><description>Ask a question in a forum.</description></item></channel></rss>