<?xml version="1.0" encoding="UTF-8" ?>
<?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>DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/products/ram-staad/f/ram-staad-forum/92956/direct-analysis-aisc-360-10</link><description>Hi, 
 Presently i am using Staad Pro V8i (Select series 4) 20.07.09.31, and input given as below for example, 
 DEFINE DIRECT ANALYSIS 
 FLEX 1 ALL 
 FYLD 345000 ALL 
 AXIAL ALL 
 NOTIONAL LOAD FACTOR 0.002 
 END 
 LOAD 201 1.2 DL+ 1.6 LL 
 REPEAT</description><dc:language>en-US</dc:language><generator>Telligent Community 12</generator><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268743?ContentTypeID=1</link><pubDate>Thu, 05 Dec 2013 06:21:49 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:33fb532f-9a45-4d04-8440-24e0c9388307</guid><dc:creator>Sye</dc:creator><description>&lt;p&gt;Unfortunately it is not possible to do that from a single DIRECT ANALYSIS. However you may actually consider carrying out a separate PDELTA 35 ANALYSIS with the serviceability cases for checking the column drifts and then do a DIRECT ANALYSIS for the strength cases. &amp;nbsp;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268600?ContentTypeID=1</link><pubDate>Wed, 04 Dec 2013 10:08:14 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:4ee8df02-baaf-4516-8892-e33c4fa8fb79</guid><dc:creator>MAHESH KUMAR K</dc:creator><description>&lt;p&gt;Exactly, the displacement i have compared are the nodal displacement to check the drift of the structure. Is it possible to get the displacement of the nodes with full EI after analysis to check the serviceability (drift) limits, i believe that the reduced stiffness are to be used for calculating the required strength only as per Cl. C2.3&amp;nbsp;Adjustments to Stiffness (Chapter C AISC 360-10). Please advice.&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268547?ContentTypeID=1</link><pubDate>Tue, 03 Dec 2013 23:33:57 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:7303b347-a255-49cd-befa-2049cd627ae0</guid><dc:creator>Sye</dc:creator><description>&lt;p&gt;Although I could not see the images, but I am guessing that you are looking at the nodal displacements as opposed to section displacements. The REDUCEDEI 0 ensures that displacements at intermediate locations within the member are computed using the full E and I. The section displacements are the ones that are used for checking whether the member satisfies deflection limits ( L/240, L/360 etc ). The displacements at the nodes on the other hand comes from the analysis with reduced E and I. &lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268473?ContentTypeID=1</link><pubDate>Tue, 03 Dec 2013 13:17:37 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:5b8de934-9e65-491d-8f4b-bc63b7aafde8</guid><dc:creator>MAHESH KUMAR K</dc:creator><description>&lt;p&gt;&lt;/p&gt;
&lt;p&gt;I am getting the same displacement by changing the REDUCEDEI also, please refer to the below and advice,&lt;/p&gt;
&lt;p&gt;The displacement results shows that the full EI is used for calculating the deflections? please advice&lt;/p&gt;
&lt;p&gt;The below results with command,&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS LRFD TAUTOL 0.01 DISPtol 0.002 -&lt;br /&gt;ITERDIRECT 10 &lt;strong&gt;REDUCEDEI 0&lt;/strong&gt; PDiter 15&lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="335" width="568" /&gt;&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;The below results with command,&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS LRFD TAUTOL 0.01 DISPtol 0.002 -&lt;br /&gt;ITERDIRECT 10 &lt;strong&gt;REDUCEDEI 1&lt;/strong&gt; PDiter 15&lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="301" width="532" /&gt;&lt;/p&gt;
&lt;p&gt;The below results with command,&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS&lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="337" width="587" /&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268471?ContentTypeID=1</link><pubDate>Tue, 03 Dec 2013 13:03:32 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:c1148d34-9cf5-41bb-9c88-18aff33b1b26</guid><dc:creator>MAHESH KUMAR K</dc:creator><description>&lt;p&gt;While using the REDUCEDEI 1 or 0, there is no change in the &amp;nbsp;deflection values (i.e. getting the same deflection values&amp;nbsp; while running with&amp;nbsp; REDUCEDEI 0 or 1 ), please advice (may i assume that the deflections are calculated with full EI in all the cases and reduced EI is used for arriving the member internal forces {REQUIRED STRENGTHS} alone to account for the stability analysis as outlined in Chapter C AISC 360-10?) .&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;The below results with command&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS LRFD TAUTOL 0.01 DISPtol 0.002 -&lt;br /&gt;ITERDIRECT 10 &lt;strong&gt;REDUCEDEI 1&lt;/strong&gt; PDiter 15&lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="377" width="591" /&gt;&lt;/p&gt;
&lt;p&gt;The below results with command,&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS LRFD TAUTOL 0.01 DISPtol 0.002 -&lt;br /&gt;ITERDIRECT 10 &lt;strong&gt;REDUCEDEI 0&lt;/strong&gt; PDiter 15&lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="369" width="650" /&gt;&lt;/p&gt;
&lt;p&gt;&lt;/p&gt;
&lt;p&gt;The below results with command,&lt;/p&gt;
&lt;p&gt;PERFORM DIRECT ANALYSIS &lt;/p&gt;
&lt;p&gt;&lt;img alt="" height="350" width="583" /&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item><item><title>Re: DIRECT ANALYSIS AISC 360-10</title><link>https://communities.bentley.com/thread/268450?ContentTypeID=1</link><pubDate>Tue, 03 Dec 2013 04:01:31 GMT</pubDate><guid isPermaLink="false">6dad98f5-dbc9-4c4d-a9ba-e9da8dc6aa8e:ebe0394b-ec6a-482f-a4f7-6d695c20f1a0</guid><dc:creator>Sye</dc:creator><description>&lt;p&gt;Yes STAAD does follow the analysis procedure outlined in Appendix 7 of the AISC 360-05 code which has now been moved to Chapter C of 360-10 code. &lt;/p&gt;
&lt;p&gt;I created a wiki item based on your second query and you can find the answer at&lt;/p&gt;
&lt;p&gt;&lt;a rel="nofollow" target="_new" href="http://communities.bentley.com/products/structural/structural_analysis___design/w/structural_analysis_and_design__wiki/10599.aspx#FAQ1"&gt;communities.bentley.com/.../10599.aspx&lt;/a&gt;&lt;/p&gt;&lt;div style="clear:both;"&gt;&lt;/div&gt;</description></item></channel></rss>