When multiple tapered members are designed in group with CHECK CODE ALL command vs. designed individually, the design results do not match. Noted for multiple codes like AISC /IS 800/ S16.

323889

STAAD.Pro is not able to read the external user table files and is generating errors like

*** ERROR : FILE NOT FOUND C:\...\...

**ERROR- IN READING MEMBER PROPERTIES. CHECK DATA FORMAT CAREFULLY.

Provide the full path name to the file. For example instead of specifying

START USER TABLE

TABLE 1 wf1.txt

END

specify the input as shown next

START USER TABLE

TABLE 1 C:\Model_folder\Model_name\wf1.txt

END

STAAD.Pro is crashing during analysis when SELFWEIGHT is applied to a list as shown next

LOAD 1 LOADTYPE Dead 
SELFWEIGHT Y -1 LIST 1 TO 100  

There is an error in plotting of the axial force diagram (FX) for TRUSS members. Wedges are formed at the ends instead of a uniform plot. The values are correctly computed in the analysis.

For tapered member design as per AISC 360-05 code, design results are coming out different when members are designed in groups vs individually

Design the tapered members individually each with its own CHECK CODE command

When the report option Output > Steel Design Detail is used to get detailed design report, the generated report is incomplete for some codes like AISC 360-05 or AISC 360-10

One can get the detailed design report ( TRACK 2 output ) printed in the analysis output file. A concise version of design report can be obtained by including the option Output > Utilization Ratio Table

Some users were not able to access the STAAD News from within the startup page and also not able to connect to the Personal Portal using the Connection Client Widget.

For those users experiencing the problem the following workaround is suggested.

1. Close all Bentley products.

2. Uninstall the existing Connection Client ( from within Control Panel > Programs and Features )

3. Download an Updated Bentley Connection Client from the following page http://communities.bentley.com/products/structural/structural_analysis___design/m/structural_analysis_and_design_gallery/271606

4. Click on the Download button on the right to start downloading. Please note that you have to be logged in with your Bentley Login to be able to download the file.

5. A zip file BentleyCC.zip will be downloaded. Extract the contents of the zip to any folder in your machine and you will find 3 files

   blg6410000319en.exe

   blog10000319en.exe

   ConnectClientClrWrapper.dll

6. If you have a 64 bit OS, right click on the first exe and choose Run as Administrator to install the connection client.

7. Alternately if you have a 32 bit OS, right click on the second exe and choose Run as Administrator to install the connection client.

8. Copy the file ConnectClientClrWrapper.dll to the folder C:\SProV8i SS6\STAAD\ConnectClient. There will be a file by the same name in that folder. Replace it with this one.

9. Log in to Connection Client using your Bentley login credentials.

Design for Tee Sections as per AISC 360-10 for which critical condition  is  H2-1 may   not be correct as software is not considering the correct section modulus for all cases.

In a Pdelta analysis with tension/compression, the pdelta effect is not considered in section force calculations unless each load case is followed by the PDELTA ANALYSIS and CHANGE.

The design of double angles as per IS800:LSD code is incorrect. The cross sectional properties for Y and Z axes got reversed due to which the design is being done incorrectly.

Slenderness calculation and hence compression capacity caclulation for double angle sections as per IS800:2007 is incorrect.

If any primary load case containing self weight is included in a Repeat Load case, the effect of self weight on member section axial forces gets ignored, thereby producing incorrect axial forces at intermediate section locations for the Repeat Load case. The values at the start and end of the member are correct.

438681

Deflection check as per AISC 360, IS 800, S16-14 codes are always reporting last load case in the serviceability envelope as critical load case for deflection. The design is correct and reports the correct critical ratio. It is just the reporting of the critical load case which is incorrect and that too when deflection governs. So for any design where deflection is not the governing criteria, this reporting error does not have any effect.

Double Channel Front to Front cannot be designed as per AISC Unified 360-05 and 360-10 codes. An ERROR: MEMBER DESIGN FAILED FOR MEMBER xx is reported 

The error in noted in version 20.07.11.70. The sections can be designed in earlier versions like 20.07.11.33, 20.07.10.65 etc. This will be addressed in SS6 SP3 release planned for Q2 of 2016.