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Known Issues in STAAD.Pro CONNECT Edition

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:30:43 AM

This page contains a list of Known Issues found in the STAAD.Pro CONNECT Edition. Note that these include issues that have been addressed in the current release of STAAD.Pro, but provided here as information.

For known issues that relate to earlier V8i versions of STAAD.Pro see V8i Known Issues

Installation and Licensing

[[User ID Missing from the Output Report]]

[[The .std files are not showing up with the STAAD.Pro CE icon]]

General

[[Error Unhandled Exception when trying to open the editor in STAAD.Pro Connect Edition]]

[[Existing custom steel section databases cannot opened in the STAAD.Pro Connect Edition]]

Exception message reported when starting STAAD.Pro CE

[[Software crashes observed in STAAD.Pro CONNECT Edition 22.02.00.26]]

Graphical User Interface 

[[Black Force Diagrams, Fonts or Color Changes]]

[[Run Analysis option is greyed out]]

[[Error when trying to create analytical model from the physical model]]

[[When trying to import an ISM repository into STAAD.Pro, the Run option is grayed out]]

A "Failed to save document" error reported while creating a new model

[[The Parametric Models Fails to Generate Mesh]]

[[Crash when defining beam offsets]]

[[Members/Surfaces cannot be copied unless corresponding nodes are selected]]

[[Error in reading user table General type sections with profile points]]

Modeling

[[The Latitude parameter(IBC 2012) is being incorrectly set to zero]]

[[New material with custom properties cannot be added in the STAAD.Pro Physical Modeler]]

Analysis and Design

[[Unity ratio displayed for only one member when designed as per AISC 360-16]]

[[Error in LTB Check as per Canadian S16-14 Code]]

[[Incorrect Bending Capacity reported for Single Angles designed as per Canadian Steel Design Code CSA S16-09 or CSA S16-14]]

[[STAAD.Pro is considering incorrect Cw values in some situations leading to incorrect LTB capacity calculations when designing per AISC 360-16]]

[[Elastic section modulus is incorrectly calculated for I section with cover plates for design as per AISC ASD (9th Edition)]]

See Also

STAAD.Pro Support Solutions

Tags: CONNECT Edition, STAAD.Pro, STAAD.Pro CONNECT Edition, index, Known Issues

STAAD.Pro Developing The Model [FAQ]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:37 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: Developing the Model
 Subarea: FAQ's
 Original Author:Bentley Technical Support Group
  
  1. Is it possible to quickly find out the total number of nodes & beams in a model ?
  2. How do I stop the Auto Save screen from appearing over and over again in Staad.Pro?
  3. How can I define a built up section whose cross section shape is not that of any standard rolled section?
  4. Construction Grid Aligned to 3 Pre-defined Nodes
  5. Change Units After Entering Loading Functions
  6. Foundation Support Requires Giving the Subgrade Modulus and Supply a Direction
  7. View Selected Objects Only
  8. No Closed Polygon Found to Fill in with Plates
  9. Viewing Individual Floors
  10. Accessing STAAD.Pro Online Help
  11. Converting Single Line Input to Multiline
  12. [[Avoiding Stress Concentrations]]
  13. User Defined Grid System
  14. Applied Selfweight is More Than Total Weight of All Structural Elements 
  15. Braces Carry Lateral Loads Only
  16. Limitation on Number of Plates
  17. Assigning Offsets to Plate Elements
  18. Splitting Continuous Beams
  19. W Shape Table what does Ct Stand For
  20. Duplicated Nodes Warning
  21. Is a Plate Diaphragm - Flexible Diaphragm or Rigid Diaphragm
  22. Make Tool Tips Visible
  23. Load Transfer Result is Unexpected
  24. Change Model Units in an Existing Model
  25. How to account for joists in stiffness analysis in STAAD.Pro ?
  26. [[PRESTRESS vs POSTSTRESS member load in STAAD.Pro]]
  27. [[Importing grids (as dxf files) into the STAAD.Pro Physical Modeler]]
  28. [[Member releases in an excel sheet]]

 

See Also

Product TechNotes and FAQs

Structural Product TechNotes And FAQs

External Link

Bentley Technical Support KnowledgeBase

Bentley LEARN Server

Comments or Corrections?

Bentley's Technical Support Group requests that you please confine any comments you have on this Wiki entry to this "Comments or Corrections?" section. THANK YOU!

Tags: FAQs, SELECTservices, STAAD.Pro, Auto Save screen, Built Up, merge models, Modeling, sheet piles

STAAD.Pro Miscellaneous [FAQ]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:37 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: Miscellaneous Topics
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  
  1. Why does the program give some strange numbers when the joints are generated graphically by e.g. copying. We enter a number that has no decimals (7.00m) and in the input file the coordinate is 7.0001.
  2. When I use the Node Dimensioning Tool (Tools | Display Node to Node Dimension), how can I turn off just one dimension line rather than all of them with the Remove Node Dimension option?
  3. I am trying to model a beam connecting to the flange of a column instead of at the center. How is this modeled?
  4. How to model Pile cap attached to batter and vertical piles in STAAD.Pro?
  5. In the new 3D rendered window, how can I view the structure in plan, elevation and isometric view like I can with the other windows? Also, how do I pan across the model?
  6. When I save a file from the STAAD.Pro GUI, the joint coordinate data and member incidence data are written into the .std file in such a manner that there are several entries per line, separated by semi-colons. I would like it to be written in a way that the joint coordinate data is written as one joint per line and the member incidence data is written as one member per line. Is there some setting in the program to facilitate this?
  7. Can you please tell me how to transfer data from EXCEL to STAAD-PRO?
  8. How do I graphically display the distance between two nodes?
  9. I have a rather large frame building consisting of several floors. I want to look at individual floors by themselves without the rest of the structure cluttering up the view. Can you tell me how to do that?
  10. How do I access online help in STAAD.Pro? The F1 key does not bring up any help screens.
  11. How can I convert single line input to multiple line input? The program currently converts my joint coordinate and member incidence data from multiple line to single line input.
  12. Plate Error - Badly Shaped, Warped, Not Convex, or Not Numbered Counter-Clockwise
  13. STAAD.Pro fails to run the analysis

See Also

Product TechNotes and FAQs

Structural Product TechNotes And FAQs

External Link

Bentley Technical Support KnowledgeBase

Bentley LEARN Server

Comments or Corrections?

Bentley's Technical Support Group requests that you please confine any comments you have on this Wiki entry to this "Comments or Corrections?" section. THANK YOU!

 

   

Tags: FAQs, SELECTservices, STAAD.Pro Error Report, STAAD.Pro, Error Report

STAAD.Pro Postprocessing Solutions

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:37 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: Postprocessing Solutions
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

This page contains items related to the Postprocessing in STAAD.Pro

  1. Changing / inserting the name to be printed in STAAD.Pro report / output
  2. Max Absolute stress in Plate Contour
  3. Print Section forces in STAAD Output
  4. Results Along Line
  5. Stability Checks for a mat foundation modeled in STAAD.Pro
  6. Including pictures in STAAD.Pro Reports
  7. Plotting Bending Moment Diagram on a selected set of members
  8. [[Finding out Forces/Moments for reinforcement design of slabs modeled using solid elements]]
  9. [[Finding out the max forces/displacements/support reactions/stresses for a group of entities]]
Tags: Postprocessing, absolute stress, Results Along Line, section force output, report name, FAQ's

STAAD.Pro Crashing for DELL laptop when Browsing a File Location

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:37 AM

Applies To
Product(s):STAAD.Pro
Version(s):CONNECT Edition (21.xx.xx.XXX) and upper
Environment: ALL
Area: STAAD.Pro Installation Solutions
Subarea: Installation/ Crash
Original Author:Abhisek Mandal, Bentley Technical Support Group

Problem Description:

STAAD.Pro crashes whenever the user clicks on the browse button in the opening page the program. Sometimes users just try to create new file and program crashes. The user is using DELL laptop.

Solution:

This is a known issue due to 'Dells Backup & Recovery' software. It is advised to uninstall the said software as a solution. Please find below some of the supportive links.

https://stackoverflow.com/questions/30833889/dll-hell-with-sqlite?noredirect=1

https://community.easymorph.com/t/easymorph-crash/156

Uninstalling the same will solve the issue.

Tags: crash at startup, STAAD.Pro CONNECT Edition, crash when opening model, browse, Dell, known issue

STAAD.Pro Miscellaneous Solutions

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:48 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Miscellaneous Solutions
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

This page contains items related to miscellaneous topics about STAAD.Pro 

  1. Section Wizard Tutorial
  2. [[Turning off Labels]]
  3. [[STAAD.Pro crashes during startup]]
  4. [[STAAD.Pro crashes during opening]]
  5. STAAD.Pro CONNECT Edition has stopped working
  6. [[STAAD.Pro crashes when opening a model in a user machine]]
  7. [[I do not see the AISC 360-16 code listed in the list of design codes in the STAAD.Pro Connect Edition]]
  8. [[Auto save is not working]]
  9. [[Output items do not appear within Results Setup in STAAD.Pro]]
  10. [[Chord Branch type connections between HSS members]]
  11. [[Creating a Custom Connection in the RAM Connection interface within STAAD.Pro ( CONNECT Edition )]]
  12. [[iTwin Design Review in STAAD.Pro CE Update 5]]
Tags: section wizard, Miscellaneous

STAAD.Pro Driver Downloads [FAQ]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:50 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: Driver Downloads
 Subarea: FAQ's
 Original Author:Sye Chakraborty
Bentley Technical Support Group
  

Index

  1. I get a message "Security Drivers are Old"
  2. My hardware lock is connected to my machine. I still get a message that no hardware lock is found
  3. CDaoException - Failed to open database/ **ERROR- IN READING MEMBER PROPERTIES.CHECK DATA FORMAT CAREFULLY

See Also

Product TechNotes and FAQs

Structural Product TechNotes And FAQs

STAAD.Pro Tutorials

External Link

Bentley Technical Support KnowledgeBase

Bentley LEARN Server

Comments or Corrections?

Bentley's Technical Support Group requests that you please confine any comments you have on this Wiki entry to this "Comments or Corrections?" section. THANK YOU!

 

 

Tags: FAQs, Jetdatabase, STAAD.Pro, Security Drivers, CDAOJetdatabase, License, HASP

Procedure for Downloading STAAD.Pro CE

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:56 AM

Applies To
Product(s):STAAD.Pro
Version(s):CONNECT Edition (22.00.XX.XX)
Environment: ALL
Area: STAAD.Pro Installation/Licensing Solutions
Subarea: Installation
Original Author:Abhisek Mandal, Bentley Technical Support Group

Problem Description:

How do I download latest version of STAAD.Pro?

Steps to follow: 

1. Open a browser in your system with internet connection.

2. Go to https://connect.bentley.com/

3. Log in in the page with your credentials.

4. (Optional) If it requires any other permission, please provide.

5. Now, go to the bottom of the page and you will find Software Download option as shown below.

 

6. Click on Software Download option and it will open software download page as shown below.

7. Now, type the product name in “Search by product name” box. You will find some softwares in the page. If you get the software you were looking for then click on "GET SOFTWARE" option below that software. Else, you can search the software using search box as marked above. If you know the product line and brands then you can search for them directly from the dropdown as shown below.

 

8. Now clicking on the get software option will show you the below page. Set the required filled from the dropdown and click on apply. Then click the  download button as shown below.

9. Keep this installer in a folder as per your requirement.

10. You can use this installer to install the software. To install the software, right click on the installer and choose the Run As Administrator option. If you want to know more about the installation process, double click on the installer and click on the question mark (Help) at the right top corner of the installer window.

Tags: software download, STAAD.Pro CONNECT Edition, downloading staad.pro

Known Issues in STAAD.Pro V8i

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:59 AM
Product(s):STAAD.Pro V8i
Version(s):ALL
Environment: ALL
Area: All

Known Issues in STAAD.Pro SS5

Known Issues in STAAD.Pro SS6 

It may be worth noting that all issues that are known at the time of release are documented as part of the Known Issues section within the Readme file that is provided as part of the installation and can be accessed through Start > All Programs > Bentley Engineering > STAAD.Pro V8i ... > Read Me as shown next

This would open a HTML page. One can click on Known Issues under Local Information on the left side of the page to get a list of known issues.

   

Tags: STAAD.Pro, known defects, Defects, index, known issue

STAAD.Pro OpenSTAAD [FAQ]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:59 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: OpenSTAAD
 Subarea: 

FAQ's

 Original Author:Bentley Technical Support Group
  

Notice: This content is currently under editorial review. There may be several out-dated items currently posted here. Please be patient as this page is made current.

  1. OpenSTAAD Macro for Calculating K Factors
  2. Using OpenSTAAD to Create a Model Outside STAAD
  3. Using OpenSTAAD to Extract Moving Load Data
  4. Support of VBA Functions in OpenSTAAD
  5. OpenSTAAD Beta Releases
  6. OpenSTAAD Database Compatibility
  7. Force and Moment Envelopes in OpenSTAAD

 

See Also

Product TechNotes and FAQs

Structural Product TechNotes And FAQs

External Links

Bentley Technical Support KnowledgeBase

Bentley LEARN Server

Comments or Corrections?

Bentley's Technical Support Group requests that you please confine any comments you have on this Wiki entry to this "Comments or Corrections?" section. THANK YOU!

 

Tags: SELECTservices, FAQ, OpenSTAAD, STAADPro, STAAD

STAAD.Pro Import Export Solutions

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:59 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: Import Export Solutions
 Subarea: Import/Export
 Original Author:Bentley Technical Support Group
  
  1. In Memory Member Splitting and Node Merging
  2. Export a Solid Slab or Wall
  3. Structural Modeler To Staad Export Does Not Work
  4. Code/Country Code Mapping
  5. Design Parameters
  6. Import Model in STAAD
  7. Beams from STAAD to Tekla at Top of Steel
  8. STAAD.Pro Import File Format
  9. ISM-No STAAD filename provided error
  10. STAAD.Pro ISM Import Error from Network Drive
  11. STAAD.Pro CONNECT Edition - Ram Concept
  12. [[Importing AutoPIPE files into STAAD.Pro Connect Edition through Pipelink]]
Tags: Import/Export, import, STAAD.Pro, Export, Power Structural Modeler, Structural Modeler, mvba

STAAD.Pro Design Solutions

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:36:59 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Design Solutions
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

This page contains Design related wikis for STAAD.Pro

  1. IS 456 Documents
  2. STAAD.Pro Aluminum Design FAQ's
  3. STAAD.Pro Concrete Design FAQ's
  4. STAAD.Pro General Design Solutions
  5. STAAD.Pro Steel Design FAQ's
  6. STAAD.Pro Timber Design FAQ's
Tags: General Design, Aluminum, Steel, concrete, IS 456, timber

STAAD.Pro TechNotes [TN]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:37:01 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Tech Notes
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

This page contains a list of TechNotes related to STAAD.Pro

  1. Member Tension And Combination Load Cases [TN]
  2. Pushover Analysis of Steel Structure using STAAD (TN)
  3. Reference Loads An Introduction [CS]
  4. STAAD.Pro Wall Analysis For Dams [TN]
  5. STAAD.Pro EN 1993-1-1:2005 Implementation: Elastic Verification of Cross Sectional Resistance
  6. STAAD.Pro EN 1993-1-1:2005 implementation: Calculation of Torsional Capacities of Cross Sections as per SCI P057
  7. STAAD.Pro EN 1993-1-1:2005 Implementation: Code Check for Torsion
  8. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 2 verification as per SCI P364
  9. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 3 verification as per SCI P364
  10. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 4 verification as per SCI P364
  11. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 9 verification as per SCI P364
  12. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 10 verification as per SCI P364
  13. STAAD.Pro EN 1993-1-1:2005 Implementation: Example 11 verification as per SCI P364
  14. Discussion on Seismic Detailing Concept of RC Structures (IS:13920-1993)
  15. Limitations of the curved beams in STAAD.Pro ( TN )
  16. “Missing Mass” in Dynamic Analysis
  17. IS:1893 (Part-I)-2002 Response Spectrum Philosophy
  18. Linear static, P-Delta, small P-Delta, stress stiffening, and geometric non-linearity in STAAD.Pro
  19. Direct Analysis per AISC 360-05 and its Implementation In STAAD (TN)
  20. Computation of Center of Rigidity
  21. Using RAM Connection in STAAD.Pro

Tags: STAAD.Pro, TechNote

STAAD.Pro Modeling Solutions

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:37:04 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Modeling Solutions
 Subarea: Modeling
 Original Author:Bentley Technical Support Group
  

This page contains FAQs related to Modeling in STAAD.Pro.

Please use the tree structure on the left to browse to the individual FAQs ( wikis ).

  1. Section Properties not Entered for Member
  2. Analyzing Multiple Disjointed Structures
  3. Applying Line Loads on Plates
  4. Modeling a Retaining Wall
  5. Beam and Plate Orientation
  6. Compression Force in Tension Members
  7. Connectivity Issues
  8. Create Section by Specifying Profile Points
  9. Defining Temperature Load
  10. Fixed and Enforced Support
  11. Difference Between Plate, Shell, and Surface Elements
  12. Distributing Wheel Loads
  13. Total Joint/Element Limits Exceeded
  14. Steel Section Encased in Concrete or with Concrete Core
  15. Center of Gravity
  16. Model Solid Rods
  17. Modify Section Database
  18. New Section Database
  19. Convert "SET Z UP" to "SET Y UP"
  20. Define Cable Section
  21. Total Weight of Plates
  22. Modeling Corrugated Steel Plates
  23. Scale Down Supports
  24. Specify Values of Stiffness for Compression and Tension at a Support
  25. Edit Load Rules for Auto Load Combination Generation
  26. Joint Coordinates Modified when Model Moved
  27. Load Path Consideration
  28. Modeling & Designing Gusset Connection
  29. Model Shear Walls Using Plates
  30. Model Slab on Top of Beams
  31. Multiple Support Conditions in Same Model
  32. Cannot Copy a Member, Node or do Transitional Repeat
  33. Specify Seismic Weights Through Reference Load Cases
  34. Aspects to Consider Analyzing Mat Foundations
  35. Create Material Macro
  36. How to convert a LOAD COMBINATION to a REPEAT LOAD
  37. [[ERROR***MATERIAL GROUP AND EXPLICIT CONSTANT SPECIFICATION CANNOT BE USED TOGETHER]]
  38. [[Modeling base plate with anchors in STAAD.Pro]]
  39. [[How to measure node to node distance and dimension beams in STAAD.Pro Connect Edition ?]]
  40. [[Customizing the Interface in STAAD.Pro Connect Edition]]

  41. [[Identifying face numbers for Solid Elements]]
  42. [[Different member release for different load cases]]
  43. [[How to use loads of the same loading type in mutually exclusive combinations when using automatic load combination]]

  44. [[Loads are not displayed in the STAAD.Pro graphical user interface]]

Tags: connectivity, Temperature, orientation, Line Loads, transitional repeat, corrugated, rods, model moved, STAAD.Pro, Reference Load Cases, Surface, cable, Total Weight, Mat Foundations, Enforced, Gusset Connection, element limits, multiple support conditions, retaining wall, Modeling, Set Z Up, section database, center of gravity, Create Material, temperature load, wheel, SET Y UP, scale down supports, shell, Fixed, Disjointed, plate, joint limits, core, Section Properties, compression, Encased, load path, Shear Wall

STAAD.Pro Import/Export [FAQ]

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 11:37:06 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):ALL
 Environment: N/A
 Area: Import/Export
Subarea: FAQ's
 Original Author:Sye Chakraborty, Bentley Technical Support Group
  

How can I get my RISA model into STAAD.Pro ?

I do not see the option import/export using StrucLink module.

How to Open a QSE File?

How can I get data transferred between STAAD.Pro and Autopipe ?

How to import a section from the Section Wizard into STAAD.Pro?

Why my DXF drawing is not imported correctly from AutoCAD into STAAD.Pro?

Tags: Import/Export, import, StrucLink, DXF, FAQ, STAAD.Pro, Export, GTSTRUDL, DWG, SELECTsupport

TRUSS Members

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Revision 1 posted to RAM | STAAD | OpenTower Wiki by Carlos Aguera on 12/21/2020 12:04:29 PM
 Product:STAAD.Pro
First Affected Version:22.05.00.131
 Found in Version:22.05.00.131
Fixed and Released in Version:N/A
 Area: Analysis
 Issue #:A-492168

Problem Description

The results of members defined with a TRUSS specification is not correctly accounting for the effects of transverse loads when applied as member loads.

Background

In order to prevent a member from transferring any moment across the start or end of a member, it is possible to specify releases using a MEMBER RELEASE command in each of the three local axes. However, STAAD.Pro additionally includes a quick method for defining a member as having releases at both ends simultaneously, by assigning a TRUSS specification.

In the update 5 release of STAAD.Pro CE version, a modification was introduced to assist with the use of self-weight on members with a TRUSS specification as this loading equates to a UDL on the member. This modification however did not fully account for the axial forces that may be present in such members.

Solution

The current recommendation is not use TRUSS member specification on members that have transverse loads and are intended to carry axial forces alone. Instead it is strongly advised to use MEMBER REEASE commands in order to account for the releases in the 3 rotational degrees of freedom at the start and ends of such members.

RAM Structural System Tilt-Up Workflow

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Allen Adams on 12/22/2020 3:17:31 PM

Overview

Tilt-up walls are thin concrete panels.  When a slender wall is subjected to axial compression and out-of-plane bending, second order effects must be considered.  ACI 318 permits an amplified first order approach, elastic second order approach, or inelastic second order approach.  ACI 318 also provides an alternative analysis for slender walls which is an amplified first order approach and is the basis of ACI 551.2R.  RAM Structural System has implemented an elastic second order analysis to handle the slender wall problem.

In addition to the elastic second order analysis, several features where implemented to facilitate the in-place analysis and design of tilt-up structures in a 3D model.

  • Distributed wall self-weight
  • Gaps (joints) can be assigned to provide analytical separation from adjacent panels
  • Assignment of eccentricity parameter for automatic application of out-of-plane gravity moments
  • Pressure loads on walls
  • Mechanism to isolate out-of-plane behavior
  • Asymmetrical wall reinforcement for different cover on interior and exterior faces
  • Net section consideration for reveals

Wall Self-Weight Criteria

By default, self-weight of walls is computed by story and applied at the top of the member.  This is conservative but can lead to excessive out-of-plane 2nd order effects in slender walls.  An option in RAM Manager – Criteria – Self Weight has been added to distribute wall self-weight to the finite element mesh.  Rather than applying self-weight to the top of the physical wall, self-weight is applied to the top of each shell finite element within the wall.

Modeling Tilt-Up Walls

Since the tilt-up wall analysis is performed in RAM Frame, all tilt-up walls to be considered in the analysis must be modeled as lateral walls.  To distinguish tilt-up concrete walls from cast-in-place concrete walls (default assumption), a type property was added to the wall layout and change properties dialogs.  When tilt-up is selected, the gap properties are available and can be assigned to either end.  Exposure is assigned to the wall faces and impacts reinforcement cover in RAM Concrete Wall.

When modeling tilt-up walls that have a physical joint between panels, the gap assignment is used to provide analytical separation between the walls rather than physical modeling the separation.  Gaps are displayed in plan as orange rectangles with tails that point toward the wall they are modeled on.  In elevation, gaps are displayed as bold orange lines with tabs pointing to the interior of the wall they are modeled in.  A gap only needs to be assigned to one wall end at a joint but can be assigned to both wall ends to facilitate rapid modeling.  However, this can lead to ambiguous conditions for supported members at joints.  RAM Modeler – Integrity – DataCheck will flag these conditions as errors when they occur.

When a wall is modeled on a floor layout, the i-end of the wall is the end that has the lesser X coordinate, or lesser Y coordinate if the X coordinate are the same, regardless of which point is clicked on first when modeling the wall.  The primary face of the wall is on the right side as you walk from the i-end to the j-end of the wall.  When looking at a wall in elevation, you are always looking at the primary face.  RAM Modeler – Options – Show Wall allows the primary face and exposure properties to be turned on in the graphical display.  The primary face arrow points away from the primary face.  Labels for Exterior and Interior exposure assignments are displayed on the corresponding face.

 

Cracked Factor For Out-Of-Plane Bending

An elastic second order analysis requires consideration for cracked regions on the wall.  Stiffness after cracking is a function of internal forces and the placement of reinforcement.  Wall reinforcement is not determined until after the analysis is performed and designed in RAM Concrete Wall.  Therefore, the RAM Frame analysis relies on a cracked factor assigned to the wall that is applied to all finite elements to approximate the cracking effects.  The cracked factor (bending) shown in the Add Concrete Wall dialog above modifies wall out-of-plane stiffness in the RAM Frame analysis. 

ACI 318 permits the use of a reduced moment of inertia with an elastic second order analysis to account for cracking.  ACI 551.2R states that a panel at ultimate load conditions typically exhibits cracks over most of the height and that testing and analytical studies confirm that assuming Ec Icr over the full panel correlates closely with test results.  ACI 318 alternative analysis for slender walls provides an equation for the cracked moment of inertia which is typically less than 0.35 Ig.

The cracked factor (bending) factor requires engineering judgement.  It should represent an effective out-of-plane moment of inertia for a factored load analysis (conditions at strength failure) with a reduction for uncertainty.  It is recommended that the engineer start with a conservative cracked factor to avoid underestimating the 2nd order effects and later refine the cracked factor if more accuracy is desired.

The DA Tilt-Up Tools spreadsheet can be used to help determine if the cracked factor assigned in Modeler is consistent with ACI 318 Alternative Method for Slender Walls.

Assigning Wall Eccentricity

Wall eccentricities are assigned automatically when a wall is modeled based on the default criteria specified in RAM Modeler – Set Defaults – Eccentricities.  After a wall has been modeled, the eccentricity assignment can be changed using Layout – Wall – Change Eccentricity.  Note that wall eccentricity applies to all walls, but currently moments due to the eccentricity are only considered on lateral walls in the RAM Frame analyses.  The eccentricity is measured orthogonal to the plane of the wall and is applied to all loads from one way decking and supported gravity beams/joists.  If a rigid link is assigned to a gravity beam supported by a wall, the rigid link overrides the eccentricity assignment.

 

Wall Pressure Loads

Wall pressures are added in elevation mode in RAM Modeler.  A lateral load case is created in Prop Table – Lateral Load Cases.  There is an option to Lock Diaphragm Displacements which is a separate property for each load case.  When this option is selected, the diaphragm will not displace in the RAM Frame analysis when the load case is analyzed.  The purpose of this option is to isolate out-of-plane behavior from in-plane behavior.  For example, the wind pressure producing out-of-plane bending in a wall is often a components and cladding load that is not necessary to be considered for the main lateral force resisting system.  By preventing the diaphragm from displacing, the engineer can model the components and cladding wind pressures on all walls in a single load case and no in-plane forces will be produced in the 3D analysis.  This option is ineffective for a flexible diaphragm.

Pressure properties are created in Prop Table – Lateral Loads – Wall Pressure Loads.  Pressures are always applied orthogonal to the plane of the wall.  Hence, you define the magnitude of the pressure and whether it acts towards or away from the primary face.  In elevation mode, you are looking at the wall primary face.  The direction towards is into the screen.  Pressure can be defined explicitly as top and bottom pressures (linearly varying between top and bottom based on elevation) or as an inertia force based on the wall weight and fraction of gravity to consider.

Once a lateral load case and pressure property have been defined, pressures can be assigned by referencing a load case, selecting a load property, and applying it to the walls.  Hatching and labels with the assignments will be displayed.

Wall openings have a distribution property to determine how to handle the portion of the wall pressure that exists over the opening.  The pressure can be distributed to the vertical or horizontal sides of the opening, or completely ignored.  Openings are created and changed in elevation mode in RAM Modeler.

 

RAM Frame Analysis Criteria

By default, wall out-of-plane stiffness is ignored in RAM Frame.  Out-of-plane stiffness can be turned in RAM Frame Analysis – Criteria – General.  Typically tilt-up walls are pinned at the base for out-of-plane behavior, so the release rotational fixity option should be selected as well.  Convergence on theoretical results occurs as the mesh sizes decreases and may require the default maximum distance between nodes to be reduced.  However, reducing the mesh size will increase the analysis time.

When gravity moments due to eccentricity and lateral pressures are applied to walls, diaphragms cannot be assigned as flexible or pseudo-flexible because these are no diaphragm conditions.  Without a diaphragm, there is nothing for the wall to lean against in the finite element analysis.  If there are gravity moments due to eccentricity, you will encounter an instability in the analysis or massive displacements.  Similarly, pressures on the wall will produce excessive displacements unless the diaphragm displacements are locked (not applicable to flexible diaphragms) unless your intent is to look at a cantilevered walls with fixed bases.

RAM Frame Elastic Second Order Analysis

The creation of story force cases for in-plane analysis in RAM Frame and the analysis of individual load cases is no different than previous versions of RAM Structural System.  After the load cases have been analyzed, the elastic second order analysis is performed in RAM Frame Analysis – Load Combinations mode.  The Combinations menu has Custom, Strength, and Service Combinations.  The Custom Combinations are the superimposed load case results that are not analyzed.  The Strength and Service combinations are considered in the Advanced Analysis.  The engineer should only create advanced analysis combinations for conditions where an iterative analysis is required.  For example, assume that a single wind pressure case was created for the components and cladding forces that will control the out-of-plane design, and generated story force wind cases were created for the main force resisting system in-plane design.  Small p-delta effects are negligible for the in-plane design and the P-Delta implementation in Frame Analysis Load Cases mode is adequate for any big P-Delta effects that impact in-plane behavior.  Therefore, the advanced analysis combinations can only include combinations that include the out-of-plane pressure case as shown below.

The criteria defined in Load Cases mode is used in the load combination analysis, as well.  Some criteria will cause the analytical model for a gravity case to be different than a lateral load case.  This would present a problem for the analysis of a load combination that contains both cases.  Errors will be thrown when these conditions occur.  The user will need to change the selections in Load Cases mode before proceeding with the load combination analysis.

Additional criteria that is only relevant to elastic second order analysis exists in RAM Frame Analysis -Load Combinations mode – Criteria – Advanced Analysis.  As discussed previously, the cracked section factors entered in RAM Modeler are intended to be used for a strength analysis.  When analyzing service conditions, the crack factors can be relaxed.  Rather than entering separate cracked factors for strength and service combinations, a single cracked factor modifier is entered for service combinations (see Service Analysis section below).  Live load reduction can be turned enabled or disabled.  Trouble shooting criteria for the iterative analysis is available to assist in achieving convergence.

The advanced analysis is performed by going to Process – Advanced Analysis, selecting the combinations to consider, and then clicking OK.  If advanced combinations have not been defined or no valid combinations are selected, the combination type will have a red status light.

Viewing and reporting of load combination analysis results requires selection of the appropriate load combination type to consider.  Reports and onscreen results only consider the active output mode load combination type.  Similarly, the Frame Shear Wall Forces module has a dialog to select the combination type for envelope results.

Service Analysis

The service combination analysis in RAM Frame Analysis Load Combination mode is an elastic 2nd order analysis that scales the cracked factors assigned in RAM Modeler by the service multiplier in Criteria - Advanced Analysis.  The service analysis in the ACI Alternative Method for Out-of-Plane Slender Wall Analysis is an iterative bilinear interpolation that considers the displacement at the cracking moment with the gross moment of inertia and the displacement at the nominal moment with the cracked moment of inertia.  The out-of-plane displacements in RAM Frame will be larger than displacements calculated using ACI slender wall for practical moments.  If the maximum nodal displacement in RAM Frame for the service combination exceeds displacement limits, a more detailed analysis should be performed prior to changing wall stiffness.

First, rerun the service analysis using the gross moment of inertia.  To force the service analysis to use the gross moment of inertia, the service modifier in the advanced analysis criteria should be larger than 1 divided by the bending cracked factor assigned in RAM Modeler.  The program will cap the stiffness at 1.0 times the gross moment of inertia in the analysis.  If the maximum service moment in the wall considering 2nd order effects is below 2/3 the cracking moment, then the wall remains uncracked for the service combination per ACI slender wall.  The assumption to use the gross moment of inertia was valid.

If walls are cracked, rerun the service analysis with a service modifier that brings the cracked factor assigned in RAM Modeler to a service state (e.g. 1.4).  If the cracked factor in Modeler represents a fully cracked section, the RAM Frame results are conservative and can used directly if desired.  If displacements are exceeding deflection limits, the service modifier typically can be increased because the service moments are less than the moment that reduces stiffness to fully cracked.  However, this is decision that requires engineering judgment.

The DA Tilt-Up Tools spreadsheet can be used to help investigate the service analysis.

RAM Concrete Wall

RAM Concrete Shear Wall has been renamed RAM Concrete Wall in v17.00.  The program was enhanced to allow reinforcement to be placed asymmetrically and consider reveals.  In addition, consideration of the advanced analysis strength combinations and tilt-up reinforcement cover have been added.

The generated and custom load combinations superimpose the load case results to create a load combination force.  Assuming the 2nd order analysis was performed for out-of-plane forces only, the generated and custom combinations should only consider in-plane cases.  The strength load combinations considered in the elastic 2nd order analysis can be selected for design in RAM Concrete Wall – Load Combinations – Advanced.  All selected combinations are considered in the design of all section cuts.

The criteria in Concrete Wall – Criteria – Design Criteria has options for cover and bar placement at wall face.  Tilt-Up walls use the minimum cover requirements for precast.  Exterior faces assume weather exposure that require additional cover per ACI 318.  RAM Concrete Wall – Assign – Wall Panel Clear Cover allows the engineer to override the global cover criteria.  Tilt-up walls typically have the vertical bars closest to the wall face to maximize the out-of-plane flexural capacity for a wall spanning vertically.  Previous versions assumed the vertical bars were inside the horizontal bars.  Therefore, separate placement options exist for the Cast-In-Place and Tilt-Up wall types.

Concrete Wall – Assign – Wall Pane Reveal Depths allows a depth to be specified that impacts bar placement and the concrete section considered in design.  For example, if a wall is 10” thick with 1” of clear cover and there is a 0.75” reveal on the primary face, the cover to the bars closest to the primary face is measured from inside the reveal depth.  If the vertical bars are closest to the face, the distance from the face of the 10” wall to edge of the vertical reinforcement edge is 1.75”.  The reveal depth is applied to all section cuts in the wall panel.  The concrete section considered in strength calculations excludes the reveal depths.

Critical horizontal sections for in-plane forces typically occur at the bottom of walls and openings.  For out-of-plane design, critical horizontal sections will often occur mid-height where the out-of-plane moment is the largest.  The program does not attempt to locate the maximum out-of-plane moment and add a section cut at that location.  The engineer is required to add cuts where they are desired to be checked.  If it is not obvious where the critical section for out-of-plane flexure will occur over the height of the wall, the engineer can use maximum cut spacing parameters in the section cut generator to create multiple cuts over the height of the wall.  However, increasing the number of section cuts will increase the design time.

The Concrete Wall – Process – View/Update dialog and section cut design summary report include an out-of-plane shear check.  Reveal locations and accurate bar placement can be visualized in the section view.  Axial-flexure interaction has always considered weak axis moments in the wall.  Pure out-of-plane bending occurs with a beta angle of 90 or 270 degrees.

Tags: RAM, tiltup, Tilt-up

RAM Concept Load History Deflection Calculations

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Current Revision posted to RAM | STAAD | OpenTower Wiki by Karl G on 12/23/2020 2:41:10 AM

Long-term concrete deflections are difficult to predict due to the influence of several non-linear behaviors that complicate the calculations. Historically, design engineers have relied on approximate methods, like deflection multipliers, to simplify the calculations and estimate long-term deflection. Although these methods reduce the calculation effort, they crudely approximate or even exclude some of the important non-linear behaviors and may predict unconservative deflections as a result.

The load history deflection analysis in RAM Concept follows a more rigorous approach that is based on detailed, time-dependent curvature calculations on cross sections. These rigorous calculations accounts for each of the following behaviors that influence long-term concrete deflections:

  • Material Nonlinearity
  • Early Age Concrete Strength
  • Cracking
  • Tension Stiffening
  • Creep
  • Shrinkage
  • Internal Restraint to Shrinkage (from reinforcement)
  • External Restraint to Shrinkage (from stiff supports)
  • Load History

This article briefly discusses how each of these behaviors are included in RAM Concept’s load history deflection implementation.

Material Nonlinearity

The modulus of elasticity is an important concrete property for long-term deflection calculations because it is directly associated with element stiffness. Although the stress-strain curve of concrete is non-linear (see figure below), in a finite element or frame analysis, the modulus of elasticity is normally assumed to be a constant value as prescribed by the governing building code or standard

RAM Concept uses the PCA concrete stress-strain curve in its cross-section calculations and in doing so considers the material non-linearity of concrete in the load history calculations. At each cross section, the non-linear stress-strain curve is used to determine the concrete material stress from the calculated long-term cross section strains. These stresses are integrated over the cross section to calculate forces resultants, which are calculated to be in equilibrium with the external loads acting on the cross section.

Early Age Concrete Strength

Concrete compressive strength is an important property for accurate deflection prediction because it is used to determine other material properties like the modulus of elasticity (associated with member stiffness) and the modulus of rupture (associated with cracking). Although concrete strength increases over time, it is common to analyze and design concrete structures using a 28-day concrete strength (f’c). Using f’c in deflection calculations, however, can lead to unconservative deflection predictions, especially if construction loads are significant and cause cracking at an earlier age when the concrete strength is lower.

RAM Concept automatically adjusts the modulus of rupture to the actual time of loading to account for reduced strength at early age loading steps and more accurately calculate long-term deflections. These adjustments are calculated using equations referenced in the design code associated with the selected creep/shrinkage model.

Cracking

Cracks initiate when an applied load or shrinkage strain produces a tensile stress that exceeds the cracking stress. When a crack forms, stress is relieved at the crack location and a redistribution of stress occurs, which may cause cracks to form in other areas. At cracked cross sections, there is a decrease in stiffness and an increase in cross section curvature, which leads to increased deflections.

RAM Concept accounts for cracking of sections subject to axial and flexure by comparing the calculated tensile stress at the extreme top and bottom fibers with the calculated modulus of rupture. The tensile stress calculations are based on transformed cross sections, which can contain concrete, mild-reinforcement, post-tensioning, or any combination thereof and consider long-term effects such as restraint to shrinkage (both internal and external) and creep. When the calculated tensile stress is less than the modulus of rupture, the section is considered uncracked. In this case, RAM Concept uses a concrete stress-strain curve that accounts for the ability of concrete to resist both tension and compression. When the tensile stress exceeds the modulus of rupture, the section is considered cracked. In this case, RAM Concept calculates cracked curvatures based upon a concrete stress-strain curve that has no tension capacity.

Tension Stiffening

Tension stiffening refers to the ability of concrete to resist tension between cracks and the stiffness that is provided by this tension. This effect is reduced as the loading and cracking is increased. Normally, the mean curvature used for deflection calculations is interpolated between the calculated uncracked transformed curvature and the cracked curvature using a tension stiffening model. Examples of tension stiffening models used in practice include the models developed by Branson (see ACI 381-14 24.2.3.5), Bischoff (see ACI 318-19 24.2.3.5), and the model outlined in Eurocode 2-2004 (Equation 7.19).

RAM Concept uses the Eurocode 2 tension stiffening model for load history calculations with all building codes and creep/shrinkage models, with the following modifications:

  1. Mcr (gross section cracking moment) is replaced with fcr (concrete modulus of rupture), and Ma (gross section resultant moment) is replaced with fa (gross section top or bottom tensile stress). This modification is required because the original formula does not consider axial forces in combination with bending, which may be present and are especially important when post-tensioning is present.
  2. b is assumed equal to 1. Eurocode 2 states that b should be taken as 1 for short-term loading and 0.5 for long-term loading (see Clause 7.4.3). Some experts have concluded that b is equivalent to reducing the cracking moment by about 30 percent and is an approximate way to account for shrinkage induced cracking (i.e. shrinkage restraint)1. Since this behavior is already accounted for in RAM Concept’s load history calculations (see “Internal Restraint to Shrinkage” and “External Restraint to Shrinkage” below), the program uses b = 1 to avoid double counting that effect.

RAM Concept accounts for redistribution of forces using element stiffness adjustments and an iterative analysis. For each cracked cross section, RAM Concept calculates an elements stiffness adjustment using the ratio of the linear elastic section curvature to long-term section curvature and applies it to all finite elements that are tributary to the section. After the element stiffness adjustment is applied, another analysis is completed, and the cross-section strain/curvature calculations are repeated. This iterative process continues until the calculated deflections converge for the loading stage.

Reference

1 Gilbert, R.I and Ranzi, G., “Time-Dependent Behavior of Concrete Structures”, CRC Press, 2019.

Creep

Creep accounts for the increase in concrete strain with time due to sustained loads. Typical concrete creep strains range between 2-4 times the elastic strain and are important for accurate prediction of long-term deflections as a result. Actual creep behavior is affected by the rate of load application and the variation of concrete strength over time.

RAM Concept calculates a differential creep strain over the duration of each loading stage using one of the following creep models that are implemented in the program: ACI 209R-92 (ECR Values), ACI 209.2R-08/GL 2000, AS 3600-2018, and Eurocode 2-2004. When calculating the strains and combining the effects over the load history, RAM Concept assumes that the creep strains are a linear factor of the elastic strain for a particular load and that creep strains of like or opposing signs can be superimposed. These assumptions are reasonable for typical service loads.

RAM Concept uses the age adjusted effective modulus method, which adjusts creep strains using an ageing coefficient, to approximate the effects that age and rate of loading have on creep behavior. The resulting modified creep strains are then used in the cross-section strain compatibility calculations.

Shrinkage

Shrinkage is the reduction in concrete volume over time due to hydration of cement, loss of moisture, and other factors. It occurs independent of loading and is normally specified as a strain. In general, restraint to shrinkage (see following sections) causes time-dependent cracking and increases long-term deflection.

RAM Concept calculates a shrinkage strain for each loading stage using one of the following shrinkage models that are implemented in the program: ACI 209R-92 (ECR Values), ACI 209.2R-08/GL 2000, AS 3600-2018, and Eurocode 2-2004. The resulting shrinkage strains are then used in the cross-section calculations. Due to strain compatibility, the imposed shrinkage strain results in internal stresses in the reinforcement (normally compression) and concrete (normally tension) caused by shrinkage strains.

Internal Restraint to Shrinkage

Internal restraint to shrinkage is due primarily to bonded reinforcement. As concrete shrinks, the reinforcement is compressed, and an equal and opposite tension force is induced in the concrete. When the reinforcement in the section is asymmetric (more bottom reinforcement than top reinforcement, or vice versa), this tension force is eccentric to the centroid of the concrete section and a curvature is imposed on the section. This curvature, also known as shrinkage warping, may cause cracking to occur and increase deflection as a result. In extreme cases, cracking due to shrinkage warping may occur in the absence of superimposed loads.

RAM Concept rigorously accounts for the shrinkage warping effect in the strain/curvature calculations at each cross section, considering all reinforcement intersecting the section. The approach is similar to the one outlined in Eurocode 2 -2004 Clause 7.4.3(6) Equation 7.21.

External Restraint to Shrinkage

External restraint to shrinkage from stiff supports or adjacent slabs can lead to a build-up of tensile stress and increased cracking in concrete floors. Failure to account for this effect in long-term deflection calculations may lead to unconservative results.

RAM Concept accounts for external shrinkage restraint using an input External Shrinkage Restraint setting, which translates to a shrinkage restraint percentage. This percentage is multiped by the shrinkage strain at any loading stage to estimate a “restrained” shrinkage strain. This fictitious strain is then superimposed with the strains caused by loads and other effects and applied to the tension stress calculation used in the tension stiffening model but not the cross-section strain/curvature calculations. As such, the fictitious external restraint strain affects cracking prediction only but not the calculated curvatures directly.

Load History

Load history is an important consideration for accurate deflection prediction, especially for structures subject to significant construction loads that cause early age cracking. RAM Concept accounts for load history using a series of user defined loading steps, which are mapped with a load combination and a load duration. Each loading step considers the effect of cracking, creep, and shrinkage from all previous steps. Creep strains are all linearly superimposed, and an unloading event is considered the same as a subsequent loading event of opposite sign as a previously applied loading. Once a cross section is determined to be cracked during a particular loading stage, it is assumed to be cracked for all future iterations and load history steps.

Related Publications Authored by the RAM Concept Team

  1. Hirsch, J., “Accurate Long-Term Deflection Prediction in Flat Slabs Using Linear Elastic Global Analysis”, 24th Biennial Conference of the Concrete Institute of Australia, Sydney, Australia, 2009.
  2. Hirsch, J., Calabrese, F., Connolly, E., and Bommer, A. “Practical Deflection Prediction of Concrete Slabs”, ACI SP284-18, March 2012.
  3. RAM Concept Manual, Chapter 70 “Load History Deflections”

Tags: shrinkage, creep, RAM Concept, tension stiffening, load history, concrete, Shrinkage Restraint, deflection, cracking

RAM Concept Load History Deflection Analysis Results Table

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Revision 2 posted to RAM | STAAD | OpenTower Wiki by Karl G on 12/23/2020 2:54:22 AM

RAM Concept’s load history deflection calculations are complex due to the many non-linear behaviors that are considered (see Load History Deflection Calculations for more information). When unexpected results are obtained, it can be difficult to verify the calculation or even isolate the effect of the different behaviors (creep, shrinkage, cracking, etc).

The Load History Deflection Analysis Results Tables were added in RAM Concept Version 8 Update 2 to give the user more access to the data used to calculate the load history deflections. These tables include both information that is directly used by RAM Concept to calculate the load history deflections and information that is not used directly but is useful for better understand the relative importance of different behaviors. A separate table is available for each load history step. Each table includes information for all sections, both span sections and design sections, included in the model.

This article defines the information included in the table and provides insight on how the information might be used.

Definition of Tabulated Items

Fa/Fcr– The ratio of the calculated axial stress at the extreme fiber of the section over the cracking stress (normally the modulus of rupture). A separate ratio is tabulated for both the top and bottom of the section. The calculated axial stress is the result of applied loads and induced strains, including the shrinkage restraint %. A section is considered cracked when this ratio is greater than or equal to 1.

Fa/Fcr (unrestr.)– The Fa/Fcr ratio above but with the effect of the shrinkage restraint % removed. A ratio is tabulated for both the top and bottom of the section. These ratios are not used directly in the load history calculations. They are intended to be compared with Fa/Fcr ratios, which include the effect of the shrinkage restraint %, to better understand the influence of external restraint to shrinkage on the load history deflection calculations.

Modulus of Rupture– The calculated modulus of rupture, which is normally the cracking stress of section. The tabulated value includes adjustments to account for reduced concrete strength at early ages (less than 28 days). Refer to the RAM Concept Manual for more information on this adjustment.

Max Fa/Fc Ratio – The maximum ratio of the calculated axial concrete compressive stress in the section over the concrete compressive strength. A ratio is tabulated for both the top and bottom of the section. This ratio may be used to identify sections with high compressive stress that may be subject to non-linear creep behavior (see AS 3600-2018 3.1.8.3 and Eurocode 2-2004 3.1.4(2)). Non-linear creep behavior is not accounted for in RAM Concept’s load history deflection calculations.

Max Fs/Fy Ratio – The maximum ratio of the calculated tensile stress in the reinforcement over the yield stress of the reinforcement. A separate ratio is tabulated for the extreme top and bottom reinforcement. The reinforcement is yielding when this ratio is greater than 1. A ratio much larger than 1 indicates excessive yielding, which could lead to significant element stiffness reduction and possible local instability.

Incr. Creep Coefficient– The incremental creep coefficient (creep strain/elastic strain) over the duration of a given load history step based upon a loading applied at the initial load application time. This coefficient excludes the creep effects from any previous load history step. The coefficient includes adjustments to account for time of loading for creep models that calculate creep based on the modulus of elasticity (Ec) at the time of loading instead of the 28-day Ec (refer to the RAM Concept Manual for details).

***. Creep Coefficient– The cumulative creep coefficient (creep strain/elastic strain) over the total age of a given load history step based upon a loading applied at the initial load application time. This coefficient includes the creep effects from all previous load history steps. The coefficient includes adjustments to account for time of loading for creep models that calculate creep based on the modulus of elasticity (Ec) at the time of loading instead of the 28-day Ec (refer to the RAM Concept Manual for details).

Incr. Shrink. Strain - The incremental shrinkage strain over the duration of a given load history step. This strain excludes the shrinkage from any previous load history step.

***. Shrink Strain - The cumulative shrinkage strain occurring up to the end of a given load history step. This strain includes the shrinkage from all previous load history steps.

Gross Curvature – The calculated curvature using gross section properties caused by externally applied loads and post-tensioning only.

Uncr. Trans. Curvature– The calculated curvature including the effects of creep and internal restraint to shrinkage on the uncracked transformed concrete section.

Cracked Curvature - The calculated curvature including the effects of creep and internal restraint to shrinkage on the cracked transformed concrete section.

Mean Curvature– The average curvature interpolated between the uncracked transformed curvature and the cracked curvature using the tension stiffening model. This curvature includes the effects of external restraint to shrinkage. The element stiffness reduction is determined by the ratio of the mean curvature to the gross curvature.

Uncr. Shrink Warp.– The calculated curvature due to only internal restraint to shrinkage (shrinkage warping) on the uncracked transformed section. This ratio can be compared with the uncracked transformed curvature to better understand the influence of internal restraint to shrinkage on the load history deflection calculations.

Cracked Shrink. Warp. - The calculated curvature due to only internal restraint to shrinkage (shrinkage warping) on the cracked transformed section. This ratio can be compared with the cracked transformed curvature to better understand the influence of internal restraint to shrinkage on the load history deflection calculations.

Mean Shrink. Warp.– The average curvature due to only internal restraint to shrinkage (shrinkage warping) interpolated between the uncracked transformed and cracked shrinkage warping curvatures. This ratio can be compared with the mean curvature to better understand the influence of internal restraint to shrinkage on the load history deflection calculations.

Tags: shrinkage, curvature, creep, RAM Concept, load history, results, concrete, table, deflection, cracking

xRAM Concept Load History Calc Options (Versions Prior to Version 8 Update 2)

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Revision 1 posted to RAM | STAAD | OpenTower Wiki by Karl G on 12/23/2020 2:15:10 PM
 Applies To 
 Product(s):RAM Concept
 Version(s):Various
 Area: Analysis

Load History Parameters in RAM Concept

RAM Concept uses the ACI 209R-92 models for creep and shrinkage. In these models, only modifications that are a function of time are accounted for internally by the program. Other factors that affect creep and shrinkage rates are defined by the user in the Calc Options dialog (see Figure 1 below). The purpose of this tech note is to describe how these parameters are used in the load history calculations and discuss the default values.

More discussion on the theoretical basis for the load history deflection method used in RAM Concept can be found on the following web page:

Load History Article

Figure 1. Load History Parameters in Calc Options Dialog

Creep Factor

The creep factor is defined as the ratio of total strain (elastic strain + creep strain) to elastic strain. According to ACI 209, an average value creep strain:elastic strain is 2.35. As a result, RAM Concept adopts a default creep factor of 1 + 2.35 = 3.35. The ACI 209 average value and the RAM Concept default are based on standard conditions. Other factors, like curing method, concrete composition, and cement content, can affect creep and should be incorporated into the creep factor that is defined.

The ACI 209 creep model assumes that the initial loading is applied at 7 days. Some codes, like AS 3600, assume a different time for initial load application. When using the load history calculations in RAM Concept, the creep factor should be converted for an initial loading time of 7 days.

ACI 209 defines a modification factor for initial load application times other than 7 days. This correction is automatically included in the load history calculations and should not be incorporated into the input creep value. The initial load application time defined in the Calc Options dialog is used to calculate this correction. This correction factor is automatically calculated and applied for each load history step and is based upon the time of application of loading in each step.

Shrinkage Strain

According to ACI 209, average shrinkage strains range from 0.000415 to 0.001070 for standard conditions. RAM Concept uses a default value of 0.0004.

Environmental factors, especially ambient relative humidity, can have a significant impact on the ultimate shrinkage strain and should be considered when inputting the value in the Calc Options dialog. If the relative humidity is low, the shrinkage value could be significantly higher than the default value.

ACI 209 defines a modification factor for shrinkage strain for conditions with a moist cure duration other than 7 days. RAM Concept uses the input Moist Cure Duration in the Calc options dialog to automatically account for this modification. Input shrinkage strains should not include this modification.

Shrinkage Restraint

Elements like stiff columns and walls restrain shrinkage movements and cause a gradual buildup of tensile stress in the concrete, which leads to cracking. The shrinkage restraint percentage is a simple way to account for this cracking. The higher the percentage the earlier cracking will occur and the more the tension stiffening effect will be reduced.

RAM Concept uses the shrinkage restraint percentage as follows:

The ACI 209 time function for shrinkage and the input ultimate shrinkage strain are used to calculate the shrinkage strain at each given time step. This shrinkage strain is multiplied by the defined shrinkage restraint percentage. This tension strain is then summed with the modified concrete strain determined in the load history calculations (accounting for creep, etc.) for use with the concrete stress-strain curve to find the concrete stress.

Here is a simplified numerical example, illustrating the effect of the shrinkage restraint percentage:

  • User input shrinkage strain = 0.0004
  • User input shrinkage restraint = 10%
  • Elastic Modulus of Concrete = 3605 ksi

Assuming the concrete is linear elastic, the stress increase due to the shrinkage restraint would be (3605ksi)*(0.0004)*(0.1) = 0.144 ksi. This is roughly 1/3 of the cracking stress. In other words, the shrinkage restraint is reducing the cracking moment by about 1/3.

From a practical standpoint, setting the restraint percentage to 30% would reduce the cracking moment to zero (in the
absence of axial compression), cause all elements on the floor to crack, and significantly increase deflections. Increasing the value above 30% would have very little effect, since it would not affect cracking and would only reduce the tension stiffening effect slightly.

The following are some recommendations for the user input shrinkage restraint assuming an ultimate shrinkage strain of 0.0004 (use engineering judgment for interpolations between):

  • 0% - unrestrained or very lightly restrained slabs (flexible columns only, single stiff element)
  • 10% - normally restrained slabs (more than one stiff element, some flexibility)
  • 20% - completely restrained slabs (basement walls around entire perimeter, etc. causing a high degree of restraint)

For other values of shrinkage strain, the percentages can be calculated based on an appropriate reduction to the cracking moment using the simple numerical example above. For example, for a given shrinkage strain and a desired reduction in cracking moment of 33%, the user input shrinkage restraint would be calculate from fr*0.33/(E*n)

Where,

fr = modulus of rupture

E = Elastic Modulus of Concrete

n = shrinkage strain

Ageing Coefficient

The ageing coefficient accounts for the rate of application loading for the calculation of creep effects. The RAM Concept Manual describes this parameter as follows:

“An ageing coefficient is used as a modifier of creep to account for the rate of application loading, its effect on the creep and the variation of concrete strength over the time period. While the rigorous calculation of the coefficient is rather involved, this value can normally be taken as 0.8 with little loss in accuracy.”

See Also

Load History Article

Ram Concept - Load History Convergence

RAM Concept Load History Deflections and ACI Deflection Limits

Structural Product TechNotes And FAQs

Tags: shrinkage, creep, RAM Concept, load history, concrete, Deflections
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