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Ram Frame Analysis Log Warnings

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Revision 1 posted to Structural Analysis and Design - Wiki by Seth Guthrie on 12/17/2013 5:55:15 PM

  
 Applies To 
  
 Product(s):RAM Structural System
 Version(s):Any
 Environment: N/A
 Area: Anaysis
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

 

 

 

 

 

 

 

 

The Ram Frame analysis completes but indicates there are warnings, where can I find more?


Use the Report - Analysis Log to get further details. Warnings are listed at the beginning of the report under "Summary of Numerical Behavior of Model". The most common illustrated below:

  1. Local instability at or near Node # (0.00, 0.00, 12.00)
  2. Line Load on Wall # of Story "Roof"  Found (starting at 0.000 ft and ending at 8.916 ft). The Portion of this load over Opening Ignored in Analysis. 
  3. Beam  62 (Roof)  Has Larger Rigid End Zone Lengths (REZ) Than Member's Length. REZs Set to Zero. 

1. Local, instabilities. The instability wiki discusses some common causes for these. Typically they occur where all the frame members at a joint are pinned leaving the node free to rotate.

2. Loads on walls partially ignored. This happens when an opening in a wall crosses a story line when there are floor decks/loads or line loads modeled on the floor that is met or crossed. The plan view does not show these openings so the elevation view should be used to review these conditions. Note, it’s only the loads from one-way decks, lines loads and wall self-weight affected by the warning, loads from meshed 2-way decks are still considered.

3. Rigid end zone warnings. These tend to happen when the length of the Rigid End Zone based on intersecting beam and column dimensions is greater than the center to center length of the member. In those situations, the original center to center length is used inthe stiffness matrix for the affected members.

The next section, "Summary of Equilibrium Check of Model" includes the total reactions for each loading. The program includes the nodal reactions of all columns and walls even if they terminate higher than the base, so the sum of the reactions can be checked against the total applied loads to confirm equilibrium, Small deviations are expected when performing P-Delta analysis.


Note, the summation of moments is now reported about that global model origin so that overturning equilibrium can also be evaluated. In older versions (< v14) the reported moments were a simple summation of the column base moment reactions. Refer to the Modeling wiki for more on story height and how it affects the elevation of rigid diaphragm lateral loads

 

See Also

Structural Product TechNotes And FAQs

RAM Instability In Finite Element Analysis

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: analysis, RAM Frame

SELECTsupport TechNotes And FAQs

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Revision 309 posted to Structural Analysis and Design - Wiki by Seth Guthrie on 12/17/2013 5:57:46 PM

Key:
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TB – Technical Bulletin TN – TechNote
VID – SELECTsupport Video

The following TechNotes and FAQs are provided as a reference by Bentley's Technical Support Group.

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Tags: STAAD.Pro, RAM Concept, RAM Elements models, RAM Connection, MultiFrame

RAM Connection Capabilities and Modeling FAQ

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Revision 7 posted to Structural Analysis and Design - Wiki by Seth Guthrie on 12/18/2013 7:57:59 PM

  
 Applies To 
  
 Product(s):RAM Connection
 Version(s):Any
 Environment: N/A
 Area: N/A
 Subarea: 
 Original Author:Bentley Technical Support Group
  

 

 

 

 

 

 

 

Can I assign a section such as a HSS or channel to a beam?

Currently, only I-shaped sections can be assigned to beams in RAM Connection. It is not possible to assign other section types, like HSS or channels, to beam members.

 

What is the difference between Basic Connections and Smart Connections?

The RAM Connection Manual defines these connections as follows:

Basic Connection:  A connection template that can automatically adjust the geometry (position or dimensions) of the connection pieces to fit the connection members. It does not calculate the quantity or dimensions of the connecting pieces (bolts, plates, etc) to resist the applied forces.

Smart Connection: A connection template that can automatically calculate the quantity and dimensions of the connecting pieces (bolts, welds, plate sizes etc) to resist the applied forces.

When basic connections are designed, the program searches through a list of predefined connection templates and selects the first connection in the list that satisfies the design requirements.

When smart connections are designed, the program optimizes the connection parameters. See the RAM Connection Manual for a list of parameters that are optimized for each connection type. If a parameter is not optimized, the program uses a default value that be modified in the Connection Pad as needed.

 

Where are the abbreviations used for joint types and connections defined?

The abbreviations are defined in the RAM Connection Manual. In the v8.0 Manual, the naming conventions for both joints and connections are listed on page 42 and 43.

 

How can I change the design code (AISC 360 or BS 5950) or the design method (ASD or LRFD)?

In RAM Connection Standalone:

  1. Click on the Design menu tab at the top of the program window.
  2. Find the Assignment toolbar.
  3. Double click on the small square box with arrow pointing to the lower right corner to open the Customize Connection Design dialog.
  4. Edit the design code or design  method.

In RAM Connection for RAM Structural System:

  1. Click on the Design menu tab at the top of the program window.
  2. Find the Assignment toolbar.
  3. Double click on the small square box with arrow pointing to the lower right corner to open the Customize Connection Design dialog.
  4. Edit the design code or design method.

In RAM Connection for Elements:

The design code and design method is controlled by the code selected for design when performing a design in the RAM Elements model. To change the design code or design method, redesign the model and choose the desired design code.

Changing the design code will not automatically update generated load combinations. After changing the design method, delete and regenerate the load combinations.

 

When designing a base plate connection, the ACI 318 Appendix D checks are not completed.

Since the ACI Appendix D checks are based on ultimate limit state design, RAM Connection will only complete the ACI Appendix D checks if LRFD is selected for the design method. See frequently asked question above for information on changing the design method.

 

Information that is modified in the Connection Pad is not saved after clicking the Save button and exiting the dialog.

Any item that has an icon with a red arrow to the left of it (see figure below) is defined in a dialog outside the Connection Pad. These parameters can be edited in the Connection Pad, but the information will be lost after closing the dialog. To change the parameters permanently, modify the values in the dialog where the information is initially defined. Edit the Joint to modify loads, section, materials, etc. Edit the seismic provision options in the Customize Connection design dialog.

 

Can I design a Gusset Connection using a Pipe Column?

No, currently in Column-Beam-Brace joints (CBB) only Wide flange (W) and Square or Rectangular Tube (HSS-rect) shaped sections can be used for columns. Circular shapes can be used as columns in some joints but not the gusset type. A change request for pipe columns in these joints has been logged.

The Results Report identifies the controlling load condition as a load case. The design should be based on load combinations and not individual load cases.

RAM Connections completes a design check for all load conditions, including individual load cases and load combinations. For some connection types, such as a base plate connection with wind uplift, the design for an individual load case may control the design. The load cases can be removed as follows:

In RAM Connection Standalone:

  1. Enter the Connection Pad by either double-clicking the large 3D display of the connection or clicking on the Design menu tab – Connections toolbar – Edit.
  2. In the Connection Pad, click on <Loads> to open the Loads worksheet.
  3. Click on the Load # associated with the load case and then click on the Delete button on the keyboard to delete it from the worksheet.

Please note that this will not permanently delete the load case results from the worksheet. See frequently asked question above for details.

In RAM Connection for RAM Structural System:

  1. Enter the Customize Connection Design dialog by clicking on the Design menu tab – Assignment toolbar – Small square box in lower right corner of the toolbar.
  2. Click on the “Select All Load Combinations” button to only select the load combinations.

In RAM Connection for Elements:

  1. Enter the Connection Pad by either double-clicking the connection box at the joint where the connection is assigned or clicking on the Modules menu tab – Connections toolbar – Edit.
  2. In the Connection Pad, click on <Loads> to open the Loads worksheet.
  3. Click on the Load # associated with the load case and then click on the Delete button on the keyboard to delete it from the worksheet.
  4. If a second-order analysis was done in RAM Elements, you can bypass Steps 1-3 by unselecting the individual load cases when analyzing the model in the main program.

I'm designing a connection with seismic provisions, but the Ry and Rt values don't look right, what's wrong?

Ry (Yield strength ratio) and Rt (Tensile strength ratio) are properties of the material in Ram Connection. The can be reviewed using Home - Databases - Materials - Edit.

To add your own materials with different values, refer to the wiki Creating custom elements in RAM Elements which also applies to Ram Connection.

Note, imported materials from RAM Structural System or STAAD.pro may not have the expected values for Ry and Rt since those are not directly supplied by either of those applications. For Ram Elements users with imported RAM SS files, edit the imported RAM SS materials as shown below (or reassign different steel materials to the members):

For STAAD users, be careful to define the proper values when using the RAM Materials dialog box within the connection mode.

For further details refer to How to Customize a RAM Connection Template in STAAD.Pro 

 

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: RAM Connection, Joints

RAM SS Walls FAQ

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Revision 8 posted to Structural Analysis and Design - Wiki by kjgullerud on 12/19/2013 9:45:10 PM

  
 Applies To 
  
 Product(s):RAM Structural System
 Version(s):Any
 Environment: N/A
 Area: N/A
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

 

 

 

 

 

 

 

 

Ram Structural System - Walls FAQ

What is the difference between "Cracked Factor (membrane)" and "Cracked Factor (bending)?"

The wall element stiffness is separated into membrane stiffness (in-plane behavior) and plate bending stiffness (out-of-plane behavior). In RAM Modeler, Cracked Factor (membrane) and Cracked Factor (bending) can be used to adjust each of these.

Understanding the wall element stiffness formulation used in RAM Frame is key to understanding how the cracked factors. The wall element stiffness formulation is discussed in Section 6.4.4 of the RAM Frame Analysis Manual v14.06. Shells are 4-sided elements with 6 degrees of freedom at each node. When determining the element stiffness, the stiffness associated with these degrees of freedom are separated into a membrane stiffness matrix and a plate bending stiffness matrix. The membrane stiffness include stiffness associated with the two in-plane translational degrees of freedom and the drilling degree of freedom (in-plane rotation). The plate stiffness matrix includes stiffness associated with the remaining two rotational degrees of freedom and the out-of-plane translational degree of freedom. The membrane cracked section factor is applied to membrane stiffness matrix and affects in-plane translational (horizontal and vertical) and in-plane rotation. The plate cracked section factor is applied to the plate bending stiffness matrix and affects out-of-plane rotations and translation. The out of plane stiffness can also be completely ignored in the Ram Frame analysis under Criteria - General - Wall Element by unchecking the option to "Include out-of-plane stiffness (bending)":

In summary,

Cracked Factor (membrane) applies to in-plane wall stiffness. It affects behavior associated with axial forces, overturning moments and major axis shear (the shear stiffness is related to the membrane stiffness by Poisson's ratio and Hooke's Law) .

Cracked Factor (bending) applies to out-of-plane wall stiffness.

3-Dimensional (3D) Effects of Wall Groups

The following example illustrates how the finite element analysis of connected walls produces drastically different results than a simple two-dimensional approach. When walls are modeled in RAM Structural System such that they form a corner, it is important to understand what is happening at the point of intersection.  Because the walls frame into a common node, they will both affect the stiffness of that node.  In the RAM Frame manual, on Page 78, it states, “Since RAM Frame assembles the stiffness coefficients of its elements in a 3-Dimensional Fashion, walls that intersect at an angle (and hence share common nodes) form a 3-D system and the 3-D behavior is captured by the analysis.”  This is correct and consistent with proper Finite Element Analysis.

Typical 3-Dimensional FE-based analysis programs all Consider the 3-dimensional nature of connected walls this way. The member force output, however, is reported for the individual walls segments.

Case 1 - Consider the example of a simple building is 20 ft square with 10’ high shear walls all the way around the perimeter. A 100k lateral load is applied at the center of the rigid diaphragm and the wall forces are as follows:

#PM majorV major
1-27.970.000.00
20.00220.3350.00
30.00220.3350.00
427.970.000.00

Thus the overturning moment from the lateral load (100k x 10ft = 1000k-ft) is resisted by the parallel walls in the form of overturning moment, and in the end walls in the form of coupled axial forces:

220.33k-ft + 220.33k-ft + (27.97k x 20ft) = 1000k-ft

It should be noted that the percentage of the total overturning resisted by the walls parallel to the load can be dramatically affected by the size of the mesh. In this example, the walls were all meshed in 2.5’ squares).

 

Case 2 - The results change drastically if we place a small gap between the four wall elements so that they no longer share common nodes. Now the wall forces are as follows:

 

#PM majorV major
10.000.000.00
20.00500.0050.00
30.00500.0050.00
40.000.000.00

Here, the overturning moment is resisted entirely by the walls oriented parallel to the force.

Note, the wall elements considered in this example have zero out-of-plane stiffness, so the walls perpendicular to the load offer no resistance. For FE analysis which does include out-of-plane stiffness in walls, the results may differ slightly.

Also note, in Ram SS, it is required to place a gravity beam in the gaps to prevent a framing tables error.

 

With RAM Frame, an option is available to assign Wall Group Numbers to multiple walls. If a  wall group is assigned to all four walls in either Case 1 or 2, the reported wall group forces will be the same. The total shear on the wall group is 100k, and the total overturning moment is 1000k’ as expected. It's important to note that assigning wall groups does not change any of the behavior, member forces, etc.

This example outlines above is the simplest case, but the same general principals apply no matter how the walls connect. Walls that intersect like an “L” or “T” also interact in a 3-dimension fashion. The story height and relationship between the walls of one floor and another also have a significant impact on the force distribution.

Lintel Beams

There are 2 approaches for modeling lintels beams in walls. The first approach is to model the whole wall and then place an opening in the wall. The second approach is to model walls on each side of the opening, and then span across the opening with a beam.

Wall with opening

When a wall opening is used the area above the opening is meshed along with the rest of the wall using shell elements and using the mesh parameters set under Criteria - General. The beam is assigned the same properties and cracked section factors as the rest of the wall.

Lintel beams of this type can be designed as Coupling Beams in the Ram Concrete Shear wall Module only, though you can cut sections through the beam to get forces at specific sections.

Generally speaking this approach gives you the stiffest overall wall compared to other methods. For that reason it's preferred for beams that are fairly stout, i.e. when the depth of the beam is > 1/4 the span.

Beam between walls

When modeling the lintel as a beam, the linear finite element of the beam connects to the corner nodes of the wall only. Consequently, the total stiffness of two walls coupled with a beam is less than the method above. (For RAM SS version 14.06, a modification to the analysis options is being implemented so that a small rigid end zone is created to provide greater resistance to rotation at this node.)

Beams modeled this way can be designed in the Ram Concrete Beam module only, though forces are reported the same as other frame beams.

Generally speaking, this approach is recommended for long and skinny beams between walls, e.g. when the beam depth is < 1/4 of the span.

Note, a two-way slab between walls can also couple walls together in a similar fashion. A rigid diaphragm will tie walls together and can provide for shear force transfer from one wall to another, but a rigid diaphragm alone does not actually couple the walls together.

Combining Columns and Walls

In the Modeler, you can freely model a column at the end of any wall without warning.

Where a column pilaster like this is modeled it's important to note that:

  1. The full self weight of both will be counted.
  2. If the columns and wall are lateral, then they will be meshed together and act compositely in Ram Frame (this is also true of gravity members analyzed in Ram Concrete.)
  3. The design of the wall is based on the forces in the wall only, while the design of the column is based on the forces in the column only.
  4. Where boundary element design is intended, it is better to model using walls only.

The presence of pilasters inside shear wall systems introduces a much different distribution of loads that has to be looked at closely.  In the Figure below, P1, P2, P3, P4, P5, P7, P9 and P11 represent the axial loads in the columns whereas P6, P8 and P10 represent axial loads in walls 1, 2 and 3 respectively. R1, R2, R3 and R4 are the external reactions. 

 Axial forces in Walls with Pilasters

 

A finite element analysis of the wall system shown in the figure above will give axial loads P5, P7, P9 and P11 which are much smaller than P1, P2, P3 and P4 respectively, because these loads are transferred not only to the columns also to the shear walls below.  In fact, the shear walls will often take most of the load leaving the column pilasters with very small internal forces. Many engineers want the pilasters to be designed for at least the loads that come directly from the columns above. There is no single tool to accomplish this in the program, so we recommend hand-checking that the pilaster below has at least the same size and area of reinforcement as the column above.

The frame reactions are the total reaction at a node. These reactions include the forces from the columns and the walls supported. For this system shown, the sum of R1-R4 is equal to the sum of column loads P1-P4, but forces will be distributed differently due to the presence of the walls.

It is worth noting that the walls themselves are further subdvided into a Finite Element mesh and if you prefer to view the individual nodal reactions, rather than the wall net reactions, use Process - Results - Reactions and toggle on the option to "Show Reactions at All Nodes"

  


Walls on Beams

When a wall is being supported by a beam, it is important to understand the way forces are transferred through the walls and into the supporting structure.

Gravity Walls


Starting in version 10 of RAM Structural System, gravity walls can be used to transfer loads from level to level.

When using Ram Steel analysis methods, any load is applied to the top of a gravity wall, that load is transferred straight down to the supporting member below (another wall or a beam for example). The applied loads are not fanned out or redistributed in any way.

This simplistic approach works nicely for simple bearing walls.

When using Ram Concrete analysis, the gravity members are part of the finite element analysis and the behavior is similar to that of lateral walls described below.

Lateral Walls


Loads are tracked down through lateral through finite element analysis in RAM Frame (or RAM Concrete).

A frame wall is a shell element capable of spanning from support-to-support. If a frame wall on an upper level is supported by frame columns on a lower level, then that wall is able to span from column to column like a very deep beam. Consequently, if a beam is modeled on the lower level from column to column as well, that beam will not be directly loaded by the wall. Think of it like a small flange welded to the bottom of a very deep plate.

Bending forces in the beam still occur because the wall is meshed (based on the settings under Criteria - General) and bending deformation of the whole system is still possible. Axial tension under gravity load is expected, though a rigid diaphragm or stiff two-way slab would inhibit those forces as well.

To reiterate, the forces within a frame wall from the RAM Frame analysis are not delivered to the supporting beam in the form of an external line load. The only external loads shown on the Report - Gravity Loads are:

  1. member self weight
  2. line loads applied directly to the beam
  3. the loads applied to the deck supported by the beam
  4. reactions of gravity members supported by the beam

If the supporting beam is longer than the wall above, then the beam still acts like a flange but we can expect sudden increases in the shear and moment beyond the end of the wall.

Here the program creates additional nodes on the beam where the two finite elements are connected together and alone the length of the wall based on the mesh criteria. As the wall is vertically loaded, assuming everything is symmetric, the basic deformed shape of the beam will now look like a trapezoid (although the true deformed shape is actually a continuous curve and not “kinked”). Nodes N2 and N3 remain level and the same distance apart, thus there will be large shear forces and moments in the end segments of the beam, at the face of the wall. If the wall is broken up into smaller elements, then there will be additional nodes between N2 and N3. In this case, there can be relative displacement between the ends of the wall, but the deformed shape will still be basically the same when the wall is stiff in comparison to the beam.

 

Behavior of a Wall Supported by a Beam – Centered

For situations where the wall is not centered upon the beam, or where the system is otherwise asymmetric, the situation is further complicated. Where the beam supports one end of the wall, significant vertical displacements can be expected, as opposed to the column support which is presumably much stiffer. A net rotation of the wall results throwing shear and overturning moments into that wall and the supported structure. When a rigid diaphragm is present, other frames may even experience lateral shear due to this rotation.

 

 

Behavior of a Wall Supported by a Beam - Off Center

If there is another level of framing or a rigid diaphragm at the top of the wall, that could limit the rotation and affect the forces throughout the whole system as well.

Special Considerations for Ram Concrete Analysis

As noted in the Analysis Types wiki, Ram Concrete Analysis is also a finite element analysis, but it works by analyzing one floor at a time. Consequently some of the complex multi-story, truss like effects from having multiple levels of walls transferred on one slab with not be captured by the Ram Concrete analysis.

RAM Concrete Analysis has a useful analysis option for ignoring the stiffness of walls that are supported by beams below (see discussion in previous section). Check the box for "Ignore Wall Stiffness on Above Story" in RAM Concrete - Concrete Analysis mode - Criteria - General to minimize the deep beam effect of walls above. For the design of frame beams and columns, choose to use the gravity forces from the RAM Concrete Analysis and not the RAM Frame Analysis. This is an option in the Criteria pull down menu in both RAM Concrete Beam and RAM Concrete Column.

 

See Also

RAM SS Analysis Types

RAM SS - Rigid Diaphragm Constraints and Frame Shear [TN]

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: RAM Structural System, WALLS

STAAD.Pro Postprocessing [FAQ]

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 12/20/2013 8:14:03 PM

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

 

 

 

 

 

 

 

 

  1. How do I display the deflection diagram and the displacement values on that diagram?
  2. After running the analysis, I go to the View menu, select Tables | Node Displacements, and select the load cases for which I want to see the values. The values are displayed in inch units. I want them in "cms" units. Changing the units using Tools | Set Current Unit doesn't seem to make a difference.
  3. I want to print out a picture which consists of a truss I have modeled with the STAAD. I want the output forces labeled right on each member. This is very similar to what would be put on to a plan sheet. Can STAAD do this or must I print out a report to get these forces?
  4. When I annotate beam moments on my diagrams, I can't seem to 1) change the font by adjusting the Beam Labels option and 2) turn off the unit being written on every single number.
  5. Why are my annotations for maximum bending moment or shear values not showing up in the post-processing mode?
  6. If I have a moment vector along the local positive Z axis does it have a twisting action going to the right along the positive direction of the axis?
  7. What are the sign conventions for moments in a 3-D structure?
  8. After performing the analysis, I enter the post-processing mode to view the member end force values. I click on the Beam page on the left side of the screen and see the values listed on the tables on the right hand side. Unfortunately, the moment values are in kip-inch units, even though my current units are set to feet and pounds. What do I have to do to get the values to show up in pound-feet units in the tables?
  9. What is the purpose of the Beam - Graphs page on the left side of the screen?
  10. How do I display the bending moment diagram and the values on that diagram, or shear forces or Axial forces?
  11. When I take a picture, it prints on the top half of a 8-1/2 x 11 size page. How can I take pictures that fill the page?
  12. How to insert a company logo into STAAD.Pro report?
  13. Can I get STAAD.Pro to report the torsion stress ?
  14. How can I have STAAD report more than 3 places of decimal in the post processing result tables?
  15. How to know the version of the design code which is being used by STAAD.Pro during the analysis?
  16. How to see the displacement of only one particular node graphically?
  17. What is the difference between the local and global deflection in the member query box?
  18. I am analyzing a large 3D structure. I changed the beta angle of one of the members to 90. I expected the MY and MZ for the two scenarios ( beta =0 and beta=90) to get interchanged. However that does not seem to happen. Why ?

 

1. How do I display the deflection diagram and the displacement values on that diagram?

The first step to viewing these results is to perform the analysis of the model successfully. Select Analyze from the Staad.Pro top menu bar followed by the Analysis option.

A dialog box by the name Select Analysis Engine will appear. Click on the Run Analysis button of this dialog box. After the analysis of the file is completed, click on the Done button.

The next step is to go to the Post Processing mode to view the deflection values graphically. To enter into the Post Processing mode, select Mode from the top menu bar and select Post Processing. Remember that if your analysis is not successfully completed (for reasons such as errors in your input data), you will not be able to access the Post Processing mode.

By default, the deflection diagram always opens up in the post processing screen of Staad.Pro.

From the top menu bar, choose Results - View value. Under Ranges, choose All. (The All button means the deflection diagram will be annotated for all nodes.)

Under the Node tab, you will see the options Global X, Global Y, Global Z and Resultant. Make the appropriate choice. Click on the Annotate button. Then click on the close button.

If you would like to see the diagram annotated for a different load case, select that load case from the load selection box.

2. After running the analysis, I go to the View menu, select Tables | Node Displacements, and select the load cases for which I want to see the values. The values are displayed in inch units. I want them in "cms" units. Changing the units using Tools | Set Current Unit doesn't seem to make a difference.

The unit system in which results are displayed on the tables is set using the facilities available under the View - Options menu. These are known as the display units. To set the display units for the node displacements, please do the following :

In the View menu, select Options - Structure units. In the category called Displacement, select the units you desire and click on OK.

3. I want to print out a picture which consists of a truss I have modeled with the STAAD. I want the output forces labeled right on each member. This is very similar to what would be put on to a plan sheet. Can STAAD do this or must I print out a report to get these forces?

First, you have to ask STAAD to Annotate the drawing with the axial forces. For this, please go to the post processing mode after you have analyzed the structure.

Click on the "Beam" tab on the left side and then click on the sub-tab labeled "Forces."

Click the right mouse button on the screen and select "Structure Diagrams."

From the "Loads and Results" tab, click on "Axial" under the "Beam Forces" heading.

Uncheck the "bending zz" box and click "Apply" followed by "OK."

Maximize the screen and then go to the "Results" pull down menu and select "View Value..."

Click on the "Beam Results" tab and then check the box under the "Axial" heading labeled "Ends."

Click "Annotate" and then "Close."

The axial loading values should be displayed on your screen.

4. When I annotate beam moments on my diagrams, I can't seem to 1) change the font by adjusting the Beam Labels option and 2) turn off the unit being written on every single number.

Annotation labels, although applied to beams, nodes, plates and solids, are not altered by the associated options (i.e View | Options | Beam Labels). In order to change the display of the annotations, go to View | Options from the main menu and choose the Annotation tab. To remove the display of the units for each annotation, simply choose the option "123.4" instead of "123.4 kN" under the Style list box in the Annotation tab. This will write the unit in the bottom right-hand corner of the screen for force, length and moment. If the units are not shown, go to View | Structure Diagrams and choose the Labels tab. Check on the option "Show Diagram Info" under the General box.

5. Why are my annotations for maximum bending moment or shear values not showing up in the post-processing mode?

In order to see the annotation (from Results->View Value in the post-processing mode) for a particular force or moment, the corresponding diagram must be on. For example, if one was to select maximum bending under the Beam Results tab, the bending moment diagram must be on (either MX, MY and/or MZ). Also, under the Ranges tab, make sure that the "None" option is not selected. Obviously, this would not annotate anything if it were selected. As a final note, once the annotations are visible, the size and font can be changed from the Annotation tab under View->Options in the main menu.

6. If I have a moment vector along the local positive Z axis does it have a twisting action going to the right along the positive direction of the axis?

If a member is drawn with its longitudinal axis (local-X) from left to right, and the local Z axis coming out of the page towards you, a positive MZ would cause tension on the top fiber, and a negative MZ would cause tension on the bottom fiber.

7. What are the sign conventions for moments in a 3-D structure?

The sign conventions are as follows:

Axial (FX) : Positive = Along local X axis, Negative = Opposite to local X
axis
Shear-Y (FY) : Positive = Along local Y axis, Negative = Opposite to local Y
axis
Shear-Z (FZ) : Positive = Along local Z axis, Negative = Opposite to local Z
axis

Torsion (MX) : Positive = Along local X axis, Negative = Opposite to local X
axis
Moment-Y (MY) : Positive = Along local Y axis, Negative = Opposite to local
Y axis
Moment-Z (MZ) : Positive = Along local Z axis, Negative = Opposite to local
Z axis

For axial forces,

Positive at the start node indicates compression at the start node.
Positive at the end node indicates tension at the end node.

Negative at the start node indicates tension at the start node.
Negative at the end node indicates compression at the end node.

8. After performing the analysis, I enter the post-processing mode to view the member end force values. I click on the Beam page on the left side of the screen and see the values listed on the tables on the right hand side. Unfortunately, the moment values are in kip-inch units, even though my current units are set to feet and pounds. What do I have to do to get the values to show up in pound-feet units in the tables?

The unit system in which results are displayed on the tables is set using the facilities available under the View - Options menu. These are known as the display units. To set the display units for the bending moments and torsional moments, please do the following :

In the View menu, select Options - Force units. In the category called Moment, select the units you desire and click on OK.

9. What is the purpose of the Beam - Graphs page on the left side of the screen?

This is another way to display the bending, shear and axial force diagrams on the screen.

In the post processing mode, select the Beam page from the left side of the screen. Then select graphs.

The right side portion of the screen will display the Bending diagram (MZ), shear diagram (FY) and the axial force diagram (FX) with values. In the drawing area, if you select a member by clicking on it, MZ, FY and FX of
that member will be displayed on the right hand side. To display the diagrams of another member, select that member.

10. How do I display the bending moment diagram and the values on that diagram, or shear forces or Axial forces?

First you must Analyze the file. Select Analyze from the Staad.Pro top menu bar. Select the Analysis option. After this, click on Run Analysis at the bottom of the small window dialog box.

After the analysis of the file is completed, click on the Done button.

Next, we go to the Post Processing mode to view the forces and results graphically.

To enter into the Post Processing mode, select Mode from the top menu bar and select Post Processing. Remember that if your analysis is not complete, you will not be able to access the Post Processing mode.

By default, the deflection diagram always opens up in the post processing screen of Staad.Pro.

To view the Bending Moment Diagrams, select the Beam page from the left side. From the top menu bar, choose Results - View value. Under Ranges, choose All. (The All button means the Bending moment diagram will be displayed for all members.)

Under the Beam Results tab, you will see the options Bending, Shear, Axial, Displacement and Stresses.
Make the appropriate choice.

Click on the Annotate button. Then click on the close button.

11. When I take a picture, it prints on the top half of a 8-1/2 x 11 size page. How can I take pictures that fill the page? 

There is no direct way to change the size of the picture from within STAAD.Pro. However here are a few options that you may find useful

Option 1

  1. Before taking a picture, please ensure that the model is
    zoomed in sufficiently so that it fills up the space within the picture border as far as possible.
  2. Take the picture and include that as part of the report using the Report Setup.
  3. Go to File > Printer Setup and change the orientation to Landscape.
  4. Go to File > Print Preview Report to check whether it looks satisfactory or not and if so, print it.


Option 2

  1. You may copy the picture by going to the menu option Edit > Copy Picture. You can then paste the picture in MSWord or Excel or Paint.
  2. Adjust the size of the picture using the tools available within these applications and take a print from there.

 

12. How to insert a company logo into STAAD.Pro report?

1. Open the start-up window of STAAD.Pro and go to the Configuration option.

2. Choose “File Options” tab and tick the “Remove Bentley Logo from Report” box. This will remove the Bentley logo    from your reports

3. Open the STAAD.Pro file. Go to the Report setup page and click on “Name and Logo” option.

4. Go to file option and choose the path where you have stored your logo. The logo should be in .bmp format.

5. Write the company name. You can orient the logo and company name by the Alignment option.

 

Note, Ram Elements, Connection and Ram Structural System have similar options. For Elements or Connection go to the upper left menu - General Configuration - Print tab. For RAM Structural System you just have to replace the logo.bmp file in the program directory with your own logo.bmp or logo.jpg file. it tends to work best when the log has roughly a 1:1 aspect ratio.

13. Can I get STAAD.Pro to report the torsion stress ?

STAAD.Pro does not report stress due to Torsion but here are a couple of items which you may find useful.

The beam end forces table that you can get from Postprocessing mode Beam > Forces page, reports the torsion ( MX ) in a beam member.

STAAD is also able to account for stresses due to torsion during the design phase. In steel design for example, the torsion stresses are converted to normal and shear stresses and added to existing normal/shear stresses following guidelines laid out in AISC Design Guide 9. When it comes to the new AISC 360-10 code, currently the software can account for the torsion for HSS sections only although work is under progress to account for torsion for Non-HSS sections too and this should be available in a couple of months. 

14.How can I have STAAD report more than 3 places of decimal in the post processing result tables?

You need to go to the top menu and click on View > Options > Choose the appropriate item and change the corresponding number of decimal places as desired > Click Apply > OK.

15. How to know the version of the design code which is being used by STAAD.Pro during the analysis?

The design code version which is being used by STAAD.Pro during the design phase is written in the Output file

16. How to see the displacement of only one particular node graphically?

1. Analyze the model and go to the Postprocessing mode, Node -> Displacements page.
2. If needed, turn on the node symbol (click Shift + K on your keyboard) and node numbers (Shift + N).
3. Go to the Results -> View Value menu.
4. In the Ranges tab select Ranges and enter the node number(s) for which you want to see the displacement.


5. Then go to the Node tab and select Nodal Displacement which you want to see. Click Annotate.

Now the displacement of only selected node will be seen on the screen. Similarly, beam force diagram values, beam maximum displacements, beam combined stresses and support reactions can be set.

17. What is the difference between the local and global deflection in the member query box?

Figures (1) and (2) show the local and global deflections of the beam #2 which is a part of the beam joining 2 columns:

Figure (1) 

Figure (2)

Global deflection is the largest distance between (a) and (b) where:

(a) is the line joining the ends of the member in its un-deflected position (named as 'Original shape' in the figure (3));

(b) is the elastic curve of the member representing its deflected shape.

 

Local deflection is the largest distance between (c) and (d) where:

(c) is the line joining the ends of the member in its deflected position;

(d) is the elastic curve of the member representing its deflected shape.

Figure (3)

18. I am analyzing a large 3D structure. I changed the beta angle of one of the members to 90. I expected the MY and MZ for the two scenarios ( beta =0 and beta=90) to get interchanged. However that does not seem to happen. Why ?

The Mz and My would not simply get interchanged when you apply a beta angle to 90 for every situation. The same would be true if you are analyzing a beam in isolation without considering any effect from the rest of the structure. However when a beam is part of a bigger structure, the beam’s local stiffness in each direction would affect the global stiffness of the structure along each DOF. Depending on that there will be a redistribution of the forces which will result in different moments/shears.

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: FAQs, SELECTservices, STAADPro, Result Diagram

RAM Concept Reinforcement [FAQ]

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 12/20/2013 11:43:48 PM

  
 Applies To 
  
 Product(s):RAM Concept
 Version(s):Any
 Environment: N/A
 Area: N/A
 Subarea: N/A
 Original Author:Bentley Technical Support Group
  

 

 

 

 

 

 

 

 

How can I display the code provision that governs the design of program reinforcement?

The code controlling provision can be displayed on screen for all cross sections on any reinforcement plan on the Design Status or Rule Set Design Layer. To view the controlling criteria:

  1. Open a reinforcement plan on Layers - Design Status or Layers - Rule Set Designs.
  2. Open the Visible Objects dialog. This can be done by clicking on the visible objects dialog or clicking on
    View - Visible Objects or right clicking within the active plan window and choosing
    Visible Objects.
  3. In the Visible Objects dialog, check the box for Controlling Criteria.
  4. Click OK to close the dialog. The governing code provision will display on screen.

In some cases, "Det" will display before the code provision. This means that the reinforcement is not explicitly required at that cross section but is extended into the section to satisfy another code rule. Typically, this is associated with span detailing requirements.

 

How do I model user reinforcement?

See Chapter 25 “Drawing Reinforcement Bars” in the RAM Concept Manual for more information. There are two main types of user reinforcement: concentrated reinforcement and distributed reinforcement. Concentrated reinforcement is a fixed number of bars over a parallelogram area. This type of reinforcement is convenient for modeling beam reinforcement. Distributed reinforcement is a bar spacing applied over a polygon area. This type of reinforcement is convenient for modeling layers of reinforcement over a portion or the entire slab area.

There are six tool buttons that can be used to model the reinforcement:

  • Concentrated Reinf. (Click at Bar End Points)

  • Concentrated Reinf. (Click at Center Point and an End Point)

  • Concentrated Reinf.  Cross (Click at Cross Point and an End Point)

  • Distributed Reinf. (Click along Region Boundary)

  • Distributed Reinf. in Perimeter (Click at Bar End Points)

  • Distributed Reinf. Cross in Perimeter (Click at Cross Point and an End Point)

The “Cross” tools are convenient for defining the reinforcement in both directions. The “Distributed Reinf. in Perimeter” tools are convenient for modeling reinforcement over the entire slab area.

The bar elevation is referenced from the center of the reinforcement segment. When defining reinforcement over an area with slab and beams or slabs with drop panels, make sure that this point is in the correct area. For example, if the reinforcement shown in the screenshot below is referenced to the drop panel and not the typical slab as was intended.

I am modeling an existing slab. Can I prevent the program from adding program reinforcement?

Go to Criteria – Calc Options and check the box for “Check capacity of user reinforcement without designing additional program reinforcement.”

When this is done, program reinforcement will not be added, and cross sections that do not satisfy the code requirements are shown as failing. Some users like to plot the bending moment demand and capacity diagrams at this point to see how badly the failure it, though of course there are other possible failures besides bending.

If user reinforcement has been provided and you are confident that it satisfies the code minimum requirements, you can also turn off the Code Minimum design rule completely under Criteria - Design Rules, though we do not generally recommend this practice.

What is the significance of defining the reinforcement “Slab Face”: Top, Bottom, or Both?

Slab face controls on what plan the reinforcement is displayed. By default, reinforcement defined as “Top” and “Both” are displayed on the top reinforcement plans; reinforcement defined as “Bottom” and “Both” are displayed on the bottom reinforcement plans.

The Slab Face also affects the way the reinforcement is used in the Code Minimum Check and Span Detailing. Options for the “Code Minimum Reinforcement Location” include Elevated Slab, Mat Foundation, Top, and Bottom. Each of these options is based on where the reinforcement is placed (top of slab versus bottom of slab). Span detailing extends top and bottom reinforcement to a certain percentage of the span length (see ACI 318-08 Fig 13.3.8 for an example of a span detailing rule). If "Both" is selected for the Slab Face, then the reinforcement will be extended to meet both top and bottom reinforcing requirements.

For mat foundations, the ACI code (R15.10.4) permits the minimum reinforcing steel to be split between the top and bottom faces. If "Both" is selected for the Slab Face, then the program will use both layers in the minimum reinforcement check.

Can I design a slab with one layer of reinforcement?

Program reinforcement is always detailed in two layers: top and bottom. Slabs with one layer of reinforcement can be modeled and designed using user reinforcement as follows:

  1. Model user reinforcement in the slab. Set the Elevation Reference and the Elevation so that the reinforcement is in the correct location. Set the Slab Face to “Both.” This will force the program to use the reinforcement in the code minimum check at each cross section.
  2. In Criteria – Calc Options, check the box for “Check capacity of user reinforcement without designing additional program reinforcement.” This will prevent the program from adding program reinforcement at the top and bottom face.
  3. Run the analysis.
  4. Check the Design Status for failures.
  5. If needed, make changes to reinforcement size and spacing.
  6. Re-run the analysis.
  7. Repeat Steps 4 through 7 as needed.

How can I change the format of reinforcement on the Reinforcement Layer?

By default, program reinforcement is displayed showing bar quantity, bar size, length, and bar face. The format can be modified to include other information, like bar spacing, by doing the following:

  1. Select the reinforcement on a plan on Layers – Reinforcement.
  2. Click on Edit – Selection Properties. A dialog showing the bar information will display.
  3. In the dialog, click on the Presentation tab.
  4. Change the key value in the “Callout By Quantity Format.” See key and screenshot below:

$Q - Bar quantity       

$F - Bar face

$B - Bar name

$L - Bar length

$U - Bar length units

$u - Bar spacing units

$S - Bar spacing

\n - Start new line

 

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: RAM Concept, Reinforced Concrete, reinforcing

Slenderness Check of Laterally unsupported ISMB section

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Current Revision posted to Structural Analysis and Design - Wiki by Suro on 1/3/2014 6:12:12 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Wiki
 Subarea: Design
 Original Author:Surojit Ghosh
  

 

 

 

 

 

 

 

 

STAAD.Pro Model 

Relevant STAAD.Pro model (.std file) can be downloaded from the following link:

STAAD.Pro model for IS 800:2007 verification example

Critical Design Forces

For Sectional Properties and Critical design forces, go through the following post:

Section Classification of Laterally unsupported ISMB section

Slenderness Check

STAAD.Pro Design Output


 

Tension Capacity Check of Laterally unsupported ISMB section


Compression Capacity check of Laterally unsupported ISMB section

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Current Revision posted to Structural Analysis and Design - Wiki by Suro on 1/3/2014 9:09:18 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Wiki
 Subarea: Design
 Original Author:Surojit Ghosh
  

 

 

 

 

 

 

 

 

STAAD.Pro Model

Relevant STAAD.Pro model (.std file) can be downloaded from the following link:

STAAD.Pro model for IS 800:2007 verification example

Critical Design Forces

For Sectional Properties and Critical design forces, go through the following post:

Section Classification of Laterally unsupported ISMB section

Compression Capacity Check

STAAD.Pro Design Output


IS 800:2007

Shear Capacity Check of Laterally unsupported ISMB section

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Current Revision posted to Structural Analysis and Design - Wiki by Suro on 1/3/2014 9:26:53 AM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):All
 Environment: N/A
 Area: STAAD.Pro Wiki
 Subarea: Design
 Original Author:Surojit Ghosh
  

 

 

 

 

 

 

 

 

STAAD.Pro Model

Relevant STAAD.Pro model (.std file) can be downloaded from the following link:

STAAD.Pro model for IS 800:2007 verification example

Critical Design Forces

For Sectional Properties and Critical design forces, go through the following post:

Section Classification of Laterally unsupported ISMB section

Shear Capacity Check 

STAAD.Pro Design Output


Bentley Structural Dashboard

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Current Revision posted to Structural Analysis and Design - Wiki by jeremyhoesly on 1/3/2014 10:19:32 PM

How do I stop the Structural Dashboard from appearing?

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Revision 1 posted to Structural Analysis and Design - Wiki by jeremyhoesly on 1/3/2014 10:19:33 PM

  
 Applies To 
  
 Product(s):Bentley Structural Dashboard
 Version(s):N/A
 Environment: N/A
 Area: N/A
 Subarea: N/A
 Original Author:Jeremy Hoesly, Bentley Technical Support Group
  

 

 

 

 

 

 

 

 

XXXXXXX(Describe the task to be accomplished.)XXXXXXX

Background

XXXXXXX(If applicable, provide any other information the user needs before starting the steps; otherwise, delete this section.)XXXXXXX

Steps to Accomplish

Option 1 XXXX(Delete this heading if only one option exists.)XXXX

  1. XXXXXXX
  2. XXXXXXX(add more steps as needed)XXXXXXX

Option 2 XXXX(Delete this section if only one option exists.)XXXX

  1. XXXXXXX
  2. XXXXXXX(add more steps as needed)XXXXXX

See Also

XXXXXXX(Add links as needed for other relevant Be Communities content.)XXXXXXX

Tags: Bentley Structural Dashboard, how to, SELECTsupport

RAM SS - Center of Rigidity

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/3/2014 11:36:04 PM

  
 Applies To 
  
 Product(s):RAM Structural System
 Version(s):Any
 Environment: N/A
 Area: Analysis
 Subarea: N/A
 Original Author:
  

 

 

 

 

 

 

 

 

Center of Rigidity

In order to review the center of rigidity for a structure, a special Centers of Rigidity load case must be created under Loads – Load cases in RAM Frame. Once the analysis of that load case has been performed, a “Centers of Rigidity” report becomes available under the reports menu.

The Centers of Rigidity report lists the centers of rigidity of each diaphragm at each of the levels that contain lateral members. The report also lists the center of mass and Story Lateral Stiffness of each diaphragm.

The center of rigidity can be thought of as the location through which a lateral load would cause lateral deformation of the diaphragm without causing rotation. The concept is analogous to that of a cross section’s “shear center”.

Below are the results for a 30’x10’ structure, 10 stories tall, with walls on 3 sides.

 

Isometric view of “C” shaped wall model, center of mass at (15,5)

For buildings with torsional irregularity, the lateral load may always be on the same side of the center of rigidity even after considering a 5% accidental eccentricity of the load. In this case, the torsion will always be “adding” to the shear on one side of the building and “subtracting” shear from the other side. To ignore these effects, an additional lateral load case with the same magnitude as the generated load, but with a location exactly at the center of rigidity can be added. This, pure shear load case, can then be included in the load combos to yield a conservative design for the frame elements that otherwise would benefit from the eccentricity. Some codes may require such a conservative approach, but most building codes recognize the reality of the eccentricity and the effect it has on the structure. In those cases, the code may simply want an increase in the accidental torsion to be considered. This can be changed under Loads – Masses, within the Analysis mode of RAM Frame.

Returning to the example above, an interesting phenomenon occurs in regard to the “Yr” location. Even though the levels are identical, the center of rigidity shifts from level to level. The higher the level, the more eccentric the center of rigidity. In other words, a load must be applied from the long wall in order to bend the channel without twisting it.

A load applied to the diaphragm in line with the long wall (y=10’), actually produces a large diaphragm rotation. For a load applied to the center of the diaphragm (y=5’) the effect is even worse

 

Channel Loaded Through Center of Rigidity

Channel Loaded Through Long Wall

 

The Center of Rigidity location is not directly used in determining the loads or in the finite element analysis. The exception to this rule is in the determination of some wind loads where the eccentricity affects the applied loads directly.

The center of rigidity is always calculated using a rigid diaphragm analysis, even where semi rigid or flexible diaphragms are called out.

 

 

See Also

RAM SS Walls FAQ

Structural Product TechNotes And FAQs

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: RAM Frame, RAM Structural System, SELECTsupport

Structural Analysis and Design - Wiki

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:09:28 AM

Check out the Structural Analysis and Design TechNotes And FAQs and the Structural Drafting and Detailing TechNotes and FAQs

Structural Analysis and Design products

STAAD Products

RAM Products

[[STAAD.Pro]]

[[STAAD.foundation]]

[[OpenSTAAD]]

[[STAAD Foundation Advanced]]

[[STAAD.offshore]]

[[STAAD(X) Tower]]

[[STAAD(X)]]

[[RAM Structural System]]

RAM Revit® Link

[[RAM Concept]]

[[RAM Elements]]

[[RAM Connection]]

[[RAM SBeam V5.0]]

Other Products

[[SACS]]

ISM (Integrated Structural Modeling)

See Also

Resources

Tags: structural design, Structural Analysis

Structural Integration

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:11:36 AM

What is the Structural Dashboard V8i?

  

 Click Here to view the Dashboard and Structural Synchronizer Launch Video  

 

Download Structural Dashboard from iWare Apps.

The Dashboard is a free tool that assists in managing the data and workflow of projects from start to finish.

The Dashboard provides a Web Portal and Launch Pad to learn how Bentley's comprehensive products integrate in more efficient project workflows.

Download Here

Structural Dashboard V8i

 

Structural RSS News

Project folders/ files

Project notes & dynamic links

Built-in web links

Check for product updates
 

 

Benefits of the Structural Dashboard

The Structural Dashboard is a free tool that assists in managing the data and workflow of projects from start to finish. The Structural Dashboard provides a single interface to utilize Bentley's integrated products for a complete project workflow.

  • Manage workflows for common project type (including building workflows and plant workflows)
  • Use a unified interface to launch all your Structural applications
  • Create customized workflows specific to your projects
  • Receive Structural News from customizable RSS feeds
  • Join Structural online community and access blogs, wikis and forums
  • Download product upgrades from Bentley's SELECTservices Center
  • Manage project files and links within your workflow
  • Consolidate common project information and dynamic links to project documents

Integrating Structural Workflows

The ability to integrate structural project workflows - including modeling, analysis, design, documentation and detailing - enables structural engineers, detailers and fabricators to dramatically increase project efficiency, reduce errors, and improve quality control.

Bentley's integrated structural modeling works behind the scenes to provide engineers with a shared and dynamic repository for all structural content including visualization and revision history for increased coordination.

Rollover the links below to see integration descriptions and click the links watch integration videos :

Building Workflow Examples

        

  1. RAM Structural System and RAM Concept
  2. RAM Connection and RAM Elements
  3. RAM Structural System and Structural Modeler
  4. RAM Structural System and RAM Concrete
  5. RAM Structural System and RAM Connection
  6. RAM Structural System and RAM Elements
  7. RAM Structural System and RAM Foundation
  8. RAM Structural System and RAM Steel
  9. RAM Structural System and RAM Frame
  10. RAM Elements and RAM Concept
  11. ProStructures and RAM Structural System
  12. ProStructures, RAM Elements and RAM Connection
  13. ProStructures and RAM Connection
RAM 3D Viewer

 

    Plant Workflow Examples

             

    1. AutoPIPE and AutoPLANT
    2. ProStructures and STAAD.pro
    3. STAAD.pro and AutoPIPE
    4. STAAD.pro and STAAD.foundation
    5. ProStructures, STAAD.pro and RAM Connection
    6. STAAD.pro and Advanced Analysis Module
    A plant structure in STAAD.pro

    More info...

    To learn more and connect with others interested in this topic please visit:

     

    Tags: Structural Dashboard, product description

    Curso por Bentley en Español de RAM Elements V.8i Fundamentos

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    Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:15:47 AM

    Tipo de Curso: Presencial en Español

    Productos a utilizar: Ram Elements V.8i 12.5

    Este curso es recomendado para: Diseñadores, Proyectistas; Diseñadores de Estructuras; Ingenieros Estructuristas, Ingenieros Mecánicos,  Técnicos de aplicación en Ingeniería Estructural y profesionales en general relacionados con el Diseño y la modelación de Estructuras.

    Descripción del Curso: En este curso, el participante aprende las bases para crear modelos tridimensionales con el uso de RAM Elements, se incluyen conceptos para generar miembros y nodos, asignar soportes y propiedades a los miembros, crear condiciones de carga y sus combinaciones; desarrollar el análisis, diseño y la optimización en una estructura; así como establecer el uso de los Módulos de Detallado en RAM Elements.

    Objetivos de Aprendizaje: Después de tomar este curso el participante será capaz de:

    • Modelar utilizando la interfaz gráfica para el usuario de RAM Elements
    • Generar nodos, miembros, áreas y placas en una estructura tridimensional
    • Generar condiciones de carga y sus combinaciones
    • Desarrollar el análisis, diseño o la optimización de una estructura usando RAM ElementsDesarrollar el análisis sísmico dinámico en RAM Elements
    • Utilizarlos Módulos de Detallado en conjunto con la aplicación o por separado

    Temas del Curso:

    • Generación del Modelo
    • Propiedades de los Elementos
    • Carga del Modelo
    • Análisis, Diseño y Optimización de Miembros
    • Análisis Sísmico Dinámico
    • Módulos de Detallado

    Prerrequisitos del Curso:   Conocimiento básico de Elementos de Estructuración y principios de Ingeniería Estructural

    Fechas:  De acuerdo a Cupo Minimo

    Material:  Oficial de Bentley Institute en Ingles

    Duración:

    Informes:

    8 horas

    rolando.valenzuela@bentley.com

    Tags: RAM Elements

    Seminarios y Cursos en Español de Productos Estructurales de Bentley 2012

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    Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:16:25 AM

    Seminarios y Cursos en Español de Productos Estructurales de Bentley 2012 by Edgar Garcia-Hernandez

    En horabuena, por fin cursos en Español y Seminarios por parte de Bentley Systems. Esta es la programacion tentativa:

    CALENDARIO DE ACTIVIDADES PRODUCTOS ESTRUCTURALES BENTLEY
    TIPODURACIONTEMAAÑO 2012
    ENEFEBMARABRMAYJUNJULAGOSEPOCTNOVDIC
    SEMINARIOS
    Gratuito1 hrDiseño Estructural Inteligente y Modelos de Aplicación1717
    1 hrTrucos y Tips de STAAD.Pro para el Diseño Estructural2726
    1 hrAplicación de Análisis Avanzado con STAAD.Pro2920
    1 hrDiseño Estructural Aplicado en Vivienda1929
    CURSOS
    Con Costo16 hrSTAAD.PRO Fundamentos21-2317-195-723-2511-13
    16 hrSTAAD.PRO Avanzado16-186-88-1026-2814-162-4
    8 hrRAM ELEMENTS FUNDAMENTOS143152615
    4 hrRAM CONNECTION FUNDAMENTALS3031
    6 hrSTAAD.FOUNDATION FUNDAMENTALS21
    CURSOS STAAD.Pro POR AREA DE INTERES
    Con Costo4 hrAdvanced Analysis Engine30
    4 hrBridge Applications including STAAD.beava30
    4 hrDynamics and Seismic Analysis3026
    4 hrGetting the Most Out of the Processor29
    4 hrLoads and Load Generators28
    4 hrReinforced Concrete Analysis and Design417
    4 hrSteel Analysis and Design17

    Cualquier pregunta con Rolando.Valenzuela@bentley.com

    Recuerden subir sus preguntas en español en nuestra comunidad:

    http://communities.bentley.com/communities/user_communities/usuarios_de_bentley_en_espanol_spanish_users/f/281895.aspx

    Tags: RAM Elements

    STAAD Offshore - Base Units

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    Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:18:27 AM

    Have updated to STAAd Offshore Version 3.0.0.9 and the Base Units are set to Imperial. On the old version i just changed the base units to Metric as seen below, but in this version the file "STAADlib.cfg" doesnt seem to exist.

    Version 2.0.6.1

    Open the OpenSTAAD configuration file in TextPad or NotePad:-

    C:\Program Files\Common Files\BentleyShared\IEG\OpenSTAADBentley\Data\STAADlib.cfg

    Change the BaseUnits command to:

    [BaseUnits]

    BaseUnit=Metric

    Tags: structural design, STAAD.Pro, structural analysis software, Structural Analysis, Offshore, STAAD

    ISM API

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    Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 1/4/2014 12:22:44 AM

    The Structural Synchronizer comes with an open API (application programming interface) that is free for anyone to use. Documentation, including sample code, is available upon request through a private Be Community. For access, please send a message to community member Seth Guthrie along with the details of the integration you are planning to write.

    See Also

    Structural Technotes and FAQs

    Integrated Structural Modeling Home

    Tags: API, Integrated Structural Model, product description, ISM
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