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RAM Structural System Release Notes

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Minimum reinforcement reporting

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Revision 1 posted to Structural Analysis and Design - Wiki by Sye on 4/16/2015 10:00:56 PM

Applies To
Product(s):STAAD Foundation Advanced
Version(s):ALL
Environment: ALL
Area: Gereral
Subarea: Rigid Foundation
Original Author:Sye Chakraborty, Bentley Technical Support Group

In an isolated footing design, STAAD.Foundation advanced reports the minimum reinforcement ratio to be less than the values specified by ACI 318 code. For example I am using the ACI 318 code and for 60 ksi steel, I would expect a minimum ratio of 0.0018 as per clause 7.12.2.1 but STAAD.foundation shows the min reinforcement ratio to be 0.0016. Why is that ?

 

STAAD.foundation Advanced does check the minimum reinforcement as per the ACI clause 7.12.2.1 but depending on a global setting, it can provide the minimum reinforcement such that

 

  1. The minimum reinforcement requirement is satisfied considering both top and bottom reinforcements or in other words the summation of the reinforcement required at the top and bottom should equal the minimum reinforcement required.

  2. The minimum reinforcement requirement is satisfied for each face individually in which case, at each face the min reinforcement ratio would be 0.0018.

     

If you go to Global Settings > Rigid foundation Settings > check the box which reads “Check Minimum Reinforcement based on top and bottom combined”, the software calculates the min reinforcement as per the point 1 above. So if there is a certain amount of reinforcement already provided at the top face, it would provide the remaining amount of steel ( for satisfying the minimum reinforcement requirement ) at the bottom face. In such cases you may see the min reinforcement ratio reported to be lesser than 0.0018 as this is for that particular face only and not for the entire cross section.

 

If the box is unchecked, the software calculates the min reinforcement as per the point 2 above. If you design with this setting, you would see 0.0018 being reported as minimum reinforcement required at a single face.

Tags: minimum reinforcement, min reinforcement, 7.12.2.1, ACI 318

Strength/Serviceability check in design

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/17/2015 5:45:47 PM

Applies To
Product(s):STAAD.Pro
Version(s):ALL
Environment: ALL
Area: Design
Subarea: AISC Code
Original Author:Sye Chakraborty, Bentley Technical Support Group

I am using AISC code. How can I have STAAD do deflection check for service cases and do strength check for ultimate cases ?

 

For AISC 360-10, the design routine can do deflection checks based on SERVICEABILITY LOAD ENVELOPES and strength checks based on STRENGTH LOAD ENVELOPES as part of the same design cycle. One needs to define serviceability envelope and strength envelope first consisting of the appropriate cases and then define a LOAD LIST ENV command  for the design to consider these as explained below.

 

For example if you have a strength load case 10 and a serviceability case 11, you can set up the design as shown next

DEFINE ENVELOPE

11 ENVELOPE 1 TYPE SERVICEABILITY

10 ENVELOPE 2 TYPE STRENGTH

END DEFINE ENVELOPE

LOAD LIST ENVELOPE 1 2

PARAMETER

CODE AISC UNIFIED 2010

METHOD ASD

*specify all design parameters here including DFF, DJ1, DJ2

CHECK CODE ALL

The software would then use the Load case 11 for deflection check and load case 10 for strength checks.

Tags: serviceability load envelope, strength load envelope, Serviceability, Deflection Check, strength and serviceability

Limitations of the curved beams in STAAD.Pro ( TN )

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/17/2015 6:26:56 PM

  
 Applies To 
  
 Product(s):STAAD.Pro
 Version(s):20.07.09.31
 Environment: N/A
 Area: Modeling
 Subarea: Curved Beams
 Original Author:Modestas Turulis, Bentley Technical Support Group
  

 

 

 

The following are some of the limitations or features not supported with curved members:
 
Tapered section properties
Composite decks
PRIS ROUND sections
Beta angle
Member releases, global or tangent
Member Springs
Member offsets
Member end springs
Physical members
Member Tension/compression
 
Any span loads except "Uniform load throughout the length in global directions", such as:
 
Member Loads - UMOM, CON, CMOM, LIN, TRAP
Area Load, One Way, Floor Load
Wind Load, Prestress, Poststress
Temperature load, Strain
Fixed End Load
Snow Load
Moving load
 
Imperfections
Geometric stiffness, Pdelta, buckling, Pdelta KG with/without dynamics
Mass for dynamics will not include the effect of the member cg being off the chord line
Intermediate section displacements, and hence the deflection diagram
Intermediate section forces, and hence the bending moment and other forces diagram

Steel or concrete design at any location other than nodes
Member selection
Weld design

*Limitations faced with curved beams in designing:

It is not advisable to perform steel design on curved members using STAAD. The reasons are :
 
1) The design codes are written for straight members, not curved ones. The rules in most standard design codes do not adequately address the peculiarities of curved members. LY and LZ for example in the KL/r checks are the straight line distances between the bracing points of a straight member. To use those rules on curved members without adjusting for the curvedness may not be correct. An out of plane load on a curved member causes major torsional moments, but most codes only discuss axial forces, bending and shear, not torsion.
 
2) STAAD can calculate the member forces only at the nodes of curved members. It cannot calculate them at intermediate span locations. Consequently, during steel design, these members will be designed for the forces at their ends only. Intermediate section points within the span cannot be designed.
 
3) STAAD can calculate the displacements at the nodes of curved members. It cannot calculate them at intermediate span locations. Consequently, deflection check cannot be performed for curved members.

Due to all  these limitations, modeling the curved beams using a series of straight segments might be a better option.

See Also

STAAD.Pro TechNotes and FAQs

Tags: curved beams, STAAD.Pro, Modeling, Curved

Using SJI Virtual Joist Girder Tables in the RAM Structural System

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Revision 1 posted to Structural Analysis and Design - Wiki by Allen Adams on 4/17/2015 7:27:04 PM

Introduction to Virtual Joist Girders

Steel joists are sometimes used in moment frames for wind and in regions where the seismic loads are small. While the steel joists themselves are often designed by the joist manufacturer, the structural response of the system must be investigated and the columns and footings designed by the structural engineer. This gets complicated when the exact properties of the joists are unknown at the time that the structural analysis and design are performed. To assist in this effort the Steel Joist Institute (SJI) has created a table of Virtual Joist Girders, a series of joist members with a wide range of stiffnesses and capacities. These can be assigned to the frames in the structural model, with the sizes refined to satisfy deflection, drift and strength requirements. Based on the properties of the selected Virtual Joist Girders, the requirements for the design of the actual joist girders can be determined and specified.

 

The properties of the Virtual Joist Girders are equivalent to an I-shaped structural steel member. In the analysis software these are treated as if they are I-shaped structural steel beams, hence the term ‘Virtual’.

 

The data in the Virtual Joist Girder table has been converted to a format suitable for use in the RAM Structural System. The data was provided by SJI, and formatted to conform to the table format requirements of the RAM Structural System. This includes both a Master Table and a Steel Beam Design Table. Bentley does not warrant the suitability or accuracy of the Virtual Joist Girder table. The engineer should understand the purpose of the table, the assumptions made in creating the table, the limitations of the use of the table, and should verify the results to his/her satisfaction. Refer to the documentation on the Virtual Joist Girders produced by SJI, currently available on their website at www.steeljoist.org. Technical questions on the SJI Virtual Joist Girder table or the designs produced should be directed to SJI.

 

It is the engineer’s responsibility to use these tables properly; no warnings are given by the program if they are assigned to the wrong type of members, or to members with unsuitable properties, or with the wrong Criteria selections. It may not be apparent from the designs produced that there was an error in these selections.

 

To use the Virtual Joist Girder tables in the RAM Structural System, the following process is recommended:

 

Tables

In RAM Manager select the Master Table containing the Virtual Joist Girders using the Criteria – Master Steel Table command. The table containing those sections is called ramaiscwithvjg.tab; it is identical to the AISC shapes table ramaisc.tab except it contains the additional Virtual Joist Girder sections.

 

Next, select the Design Steel Table containing the Virtual Joist Girders using the Criteria – Design Steel Tables command. Select the Beam tab. The table containing those sections is called ramvjg.bms; select that table as the Alternate beam design table:

 

 

Modeling

In RAM Modeler, model the joist girder as a Noncomposite Steel beam, with Fy = 50 ksi. Do not model it as a Steel Joist (that will use the program’s Joist Girder selection routines, not the special Virtual Joist Girder table). Note that if the beam is assigned to be a Composite beam the resulting design will be unconservatively incorrect.

 

 

Using the Layout – Beams – Steel Table command, assign the girder to Use Alternate Steel Table. In this model only joist girders or Frame beams should be assigned to use this alternate table.

 

 

For best results assign a Maximum Depth restriction using the Layout – Beams – Size Restriction command, otherwise the sizes selected may be excessively deep (the table has joists with depths ranging from 20” to 120”). Setting a Maximum Span/Depth Ratio in RAM Steel Beam may also be helpful, although that Criteria option affects all beams, not just the Virtual Joist Girders. SJI recommends that the depth be no greater than 1/12 of the span and no less than 1/24 of the span (span/depth ratios between 12 and 24, with the most economical between 12 and 18).

 

SJI recommends that the member be designed assuming an unbraced length of zero. This can be approximated by assigning very close brace points to the girder using the Layout – Beams – Brace Points command. Note that if the actual distance between brace points is less than the value of Lp calculated for the size being investigated, the design is the same as if unbraced length is zero. This means that brace point spacing of between 2’ and 4’ (or more) is likely to be sufficient. Alternatively, for Frame Beams investigated in RAM Frame Steel – Standard Provisions mode the Criteria – Flange Bracing command can be used to specify that the Top and Bottom Flange are Continuously Braced. Be careful with this approach, however, because that criteria will apply to all Frame beams, not just those that have been assigned to use the Virtual Joist Girder table.

 

 

Gravity Steel Joist Girders

Using the Virtual Joist Girder tables is not generally recommended for standard steel joist girders carrying only vertical gravity loads. Normally these should be modeled as Steel Joists and then the program will determine the label, such as for example 18G4N2.5k. For irregularly load girders the program will merely call out the girder as xxGSP, for which the engineer is expected to supply the girder loads to the joist manufacturer. However, if there are cases where specific joist properties are needed, these Virtual Joist Girder tables can be assigned to gravity beams, and designs obtained.

 

In RAM Steel Beam select the steel code using the Criteria – Steel Design Codes command.

The table is only valid for AISC 360-05 and AISC 360-10; no other design codes should be specified.

 

Perform Design All. Unless explicit sizes have been assigned, optimized sizes based on gravity loads will automatically be selected:

 

 

These size labels do not directly represent the final Joist Girder design. See Specifying Steel Joist Girders below for information on specifying Joist Girders.

 

If assigned to gravity members, Virtual Joist Girder sizes will be included in the Takeoff, but it should be noted that the weight listed for these sizes does not include the weight of the web members and miscellaneous materials. These add approximately an additional 15% to the total weight.

 

 

 

Steel Joist Girders as Frame Members

The most common application of these Virtual Joist Girders will be as steel joists in moment frames. Create the model as instructed above. If preliminary Virtual Joist Girder sizes have not yet been assigned to the Frame beams, do so using the Assign – Beam – Size command in RAM Frame.

 

 

Or if preferred use the Layout – Beams – Assign Size command in the Modeler, which functions similarly.

 

Note that the Virtual Joist Girder sizes are included in the listing of I-section sizes as explained previously. The first number in the label is the girder depth. The second number in the label is a series number and has no physical meaning, although higher numbers within the same depth mean heavier joists. For example, VJG24-45 is 24” and is the 45th entry in the 24” girder series.

 

Note: In the 3D view, these Virtual Joist Girders will be displayed as Steel Beams, they will not be displayed as Steel Joists.

 

Analyze the frames. Verify that the drifts are acceptable; if not, assign larger Virtual Joist Girder sizes using the Assign Size command. Repeat until the drifts are acceptable.

 

After the drift requirements have been satisfied, the next step is to verify that the Virtual Joist Girder has adequate strength. To do this, go to the Steel – Standard module. For the steel design code select AISC 360-05 or AISC 360-10, ASD or LRFD. None of the other codes should be selected, as they may not produce correct results for these Virtual Joist Girders. Perform the Code check using the Process – Member Code Check command. This will identify the demand-to-capacity for that size. You can investigate the design of individual joists using the Process – Results – View/Update command. With that command different sizes can be Analyzed and investigated until the desired size is determined, which can be assigned back to the model using the Update Database command in View/Update, or by using the Assign Size command.

 

The details of the design can be seen in the Member Code Check report. Remember that the results shown here are as if the joist was an I-shape, but the data in the table has been manipulated such that the results from the Virtual Joist Girder being designed as a beam will closely approximate the design of the real joist girder of the same weight under those same loads.

 

 

Note that the Steel – Seismic Provisions mode is not applicable to Virtual Joist Girders.

 

Specifying Steel Joist Girders

As explained previously, these Virtual Joist Girders do not represent any specific Steel Joist Girder design. Rather, they are equivalent-beam section properties based on top and bottom chord material sizes commonly available from most Joist Manufacturers, and on common relative stiffnesses of chord members to web members, and they do yield reasonably close approximations of the final Joist Girder chord area, effective moment of inertia, and weight, for use in the structural models.

 

Once an appropriate Joist Girder depth selection is made using the Virtual Joist Girder tables, the SER must specify the Joist Girder design requirements using conventional Joist Girder nomenclature, as directed by SJI Standard Specifications and Code of Standard Practice, as well as any special loading requirements. If the Joist Girder stiffness (effective moment of inertia) is significant to the overall building structural model (such as in a lateral load resisting frame), then the SER must specify the Virtual Joist Girder moment of inertia as the “target” Joist Girder effective moment of inertia, along with directions to notify the SER if the final Joist Girder design moment of inertia varies by more than 10% from the “target” value.

 

On the structural drawings do not use the Virtual Joist Girder label; that may not have any meaning to the joist manufacturer. Call out a steel joist as required by the SJI Standard Specifications, indicate the depth and the required moment of inertia, and provide all of the pertinent loads and end moments so that the manufacturer can produce a joist of the necessary stiffness and strength. The gravity loads can be obtained by looking at the Gravity Loads report and the end moments can be obtained using the Member Forces report. The properties of the Virtual Joist Girder can be obtained by looking at the ramaiscwithvjg.bat file (which is located in the RAM Tables directory and can be opened using Notepad). The values in that table look like this:

The Area can be used to calculate the approximate weight of the steel joist girder that will be fabricated.

 

Again, it is important that the engineer understands the proper use of the Virtual Joist Girder tables. Refer to the documentation on the Virtual Joist Girders produced by SJI, currently available on their website at www.steeljoist.org.

Tags: Virtual Joist Girders, Steel Joists, RAM Structural System, RAM

Error : No Pile or soil support defined

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/17/2015 7:52:37 PM

Applies To
Product(s):STAAD Foundation Advanced
Version(s):ALL
Environment: ALL
Area: Gereral
Subarea: Mat foundation
Original Author:Sye Chakraborty, Bentley Technical Support Group

 

I am getting an error when analyzing a mat foundation. The error reads

Error : No Pile or soil support defined. Stopping analysis ...  What am I doing wrong ?

 

The error is being caused by the fact that there are no supports defined for the mat. If your mat is supported on soil, you should go to Analysis properties > Soil Property and ensure that you have specified the value for Subgrade Modulus and also checked the box Use Soil Spring as shown next.

 


 

Alternately if your mat is supported on piles and you are using Pile Supports, you should go to Analysis properties > Pile Spring and ensure that the spring values for the piles ( Kx, Ky , Kz … ) are specified.

 

This should take care of the problem.

Tags: mat analysis stops, error in mat analysis, error, no support, Error : No Pile or soil support defined. Stopping analysis ...

RAM Steel Joists [FAQ]

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 4/17/2015 8:16:04 PM

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

Why is the reported joist allowable load less than the value in the SJI catalog?

In the SJI Catalog only one deflection limit is considered. The live load that results in an L/360 deflection is generally listed as a red number. Given this limit, the program can easily calculate a modified allowable load for any specified deflection limit under criteria – deflection criteria for non-composite members. In other words, if you set the live load deflection limit to L/180, you’ll get twice the allowable load reported in the catalog.

More commonly, it's the net total deflection limit, which defaults to L/240, that causes a discrepancy. Any time the ratio or (D+L)/L exceeds 1.5, this limit will control over the default Live load deflection limit. L/360. Just set the net total deflection limit for non-composite members to zero (0) leaving only the live load deflection limit of L/360 to match the allowable capacities from the SJI tables, exactly.

If you have additional non-composite steel beams that need to meet some specified net deflection limit, consider using the alternate criteria for those beams (or vice versa). You can assign which members use which criterion in the Modeler.

How can I force the program to select only K series joists?

Go to Criteria – Joist criteria and for the table selection, use “RAMSJIK.JST” (or a custom table that includes only K series joist data). The default table, “ramsji.jst”, includes k, lh and dlh joists.

Why doesn’t the program select a K series joist when the equivalent uniform loads are less than the allowable?

Before converting the applied loads to an equivalent uniform load, the program first checks to see that the actual loads never exceed the upper limit for K series joists, 550 plf. In other words, if you have a triangular load on a joist that tapers from 100 plf up to 560 plf, the program will never select a K series joist, even though the equivalent uniform load might be something like 400+ plf.

Why does the program design the joist as a special (SP)?

There are several reasons why a joist will be designated as special. The most common relates to the loading. If the real load varies significantly from uniform, then the joist will be designated SP. If the load is too far from uniform, the joist will not be designed at all. “xxGSP”. Refer to the RAM Steel Beam manual for details on how the real loads are converted into equivalent uniform loads and how the tolerances set in the joist criteria dialog box determine if the joist is SP.

This also happens when the slope of the joist exceeds ½” rise per 12” run, even if the load is perfectly uniform. Any joist exceeding 45 degrees is not designed at all.

Note: For moderate to severe slopes the user should consider the effects of thrust on the supporting structure as this is not considered within the program.

Why does the program call out joist girders starting with “xx”?

The program does not truly design joist girders, it simply labels them based on the depth and the uniformly spaced point loads applied. Any joist supporting other members (regularly spaced) is automatically deemed a joist girder. The first two characters in the joist girder designation are for the depth of the member. The only way to have these numbers called out is to assign a Max Depth restriction to the member in the Modeler using Layout - Joists - Size Restrictions.

See Also

Using SJI Virtual Joist Girders

Product TechNotes and FAQs

Structural Product TechNotes And FAQs   

Tags: joist, FAQs, SELECTservices, RAM Structural System, steel joist, RAM Steel

How do I install Structural Enterprise?

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Revision 1 posted to Structural Analysis and Design - Wiki by Payel on 4/17/2015 11:50:05 PM

  
 Applies To 
  
 Product(s):Structural Enterprise
 Version(s):All
 Environment: N/A
 Area: N/A
 Subarea: N/A
 Original Author:Payel Sasmal, Bentley Technical Support Group
  

I have recently purchased a license for Structural Enterprise; what are the products I need to download?

There is no single standalone installer for Structural Enterprise. The installations for each of the products comprising Structural Enterprise need to be run separately. A list of the installers to be run is listed below:

1 ) RAM Structural System V8i (English) x64

Comments: This is one installer that installs the entire RAM Structural System suite: RAM Modeler, RAM Steel, RAM Frame, RAM Concrete, and RAM Foundation.

2) RAM Concept V8i (English) x64

Comments: This is one installer that installs both RAM Concept and the Post-Tension module.

3) RAM Connection V8i (English) x86

Comments: This will install both the standalone version of RAM Connection as well as the version that can be used within RAM.

4) RAM Elements V8i (English) x86

5) STAAD.Pro V8i (English) x86

Comments: This installer includes all design codes, the advanced analysis module, Sectionwizard and STAAD.beava.

6) STAAD Foundation Advanced V8i (English) x86

7) Microstran (English) x86

Comments: This installer includes all tiers (basic, Pro, Advanced) and design codes.

8) Limcon (English) x86

Comments: This installer includes all design codes. 

9) Structural Synchronizer V8i (English) x64

Comments: This is also known as ISM; it must be installed for ISM interoperability to be available in other products.

P.S. Once you select a product to download, make sure that you download the dependencies as well. In case, the dependency has both x86 (32 bit ) & x64 (64 bit) version of the same file, download the one according to your system's profile. 

 

External Links

Software Download Instructions

The Structural Enterprise

Tags: Structural Enterprise, installation, Structural Enterprise installation

General Support Solutions

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Current Revision posted to Structural Analysis and Design - Wiki by Payel on 4/17/2015 11:59:16 PM

The TechNotes and FAQs in this section cover various licensing and installation related topics that pertain to RAM, STAAD, or other Structural Analysis and Design applications. Use the navigation tree to the left to browse topics. Refer to the SELECTserver and Product Activation Community for more general topics. Some of the most popular topics are also listed below. 

Downloading and Installing

License Configuration

License Checkout with the IEG License Service

License Usage and Trust Licensing

Product Specific Licensing Support Solutions

  • [[Installation - RAM Structural System]]
  • [[Installation - RAM Elements]]
  • [[Installation - RAM Connection]]
  • [[Installation - RAM Concept]]
  • [[STAAD.pro Installation Instructions]]

Tags: Structural Enterprise, installation, GENERAL, index, install, Support Solutions, licensing

RAM SS Walls FAQ

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 4/20/2015 5:52:31 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
  

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

Wall element stiffness in RAM Structural System 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 behaviors.

Understanding the wall element stiffness formulation used in RAM Frame is key to understanding how the cracked factors are applied. The wall element stiffness formulation is discussed in Section 6.4.4 of the RAM Frame Analysis Manual v14.06. The shells used in the program 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. Note that 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, which also can be ignored in the analysis.

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

Modeling Podium Slabs

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

Structural Product TechNotes And FAQs

Tags: RAM Frame, RAM Structural System, WALLS, 3D wall group, SELECTsupport

RAM SS Common Framing Table Errors [TN]

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Current Revision posted to Structural Analysis and Design - Wiki by Seth Guthrie on 4/21/2015 9:39:17 PM

 Product(s):RAM Structural System
 Version(s):13.00.00.00 or later
 Environment: N/A
 Area: Analysis
 Original Author:Bentley Technical Support Group

Framing Tables Errors

General

There are many instances where modeling errors in Ram Structural System are not caught by a Data Check in Ram Modeler. Data Check looks at general geometric information, but it does not attempt to validate all of the information needed to compile the Ram Gravity Framing Tables.

Many of these errors are slab edge or slab opening related.  When one way decking is modeled, slab edges and slab openings must be associated with adjacent beams/walls.  For this reason, avoid using free formed slab edges/openings with one way decking.  Instead, use Layout - Slab - Slab Edge - Whole Perimeter and Layout - Slab - Slab Opening - In Bay to model the slab edges and slab openings.  Then, revise the slab edges/openings where the offset changes.  To further ensure accuracy, only use beams and walls in your Options - Set Snap Points.  Finally, use a positive, non-zero, slab edge offset.  Zero inch slab edge offsets are permitted, but the program algorithms were originally developed assuming non-zero offsets and some configurations can be problematic.

Below are several common modeling configurations that cause problems for the program but are not caught by Data Check.  The right hand image shows the typical error message produced while building the framing tables.  In the background, the framing tables usually halt at a particular member on a particular floor as shown in the left hand image.  Typically, but not always, the modeling issue occurs in the vicinity of the member where the framing tables halt. 


Illegal Framing Configuration

  

Most illegal configuration errors are slab edge or slab opening related.  Subtle inaccuracies in member end locations can cause small slab edge segments that are problematic for the framing tables.  Review the member end coordinates using the Layout - Beam - Show command and the slab edge coordinates using Layout - Slab Edge - Show.  Try remodeling the slab edge using the whole perimeter command. 

Starting with version 14.07, this error dialog more often than not references an invalid beam number, "Illegal Framing Configuration Detected on Beam -1.", but the number listed in the background framing tables dialog is still accurate and can guide you to a point near the problem. 


Missing Slab Edge

  

Many missing slab edge errors are related to having portions of the structure isolated from the perimeter beam loop under one way decking as shown below.  To resolve the issue, model two beams that connect the isolated structure back to the adjacent framing.  If these beams are modeled parallel to the deck span, they will take no tributary load from decking.

 


Internal Error in AdvanceNodeList()

  

Typically, these errors are similar to the missing slab edge error.  The main difference is that there usually is only a single beam/wall connecting the interior structure to the perimeter beam loop as shown below.  Modeling a second beam will resolve the issue.


Beam Loop Intersection not Found

  

Typically, beam loop intersection errors are related to line loads that are slightly askew from a beam.  Often discrepancies arise when a single line load is added over multiple beams that are not truly collinear.  Review the coordinates of the beam and line load using the Layout - Beam - Show and Layout - Load - Line Load - Show command.  To resolve the issue, delete the line load(s) and remodel them using the Add On Beam command.

This error can also be associated with changes in one way deck orientation or properties.  One way decking should always transition along a beam/wall.  That includes transitions from one way decking to two way decking. 

Furthermore, one way deck angles are normally limited to angles between 0 and 179.99 degrees. If imported models have deck angles larger than 180 degrees, this can also cause a beam loop error.


Failed to Find Slab Edge Loads

  

These errors are usually related to tolerance problems between the slab edge loop and perimeter beam loop.  Review the slab edge and beam coordinates using the Layout - Slab - Slab Edge - Show and Layout - Beam - Show command.  Try remodeling the slab edge using the whole perimeter command.

Failed to Create Slab Edge Load Polygons

This error tends to happen when there is a small level with an incomplete perimeter of framing similar to the one pictured below. Adding the short beam on Gird B between the two concrete columns completes the loop with beams 40, 39 and 41. Adding the other beams would only be required if the deck was intended to load beam 42.

Crash with no warning or error message

If a model crashes with no warning or error message then it is harder to diagnose the problem (especially if the Integrity - Data Check offers no clues)

One specific situation that can cause a crash is when a braced frame on an upper level is supported on a two-way deck with no supporting transfer beam. Where it's impractical to add a supporting beam, a work-around for this situation is to model the braces using the Add Standard - Knee brace approach using a vertical offset just a little less than the story height. When the braces intercept the column above the two-way transfer level the framing tables work properly without crashing the analysis and this should have minimal effect on the stiffness matrix.

Two Beams Overlap

Under normal modeling circumstances it should not be possible to model two beams that overlap or cross, but it can happen in some models particularly where the geometry is imported (from dxf, Revit or ISM). 

It's difficult to visually identify where two collinear beams overlap for part or all of the length. Turning on the display of beam numbers can sometimes help.  We have seen cases where one simple span beam and one cantilever beam are in the same location and two numbers will be shown rather than one.


Since the data check does not identify such a problem it only appears when running the framing tables. The error message does not indicate exactly where the problem occurs, but you can usually tell the level with a problem by the status of the framing tables just before the error occurs. 

Finding the beams with the problem usually requires a trial and error process, deleting framing gradually until it works. Then going back and examining those beams that were deleted last in the backup more closely, moving them as required.

We have also seen cases associated with problematic slab opening edges. Deleting and carefully remodeling the slab opening edges at the beam identified where the framing tables stop resolved the problem.

Forcing a "Reframe"

In some cases the beam design module can open and not require a rebuilding of the framing tables, what is commonly referred to as a reframe. A reframe is generally triggered by making any kind of change on a particular level. You can also force a reframe by changing any of the Ram Manager criteria like Self Weight or Live Load Reduction code.

If the design module produces an unexpected error, one simple thing to try is forcing a reframe. You can change one the criteria mentioned above, and click OK. You should get a window like this if previous results are going to be discarded:

Then change the criteria back the way it should be and try the beam design again.

Tags: beams overlap, SELECTservices, Illegal Framing Configuration, RAM Structural System, Internal Error in AdvanceNodeList(), TechNote, Framing Tables, Missing Slab Edge, Beam Loop Intersection, RAM Steel, Failed to Find Slab Edge Loads

STAAD.Pro Import/Export [FAQ]

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Revision 16 posted to Structural Analysis and Design - Wiki by Modestas on 4/22/2015 2:41:01 PM

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

 

 

 

 

 

 

 

 

  1. How can I get my RISA model into STAAD.Pro ?
  2. I do not see the option import/export using StrucLink module.
  3. How to Open a QSE File?
  4. How can I get data transferred between STAAD.Pro and Autopipe ?
  5. How to import a section from the Section Wizard into STAAD.Pro?
  6. Why the DXF drawing is not imported correctly from AutoCAD into STAAD.Pro?

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

There is no way to directly get a RISA model into STAAD.Pro. You may check whether RISA can export in the following formats, both of which can be imported by STAAD.Pro.

1.  CIS/2
2.  3D DXF

Out of these, the CIS/2 is the best option as it lets you transfer not only the wireframe but other member information like Member properties, Material properties, Member orientation, Member end conditions like Releases, Support conditions, Loading information

3D DXF transfer will let you transfer the wireframe only.

These import options in STAAD.Pro can be accessed from within the top menu File > Import

P.S. Although this wiki is about RISA, but it applies to other analysis software as well.

2. I do not see the option import/export using StrucLink under User Tools section.

There could be few reasons behind this.

1) You must not have installed the StrucLink while installing STAAD.Pro.

2) You may have installed StrucLink sperately, but there is a version mismatch.

To fix it, uninstall STAAD.Pro & any version of StrucLink you may have from Control Panel (Add/Remove Program or Programs and Feathures)

Reinstall STAAD.Pro, for Windows Vista/7/8 operating system, right-click on the .msi./.exe file and select the option "Run as administrator" (though you are logged in as administrator). If you run the file as the local administrator only, the program will not be installed properly. "Run as administrator" option is a must; you may need help from your IT personnel. Ensure that the check box next to the "Install companion product" is checked.

 

Once installation is done successfully, you should see the following options under "User Tools" section.

3. How to Open a QSE File?

Go to File > Import… and select QSE ASA option:

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

The transfer of data between Autopipe and STAAD is done through Pipelink. You should ensure that you have the latest available versions of both STAAD.Pro and Autopipe software. The data transfer process is explained in detail in the document PIPELINK_tutorial.pdf

The following post also contain useful information
http://communities.bentley.com/products/pipe_stress_analysis/f/275801/p/76094/205901.aspx#205901

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

  1. Create your built-up section in Section Wizard.
  2. Go to File -> Export to STAAD User Table.
  3. Choose General.  You will see the Open User Table dialog box appear.
  4. Either Select an existing UPT file or create a new one and click Open.
  5. Choose the desired units.
  6. You will see the General dialog box appear:
  7. Input a name (shown as TEST2 above).  You will notice that the properties are shown here.
  8. Click OK.
  9. Close Section Wizard and go back into STAAD.pro.
  10. Go to Tools -> Create User Table.
  11. Click New Table.
  12. Check the box that says External Table.
  13. Browse to the UPT table that you created/selected in step # 4 above.
  14. Select the Section Type as General
  15. Close out of the dialog box to return to the Modeling Mode.
  16. Go to the General -> Properties tab.  You will see the Properties dialog box appear on the right hand side of the screen.
  17. Click on the User Table button.
  18. Select the appropriate user table, click on the section name, and click the Add button.
  19. Assign the section to the appropriate members.

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

There are basically 3 rules to adhere to when generating these DXF files from AutoCAD:

1) All entities must be modeled in your AutoCAD model using simple Lines. STAAD does not import polylines or curves of any forms. You must "explode" the polylines or curves and convert them into simple line entities in AutoCAD before you create the DXF file.
2) Plate elements if any, must be modeled using 3DFace entities in AutoCAD.
3) Since solid element data cannot be stored in DXF files, STAAD cannot import solid element data.

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

Wind load on inclined member

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/22/2015 11:03:47 PM

Applies To
Product(s):STAAD.Pro
Version(s):ALL
Environment: ALL
Area: Load Generation
Subarea: Wind Load Generation
Original Author:Sye Chakraborty, Bentley Technical Support Group

How is wind load calculated on inclined members when Open Structure option is chosen ?

 

The open wind load on an inclined member is calculated based on the projected area of obstruction. The wind intensity is multiplied by the projected area of obstruction offered by the inclined member to find the total force which is subsequently divided by the member length to arrive at the value for the udl on the inclined member.

 

Let the wind intensity = w kN/m2 ( blowing horizontally )

Actual member Length = L m

B=width of area of obstruction in m

Angle of inclination of the inclined member to the horizontal = a

Projected member length ( vertical )  = Lprojected = L sina

Projected area of obstruction = A = B x Lprojected = B x Lsina

Total load on the projected surface = w x B x Lsina

So udl on the member = w x B x Lsina / L = w x B x sina .... Equation 1

 

Now please refer to the attached model. The member 1 is vertical, member 2 is inclined at 60 to the horizontal and member 3 is at 30 degree to the horizontal.

 

Substituting the following values in equation 1,

w= 1 kN/m2

For W12X14 section oriented as shown in the model, B = flange width = 10.084 cm = 0.10084 m

 

For the member 1 ( vertical ) udl = 1 x 0.10084 x sin90 =  0.101 kN/m

For the member 2 ( at 60 deg  )  udl = 1 x 0.10084 x sin60 =  0.087 kN/m

For the member 3 ( at 30 deg  )  udl = 1 x 0.10084 x sin30 =  0.050 kN/m

 

(Please visit the site to view this file)

 

Tags: inclined, wind load on inclined member

ERROR FYLD OUTSIDE THE NORMAL RANGE FOR STEEL

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/23/2015 6:28:39 PM

Applies To
Product(s):STAAD.Pro
Version(s):ALL
Environment: ALL
Area: Analysis
Subarea: Direct Analysis
Original Author:Sye Chakraborty, Bentley Technical Support Group

When I run a DIRECT analysis, I get the following warning

**ERROR- FYLD OUTSIDE THE NORMAL RANGE FOR STEEL, CHECK UNITS. What does that mean ?

 

As part of the DIRECT ANALYSIS definition, you are required to key in certain controlling parameters for the analysis which is done as part of the Direct Analysis definitions. One of these parameters is the FYLD parameter which is used subsequently by the software in computing the Taub values ( equation C2-2b of the AISC 360-10 specifications). The value that you use for the FYLD should be consistent with your input unit settings that you used when defining the parameter. The error would show up if there is an inconsistency between the value you provided and the units you used. For example if your input units were “inch Kip”, you are expected to put in a value for FYLD of 50 or 36 or 48 etc. However if you define it as 7200, you would get the error. The software does an internal check and tries to make you aware of this discrepancy by issuing this warning.

Tags: ERROR- FYLD OUTSIDE THE NORMAL RANGE FOR STEEL

DIRECT ANALYSIS


Deflections with Full E and I values

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/23/2015 6:42:15 PM

Applies To
Product(s):STAAD.Pro
Version(s):ALL
Environment: ALL
Area: Analysis
Subarea: DIRECT Analysis
Original Author:Sye Chakraborty, Bentley Technical Support Group

In a DIRECT ANALYSIS, are the beam deflections for serviceability checks computed using the unreduced E and I values ?

By default STAAD uses the reduced E and I for calculating beam deflection checks. However in the section 5.37.5 of the Technical Reference Manual ( titled Direct Analysis ), you will find mention of a parameter named REDUCEDEI which can be set to a value of 0, for the full E and I to be considered for computing section displacements.

Tags: sections displacements, direct analysis, reduced E and I, deflection, full E and I

Max Absolute stress in Plate Contour

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/23/2015 7:03:02 PM

Question:

In the Plate Stress Contour tab of the Diagrams window, a choice under stress type is Max Absolute (See the following screen shot).

What is the definition of Max Absolute?

Answer:

The membrane stresses and bending stresses can be combined to form the principal stresses, SMAX and SMIN, on the top and bottom surfaces of plate elements. The procedure for obtaining these is explained in example problem 18 of the
Application Examples manual.

Thus, for each load case, there is an SMAX and an SMIN on the top surface as well as on the bottom surface of each element - four numbers per element. Let us denote them as SMAX_top, SMIN_top, SMAX_bottom and SMIN_bottom.

The absolute maximum from among SMAX_top and SMIN_top is termed as "Max Top" in the Plate Contour - stress type - selection box.

The absolute minimum from among SMAX_top and SMIN_top is termed as "Min Top".

Similarly, the absolute maximum from among SMAX_bottom and SMIN_bottom is termed as "Max Bottom".

The absolute minimum from among SMAX_bottom and SMIN_bottom is termed as "Min Bottom".

The absolute maximum from among "Max Top" and "Max Bottom" is the quantity termed as "Max Absolute".

Tags: max absolute plate stress, Max Absolute

Collection of other Postprocessing FAQs

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Current Revision posted to Structural Analysis and Design - Wiki by Sye on 4/23/2015 7:05:52 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 ?
  19. How to get Member End Forces for a specific selection of beams?
  20. How do I change stress output units in the *.ANL output file? They are coming out as kN/m2. I want N/mm2
  21. How do I save a 3D rendered view (generated by the pyramid' icon)? I am able to do this for other views using View > View Management

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.

19. How to get Member End Forces for a specific selection of beams?


The procedure of specifying the commands to report the member end forces is described in STAAD.Pro Help manual chapter 1.5.12:



Alternatively, one can use a Report Setup with specified Ranges (by group or simply typing in the member numbers in the Ranges field):

20. How do I change stress output units in the *.ANL output file? They are coming out as kN/m2. I want N/mm2.

The units of items reported in the analysis output file are based on the unit settings in the input command file ( editor ). The unit that is current at the time the relevant command triggering the output is processed, is used for the reporting. One can set the units appropriately using the editor ( Edit > Edit Input Command File ) as explained next. For example to get the support reactions and member forces reported in Newton and mm units one needs to enter the unit command before the print commands as shown next

PERFORM ANALYSIS

UNIT MM NEWTON

PRINT SUPPORT REACTIONS

PRINT MEMBER FORCES

Any other output printed in the ANL file following the above commands, would also be printed in the currently set units of Newton and mm.

21. How do I save a 3D rendered view (generated by the pyramid' icon)? I am able to do this for other views using View > View Management

As of now there is no way to save the 3D rendered view as a Saved View. However here are a couple of options that you may find useful 

  1. Right click on the 3D Rendered View and choose the Take Picture option. The picture is then saved and can be accessed from within Report Setup ( File > Report Setup ) and can be included as part of the report.

  2. Instead of using a 3D Rendered View, you can plot a full section view ( right click inside the whole structure window and choose Labels > Structure > Full Sections ). This would be similar to the rendered view but the difference is, you would be able to save it through View > View Management

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

STAAD.Pro Postprocessing Solutions

Does specifying the Notional Load Factor as 0.002 automatically define notional loads

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Revision 1 posted to Structural Analysis and Design - Wiki by Sye on 4/23/2015 7:35:28 PM

Applies To
Product(s):STAAD.Pro
Version(s):ALL
Environment: ALL
Area: Analysis
Subarea: Direct Analysis
Original Author:Sye Chakraborty, Bentley Technical Support Group

I have defined a notional load factor of 0.002 as part of my DIRECT ANALYSIS definition. Does that automatically define the notional loads in the analysis ?

 

Specifying the NOTIONAL LOAD FACTOR as part of the DIRECT ANALYSIS definition does not create the Notional Loads. This factor is just a switch that is used to instruct the software on whether to iterate Taub or not. When the factor is specified as 0.002, the program calculates Tau-b in an iterative solution based on the member forces. On the other hand, when notional load factor is specified as 0.003, then the program does not perform any additional iterations of Tau-b.

 

In addition to specifying the NOTIONAL LOAD FACTOR, the user must define the notional loads. Although these loads could be added manually on a load case by load case basis but one can save significant amount of time by using the Auto Load Combination Generator and checking the option to include notional loads as part of it as shown next.

 

   

Tags: direct analysis, Notional Load, notional load factor, 0.002
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