Clik here to view.
RE: STATIC AND DYNAMIC ANALYSIS OF STRUCTURE
STAAD.Pro V8i SS5 has been released and you can use RIGID FLOOR DIAPHRAGM from GUI.
View ArticleFRAME FOR PANEL
We have carried out the analysis this analysis is report is not matching with manual calculation. Kindly intimate where we have done mistake. kindly find the attached file.
View ArticleRE: FRAME FOR PANEL
Please provide the manual calculation citing the load case and member number?
View ArticleRE: Master/slave used in a curved bridge
I'm sorry for the mistake. “It seems like STAAD doesn't have the option to set up master/slave nodes in globle system.” I actually wanted to say "local". I have corrected my post.
View ArticleRE: RAM Concept demand exceeds the capacity when designing for reinforcement.
Here's a nice explanation for that: communities.bentley.com/.../11051.ram-concept-plotting-results.aspx
View ArticleRE: STATIC AND DYNAMIC ANALYSIS OF STRUCTURE
Sir, can you please attached an example using american codes. tnx!
View ArticleSTATIC AND DYNAMIC ANALYSIS OF STRUCTURE
Please share a realistic example of seismic analysis using STATIC and DYNAMIC inputs in a single run and explain why the said model is now ready for design (like the mass participation ratio in dynamic...
View ArticleClik here to view.
STAAD offset led to saw tooth moment diagram
The saw tooth moment diagram is as shown in figure. The diagram showed discontinuity after I offset the plate giders down unde the deck. I wonder why it happens and how can solve this problem. Thank you.
View ArticleRE: STAAD offset led to saw tooth moment diagram
When offsets are applied, rigid links are defined between the member end and the nodes from which the offset is defined. These may be visualized very rigid small columns and any shear at the ends of...
View ArticleRE: STAAD.Pro V8i Apply Vertical Load as Lateral
The closest to what you are looking for would be notional loads. If you are concerned that you have span loading which would contribute significantly towards dynamic mass, then you may consider...
View ArticleRE: STAAD.Pro V8i Apply Vertical Load as Lateral
Uncblue : It is just a requirement that the analysis engine has. For proper processing of the seismic load data, it has to read the seismic load case before any other load case. However it is just the...
View ArticleRE: clarify
Hi,In your model, if you want to consider the total undivided length of the beam as the unsupported length of each beam member, then you need to specify KY(K value in local y-axis) and KZ(K value in...
View ArticleRE: clarify
if any conditions are procedure to apply Ly and Lz. In my model a member drawn in Glodal X axis and Global z axis. so which type is select to apply.In a member both Ly & Lz is assigned to same...
View ArticleRE: clarify
You can assign both LY and LZ to a member. You need to find out the unsupported effective length in each direction and specify the length using LY and LZ. LY and LZ values specified to a member may...
View ArticleRE: clarify
You can go through Example 1 for more details (go to "Help > Contents > Application Examples > American Examples > Examples Problems > Plane Frame with Steel Design" for clarification)....
View ArticleDeflection problem
Hi :)How come the values of deflection for beam 1 remains unchanged before and after using this command:MEMBER CRACKED1 REDUCTION RIX 0.35 even though the moment of inertia have been reduced ?Thanks...
View ArticleRE: Deflection problem
communities.bentley.com/.../download.aspxThis rar file contains 3 simply supported beam models , one with;MEMBER CRACKED1 REDUCTION RIZ 0.35the other with; MEMBER CRACKED1 REDUCTION RIY 0.35and the...
View ArticleRE: clarify
I applied LY & LZ to a member the KL/r ratio is 520. But the Ratio is greater than 1. so the result showing fail so i applied only LY or LZ to a member KL/r value is 257. Then the value is greater...
View Articleclarify
A 3meters long member created with 4 nodes. The member supports at 1st and 4 th node, one end is fixed and other end is pinned. In a design 3M is a continuous member, the member is failed in L/r ratio...
View ArticleRE: clarify
Hi,Attach the relevant .std file and also mention the member number for which you are checking the slenderness ratio.
View Article