AIM

To design the RC Column and beam based on the analysis of structure.

PROCEDURE

• To open the model of Rc frame building.
• Now we consider the model to process of Analysing the whole frame, then to finding the Failure of elements will occur.
• Then, to correct the particular column and beam as per design standards.
• First go to One Frame view, then to check all properties of materials, elements and coordination, modification factor. etc..,
• After the to check all load cases as well as all load combinations also, at before get to be analyzed.
• Go to Analyze, Choose first order linear > click ok.

• To select the column and have been check the Column properties, detailing and capacity of structure.
• Similarly we have been to check Ast value of that particular column, as well as to contibriute the value of Longitudal top and bottom reinforcement details and stirrups detailng.
• If may any failure will occur, we can able to do the changes of reinforcement bars, Size, Count. similarly have to consider the same at stirrups also.
• At below we shown corrected column detailing without the failure.

• Similarly, we analyze the beam and to design the beam at required properties of without in failure stage.
• Choose one frame, and select one beam to check that designing properties.
• If one beam could be perfect condition and then make copy to other column for getting linear results.

Open the saved file in Tekla software using the open icon present in the file toolbar.

2. now select any of the column member from the model and right-click on the member

let us select C29

3. now a lot of options will appear after right-clicking on the member.

4. From that we will select the interactive design option followed by selecting static.

5. a new dialog box appears.

6. check whether it passes the tests

here our member fails in one test so we have changed its properties to make the member pass the test

7. once this clears all the tests we can use the same properties to similar members click ok

8. there is a new dialog box that appears stating that apply the same change to all the members let is click ok

we can check whether the changed properties are applied on the other members so let us select any other column C27

WE CAN CLEARLY SEE THAT THE DESIGN CHANGES ARE APPLIED TO THE REMAINING COLUMN MEMBERS.

9. now we can design beam members.

10. select a beam member and right-click on the beam

11. a dialog box appears select interactive design option followed by static option.

12. a new dialog box appears showing whether the member passes the tests

for the member we have selected has failed in a test

13.now let us modify its properties such that it much clear the tests

14. there is a new dialog box that appears stating that apply the same change to all the members let is click ok

we can check for other members whether the property is applied

RESULT:

WE HAVE SUCCESSFULLY DESIGNED RC COLUMN AND BEAM BASED ON OUR ANALYSIS

Successfully analyzed the Design of RC beam and column with using of Tekla software.

Procedure :-

Stellar model grids are typically constructed as a set of evolutionary tracks, where models of stellar evolution are run on grids of initial mass and metallicity, often with some other physical parameter varied as well (e.g., rotation, helium fraction, α-abundance, etc.). Each of these evolutionary tracks predicts various physical properties (temperature, luminosity, etc.) of a star with given initial mass and metallicity, as a function of age.

It is also often of interest to re-organize these evolution track grids into “isochrones”—sets of stars at a range of masses, all with the same age. As described in in order to construct these isochrones, the time axis of each evolution track gets mapped into a new coordinate, called “equivalent evolutionary phase,” or EEP. The principle of the EEPs is to first identify physically significant stages in stellar evolution, and then subdivide each of these stages into a number of equal steps. This adaptive sampling enables accurate interpolation between evolution tracks even at ages when stars are evolving quickly, in the post-main sequence phases.

Previous versions of isochrones relied directly on these precomputed isochrone grids and interpolated between grid points in (mass, age, feh) space. This returned for post-MS stages of stellar evolution, and thus was not reliable for modeling evolved stars. However, beginning with v2.0, isochrones now implements all interpolation using EEPs. In addition, it provides direct access to the evolution track grids, in addition to precomputed isochrone grids. Note that version 2.0 includes only the models; future updates will include more (e.g. PARSEC, YAPSI).

Model Grid Objects and Interpolation

Isochrones provides a simple and direct interface to full grids of stellar models. Upon first access, the grids are downloaded in original form, reorganized, and written to disk in binary format in order to load quickly with subsequent access. The grids are loaded as pandas dataframes with multi-level indexing that reflects the structure of the grids: evolution track grids are indexed by metallicity, initial mass, and EEP; and isochone grids by metallicity, age, and EEP.

Model grids

The Basic Model Interface (BMI) supports several different types, described below. Depending on the grid type (as returned from the function), a model will implement a different set .