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Hi All; I would like to kindly ask you how to extract ESE values component by component under hyperstudy.. The problem arises as i perform DOE study and since my desing changes so the element numbers,ID s etc.. i want to select elements "by component" and retrive their ESE values at each...

And after updating :) Thank you very much..Maybe it is long way but i have to follow the software's solution steps.. And i really wonder if there is another short ways to updating.. Anyway my problem solved by your help Thank you again...

Hi Fernando Thank you very much now it works..!! I put screenshots as how it updated in folder.. http://files.engineering.com/getfile.aspx?folder=6e62b9f8-388f-4c77-a876-16bd734afbba&file=Step_I.jpg

For example i seached and found a code similar to what i intent to do path= systempath[:len(systempath)-4]+r"\startup\materials\German\Catalog.CATMaterial" MatDoc=CATIA.Documents.Open(pfad) the path must be the working directory of my CATPart...

Hi Fernando; Q:Do you first create all those folders? How do you run the bat file? Once after creating all folders or after creation of each folder? Why do you need to save each time the catvbs in the folder? Ans:I use another software that runs and does all staff explained above..Therefore it...

Hi Fernando; Let me explain in simpleform without giving detail.. In My current directory: I have two file C:\Temp -Beam.CATPart -params.catvbs my software automatically updates my params.catvbs with new dimensions for "Height" and...

Hi thank you very much for your kind and valuable help to me I would like to give a bit detail and maybe we can a bit modify above Macro by your help I run the macro via another software via script.bat file in which some send of codes are available and at each ıteration it changes the workıng...

Hi I have a two file in one folder one of which is Beam.CATPart and the other is my macro CATIAHST.catvbs I am trying the following code using script i attached "C:\Program Files\Dassault Systemes\B20\win_b64\code\bin\CNEXT.exe" -nowindow -batch -macro...

Cat Parthttp://files.engineering.com/getfile.aspx?folder=0cd13174-e74a-4d52-9d3a-8db6d64e85c7&file=Beam.CATPart

Hi yes sure http://files.engineering.com/getfile.aspx?folder=8a225844-957a-4854-8d35-258f17fd0430&file=script_win64.bat

Hi all; I recorded a macro within Catia and would like to run this macro in batch mode aiming to update the required parameters dynamically.. I need help at this point beacuse when i update my macro and using "C:\Program Files\Dassault Systemes\B20\win_b64\code\bin\CNEXT.exe" -nowindow -macro...

Hi All; I am really confused about the application of loads that is either maneuver or aerodynamic loads at the same time or indivudiually while extracting margin of safety for each component under different loads Could you please guide me in finding MoS... Maneuver Loads:4G Aerodynamic...

Hi All I have returned to my data provider to give me full PSD thanks for your support

Hi Again; Also from the reference below i found that: "The frequently used MIL-STD-810 standard states that a 1-to-1 conversion of a sine sweep test to a random vibration test is not possible and that a measured vibration level is the best basis for formulation of vibration requirements."...

Hi; Unfourtunately no..The vibration profile given as a combination of PSD and i think sine sweep such that; 10-40 0.15 g^/Hz and the rest is 40 to 500 as 5.5 G limit. I would like to convert the second part to PSD namely g^/Hz unit so i will get full PSD vibration profile There is a formula...

Hi all; I am given a vibration profile that is stated in G unit between some certain frequency values I wonder if anyone knows conversion and theory behind it to extract the vibration profile in terms of PSD .. Example: 0.01g^2/Hz 5-10 Hz 2g 10-100Hz Thanks in advance.

SW Thank you very much for your kind help. I would like to ask to be sure if you dont mind; SW:> calculate the failure stress or strain and use that value for the other thicknesses Me:>Now i understood.As Brain and you stated aboove regardless of the thickness, the laminates will fail at...

From the maksimum failure strain point of view i think yes. Any idea about the analysis procedure?

Hello All;I had asked same in composite platform but again i would like to kindly ask here too.. My question is especially in the field of testing of composite materials and making use of the datas obtained from those tests.If i test a 2.5 mm thick specimen and get result how can i use the...

Hello All; I think i am not clear with my above question and i would like to kindly ask in other words.. My question is especially in the field of testing of composite materials and making use of the datas obtained from those tests. If i test a 2.5 mm thick specimen and get result how can i...