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General Mechanical

General Mechanical

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Fracture SMART – Crack growth Fatigue with Paris law – temp dependent constants

    • tobias.doerr
      Subscriber

      Dear All,

      I'm using Ansys 2023 R2, Mechanical Application within Workbench.

      The purpose is a crack simulation of an arbitrary crack, calculating Fatigue (number of cycles under variying loads).

      For this purpose, I use Paris law (Fig.1). This works fine as long as I use only one value for Material constant C and exponent m in the Engineering data.

       

      However, if I want to use Paris law with different material constants and exponents depending on temperature (Fig.2), it doesnt work.

      Is there a way to make it work?

              

      Thanks for your help.

      Regards,

      Tobi

         

    • Lydia Lymperopoulou
      Ansys Employee

      Hi Tobias,

      You can define a temperature-dependent crack growth law in a SMART Crack Growth analysis but you will need to employ some APDL commands.

      "The constants can be defined as a function of temperature (TBTEMP or TBFIELD,TEMP) and/or stress ratio (TBFIELD,SRAT)" :  https://ansyshelp.ansys.com/account/secured?returnurl=/Views/Secured/corp/v241/en/ans_frac/franundcgrowmech.html%23fraccgrowmechanics

      So, insert a Commands Object under your SMART Crack Growth Object; First apply Paris law  but then define the two temperature points like tbdata,1,C1,m1and tbdata,1,C2,m2

      Then assign the crack growth law to crack CGROW (ansys.com) like:

      cgrow,fcop,mtab,cglawid

      • tobias.doerr
        Subscriber

        Thank you very much for your great help.

        In the meantime another question pops up:

        I would like to map external imported Loads like initial strain on to my mesh. However, it seems, it cannot be used together with SMART fracture. 

        Is there a solution for this?

        Thanks a lot!

    • tobias.doerr
      Subscriber

      EDIT: The question before mentioned aims to adress the following:

      • 1. I want to make a creep calculation of the model
      • 2. map the residual stresses/strains onto a submodel
      • 3. calculate crack fatigue with the pre-conditioned stresses/strains (stress ratio is 0)

      Thank you very much for your help!

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