abc123ali
Mechanical
- Nov 6, 2023
- 90
Resepected ABAQUS Users, I am performing the tensile test upto the yield point of metallic sintered joint placed betwen the chips to join them. Taking the experimental data and putting into the ABAQUS property module and proceeding towards simulation are not giving the reliable results to match the experimental data. The experimental data is put in form of stress strain uniaxial tension test. The thickness of joint is made 0.4 mm, stress in MPa and the chips thickness is 0.5 mm. To achieve the yield stress which is 27.5 MPa, the strain is applied upto yield point and the yield strain is to be 0.02 according to experimental data which is multiplied by the thickness of 0.4 mm to get the value of deformation required which is 0.008 mm or simply change in length. The area of crossection of the chip is 20mm*5mm.
I am also facing problem of
""1. The applied amplitude for cyclic displacement in the load module is different from the output reaction displacement which should be possible because the model is strain controlled.""
""2. The output results are taken in terms of reaction force and displacement curve which should come out in Newton according to the units set above and the displcement should be in mm. Now the value of reaction force is very low as just 0.6 N and the applied strain peak value is 0.008 mm is not reached but just to 0.007mm why is it so. so if force is 0.6 N then the stress is 0.6/100 equals 0.006 MPa which is wrong and not even a bit near to 27.5Mpa where it should be.""
But he value shown in mises and stress COMPONENTS goes to 37 MPa to 46 Mpa not exact but a bit near
How to solve this calibration problem? The cae file is attached here
Thanks for Cooperation
I am also facing problem of
""1. The applied amplitude for cyclic displacement in the load module is different from the output reaction displacement which should be possible because the model is strain controlled.""
""2. The output results are taken in terms of reaction force and displacement curve which should come out in Newton according to the units set above and the displcement should be in mm. Now the value of reaction force is very low as just 0.6 N and the applied strain peak value is 0.008 mm is not reached but just to 0.007mm why is it so. so if force is 0.6 N then the stress is 0.6/100 equals 0.006 MPa which is wrong and not even a bit near to 27.5Mpa where it should be.""
But he value shown in mises and stress COMPONENTS goes to 37 MPa to 46 Mpa not exact but a bit near
How to solve this calibration problem? The cae file is attached here
Thanks for Cooperation