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Objective: Compare 7 cases as discussed in last 3 slides, in a tabulated format on the basis of: 1. Total number of cycles, Energy error, mass error and simulation time.2. Notice the animation of all 5 and describe the animations in brief on thebasis of whether the elements are being deleted or cracked.3. Plot energies…
Durga Varaprasad
updated on 07 Sep 2021
Objective:
Compare 7 cases as discussed in last 3 slides, in a tabulated format on the basis of:
1. Total number of cycles, Energy error, mass error and simulation time.
2. Notice the animation of all 5 and describe the animations in brief on the
basis of whether the elements are being deleted or cracked.
3. Plot energies and notice any difference.
4. Based on all the results, which case would represent the on-field
scenario.
5. Prepare a ppt/docx and list down case by case result and your conclusion
as to why the failure happened.
CASE-1 LAW2_EPSMAX_FAILURE:
1.Displacemennedt:
Displacement is the Relative position resulting from the motion that is final position of apoint relative to its intial position
2.velocity:
velocity is defined as a vector measurment of the rate and direction of motion.scalr magnitude of velocity is the speed of the motion.In calculus velocity is the first derivative of position with respect to time.velocity formula is displacement/time.
3.%THickness Reduction calculated :
4.Plastic strain along thickness:
Plastic strain is the strain that occurs after yield point which do not reverse after removing load.
5.Strain:
strain(Elastic) is the ratio of amount of deformation experienced by the body in the direction of force applied to the initial dimensions.Elastic strain which is developed in elastic region with in yield point.this can be reverse after removing the load.
6.Vonmises stress:
vonmises stress ia a value used to determine if a given material will yield or fracture.the vonmises yield criteria states that if the vonmises stress of material under load is equal or greater than the yield limit of the same material under simple tension then the material will yield.vonmises stress is the stress developed in all directions.
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
CASE2 LAW2_EPSMAX_CRACK:
In this case change values in failure_johnson_1 as Ixfem=1,Ifail_sh=1,Dadv=1.
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
CASE3:LAW2_EPSMAX_NO FAIL
IN this case delete failure_johnson card then run the simulation
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
CASE4:LAW2-
In this case delete the value of EPS_P_MAX and run the simulation
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
CASE-5-LAW-1 ELASTIC :
In this case change material card name as LAW1_Elastic.and give E,Nu,Density values as previous case. Then Run the simulation.
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
Case-6-LAW_36:
In this case create material plas_tab 36 with given values.then create a curve with values given below and Run the simulation
In this case change card image as M27_PLAS_BRIT.and run the simulation.
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
CASE-7-LAW-27 :
In this case change card image as M27_PLAS_BRIT.and run the simulation.
1.Displacement:
2.velocity:
3.% Thickness reduction :
4.Plastic strain along thickness:
5.Strain:
6.vonmisess stress:
6.Plot rigid wall forces, internal energy, hourglass energy, contact energy, total energy of the simulations.
Rigid wall forces:
Comparison of Results:
s.no | parameters | Law2_EPSMAX-fail | Law2_EPSMAX-crack | Law2_EPSMAX-No fail | Law2 | LAW_1_Elastic | Law_36_Plastab | Law 27_Brit |
1 | Energy error | 0.8% | 4.1% | 0.8% | 1.1% | 0.8% | 0.8% | 0.8% |
2 | no of cycles | 49379 | 49217 | 49407 | 49303 | 47968 | 49379 | 49506 |
3 | internal energy | 26000 | 31000 | 27000 | 37000 | 8.0E+05 | 27000 | 30000 |
4 | kinetic energy | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
5 | hourglass energy | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
6 | contact energy | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
7 | Resultant tangent force | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
8 | Resultant normal force |
6000-8500 (Sudden drop) |
peak 8500 (Gradual drop) |
6000-8500 (Sudden drop) |
peak 9500 (No drop) |
5.0E+05 |
6000-8500(UPTO 4MS) FLUCTUATES 0-1000 |
6000-8500(UPTO 4MS) FLUCTUATES 0-4500 |
9 | displacement | 1.586E+01 | 1.127E+01 | 1.932E+01 | 5.626E+00 |
4.999E+00 |
1.586E+01 | 1.669E+01 |
10 | velocity | 2.389E+01 | 2.268E+01 | 2.153E+01 | 6.704E+00 | 7.815E+01 | 2.389E+01 | 1.955E+01 |
11 | % thickiness reduction |
7.227E+00 -1.126E+01 |
9.886E+00 -1.312E+01 |
7.456E+00 -1.218E+01 |
5.402E+01 -2.282E+01 |
4.525E+01 -1.305E+01 |
7.22E+00 -1.126E+01 |
1.789E+01 -1.281E+01 |
13 | plastic strain | 1.492E-01 | 1.508E-01 | 1.509E-01 | 3.121E-01 | 0 | 1.492E-01 | 2.323E-01 |
14 | strain | 1.404E-01 | 1.426E-01 | 1.358E-01 | 4.012E-01 | 2.010E-01 | 1.404E-01 | 1.607E-01 |
15 | vonmisess stress | 2.752E+02 |
MAX 2.951E+02 MIN 2.158E-01 |
2.707E+02 |
MAX 2.451E+02 1.239E+00 |
1.089E+04 | 2.752E+02 | 2.875E+02 |
conclusions:
CASE-1(LAW2_EPSMAX_FAILURE):
In this case the element fail after reaching EPSmax value.elements will deleted after reaching the EPS MAX value.
CASE-2(LAW2_EPSMAX_CRACK):
In this case element will get crack due to Ixfem=1 means It will try to break the element like crack under given loading conditions.if IXFEM is 0 then the whole element will delete.
CASE-3(LAW-2_EPSMAX_NOFAIL):
In this case element wont get crack.the element will take as EPSMAX consideration.
CASE-4(LAW-2):
In this case the element will not get delete because of EPSMAX IS 0.so there is no heat decipation.
CASE-5(LAW1-ELASTIC):
In this case the stress strain curve is linear up to elastic limit means if we remove load it will come back to its original position but in crash it is not suitable.In this maximum internal energy is increaing as defomation increases.There is no plastic deformation thats why plastic strain is 0 in this case.due to continuous deformation the rigid wall forces are also high in this case.vonmisess stress developed is high because strain is high.
CASE-6(LAW-36):
In this case we will give additional information of lab tested curve so the stress strain curve will follow the given curve.
CASE-7(LAW-27):
There is no nonlinearity in this case the element will get fail directly there is no yielding criteria in this case.
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