Methods and systems for specifying metal necking failure criteria in finite element analysis
Methods and systems for specifying metal necking failure criteria in FEA are disclosed. FEA model contains many finite elements representing a structure, a loading condition and a metal necking failure criteria are received in a computer system. The loading condition includes a loading direction. The metal necking failure criteria includes critical strain and fracture strain values, the neck's width, and a profile of strain values between the critical strain value and the fracture strain value within the neck's width. At each solution cycle in the time-marching simulation of the structure, each finite element is check to determine whether it experiences a metal necking failure, which occurs when each finite element's strain obtained in that solution cycle is greater than an average strain value defined in a formula according to the critical strain and fracture strain values, the neck's width and the profile of the metal necking failure criteria.
1. A method of specifying metal necking failure criteria in finite element analysis (FEA) for manufacturing a product or part in a deep drawing metal forming process comprising:
receiving, in a computer system having a FEA application module installed thereon, a FEA model representing a product or part, a loading condition and a metal necking failure criteria, the FEA model containing a plurality of nodes connected by a plurality of finite elements, the loading condition including at least a loading direction, and the metal necking failure criteria including critical strain and fracture strain values associated with a neck, the neck's width and a profile of strain values between the critical strain value and the fracture strain value within the neck's width, the profile comprising two straight lines forming a triangle;
obtaining, with the FEA application module, numerically-calculated structural behaviors by conducting a time-marching simulation of the product using the FEA model under the loading condition, at each solution cycle of a plurality of solution cycles in the time-marching simulation, checking whether each finite element experiences a metal necking failure, which occurs when said each finite element's strain value obtained in the time-marching simulation is greater than an average strain value defined by a formula in accordance with the critical strain and fracture strain values, the neck's width and the profile; and
manufacturing the product in a deep drawing metal forming process based on the numerically-calculated structural behaviors obtained in the time-marching simulation.
2. The method of claim 1 , wherein the metal necking failure criteria is obtained from a material testing procedure.
3. The method of claim 1 , wherein said formula is as follows:
ɛ
average
=
ln
l
1
+
dw
l
0
,
dw
=
we
(
ɛ
f
-
ɛ
c
)
/
2
where:
w is the neck's width,
ε c is the critical strain value,
ε f is the fracture strain value,
l 0 is said each finite element's undeformed dimension in the loading direction,
l 1 is said each finite element's deformed dimension in the loading direction, and
ε average is the average strain value.
4. The method of claim 1 , wherein said profile comprises one or more curves.
5. The method of claim 1 , wherein said metal necking failure occurs in a direction perpendicular to the loading direction.
6. A system for of specifying metal necking failure criteria in finite element analysis (FEA) for manufacturing a product or part in a deep drawing metal forming process comprising:
an input/output (I/O) interface;
a memory for storing computer readable code for a FEA application module;
at least one processor coupled to the memory, said at least one processor executing the computer readable code in the memory to cause the FEA application module to perform operations of:
receiving a FEA model representing a product or part, a loading condition and a metal necking failure criteria, the FEA model containing a plurality of nodes connected by a plurality of finite elements, the loading condition including at least a loading direction, and the metal necking failure criteria including critical strain and fracture strain values associated with a neck, the neck's width and a profile of strain values between the critical strain value and the fracture strain value within the neck's width, the profile comprising two straight lines forming a triangle; and
obtaining numerically-calculated structural behaviors by conducting a time-marching simulation of the product using the FEA model under the loading condition, at each solution cycle of a plurality of solution cycles in the time-marching simulation, checking whether each finite element experiences a metal necking failure, which occurs when said each finite element's strain value obtained in the time-marching simulation is greater than an average strain value defined by a formula in accordance with the critical strain and fracture strain values, the neck's width and the profile; and
whereby the product is manufactured in a deep drawing metal forming process based on the numerically-calculated structural behaviors obtained in the time-marching simulation.
7. The system of claim 6 , wherein the metal necking failure criteria is obtained from a material testing procedure.
8. The system of claim 6 , wherein said formula is as follows:
ɛ
average
=
ln
l
1
+
dw
l
0
,
dw
=
we
(
ɛ
f
-
ɛ
c
)
/
2
where:
w is the neck's width,
ε c is the critical strain value,
ε f is the fracture strain value,
l 0 is said each finite element's undeformed dimension in the loading direction,
l 1 is said each finite element's deformed dimension in the loading direction, and
ε average is the average strain value.
9. The system of claim 6 , wherein said profile comprises one or more curves.
10. The system of claim 6 , wherein said metal necking failure occurs in a direction perpendicular to the loading direction.
11. A non-transitory computer readable storage medium containing computer instructions of specifying metal necking failure criteria in finite element analysis (FEA) for manufacturing a product or part in a deep drawing metal forming process, said computer instructions when executed on a computer system cause the computer system to perform operations of:
receiving, in a computer system having a FEA application module installed thereon, a FEA model representing a product or part, a loading condition and a metal necking failure criteria, the FEA model containing a plurality of nodes connected by a plurality of finite elements, the loading condition including at least a loading direction, and the metal necking failure criteria including critical strain and fracture strain values associated with a neck, the neck's width and a profile of strain values between the critical strain value and the fracture strain value within the neck's width, the profile comprising two straight lines forming a triangle; and
obtaining, with the FEA application module, numerically-calculated structural behaviors by conducting a time-marching simulation of the product using the FEA model under the loading condition, at each solution cycle of a plurality of solution cycles in the time-marching simulation, checking whether each finite element experiences a metal necking failure, which occurs when said each finite element's strain value obtained in the time-marching simulation is greater than an average strain value defined by a formula in accordance with the critical strain and fracture strain values, the neck's width and the profile; and
whereby the product is manufactured in a deep drawing metal forming process based on the numerically-calculated structural behaviors obtained in the time-marching simulation.
12. The non-transitory computer readable storage medium of claim 11 , wherein the metal necking failure criteria is obtained from a material testing procedure.
13. The non-transitory computer readable storage medium of claim 11 , wherein said formula is as follows:
ɛ
average
=
ln
l
1
+
dw
l
0
,
dw
=
we
(
ɛ
f
-
ɛ
c
)
/
2
where:
w is the neck's width,
ε c is the critical strain value,
ε f is the fracture strain value,
l 0 is said each finite element's undeformed dimension in the loading direction,
l 1 is said each finite element's deformed dimension in the loading direction, and
ε average is the average strain value.
14. The non-transitory computer readable storage medium of claim 11 , wherein said profile comprises one or more curves.
15. The non-transitory computer readable storage medium of claim 11 , wherein said metal necking failure occurs in a direction perpendicular to the loading direction.