Hello,
I have a simulation constraint defined as follows:
1.The temperature of the bottom face is set to 353K.
2.The initial temperature for all faces is 323K.
3.Heat flux and ambient temperature are specified as 20W/m^2K and 323K, respectively.
4.The thermal expansion coefficients -0.0032204, -0.0014441, -0.0134487.
5.The material being used is steel with a Young’s Modulus of 200 GPa and a Poisson’s ratio of 0.3.
Could someone explain how to create the inp for this constraint or how to give this constraint in the below inp?
** Nodes +++++++++++++++++++++++++++++++++++++++++++++++++++
**
*Node
1, 0.00000000E+000, 1.00000000E+001, 0.00000000E+000
2, 0.00000000E+000, 0.00000000E+000, 0.00000000E+000
3, 0.00000000E+000, 0.00000000E+000, 1.00000000E+001
4, 0.00000000E+000, 1.00000000E+001, 1.00000000E+001
5, 1.00000000E+001, 0.00000000E+000, 0.00000000E+000
6, 1.00000000E+001, 1.00000000E+001, 0.00000000E+000
7, 1.00000000E+001, 0.00000000E+000, 1.00000000E+001
8, 1.00000000E+001, 1.00000000E+001, 1.00000000E+001
9, 0.00000000E+000, 0.00000000E+000, 5.00000000E+000
10, 0.00000000E+000, 5.00000000E+000, 1.00000000E+001
11, 0.00000000E+000, 5.00000000E+000, 5.00000000E+000
12, 0.00000000E+000, 1.00000000E+001, 5.00000000E+000
13, 0.00000000E+000, 5.00000000E+000, 0.00000000E+000
14, 1.00000000E+001, 5.00000000E+000, 0.00000000E+000
15, 1.00000000E+001, 1.00000000E+001, 5.00000000E+000
16, 1.00000000E+001, 5.00000000E+000, 5.00000000E+000
17, 1.00000000E+001, 0.00000000E+000, 5.00000000E+000
18, 1.00000000E+001, 5.00000000E+000, 1.00000000E+001
19, 5.00000000E+000, 0.00000000E+000, 0.00000000E+000
20, 5.00000000E+000, 0.00000000E+000, 5.00000000E+000
21, 5.00000000E+000, 0.00000000E+000, 1.00000000E+001
22, 5.00000000E+000, 1.00000000E+001, 0.00000000E+000
23, 5.00000000E+000, 1.00000000E+001, 5.00000000E+000
24, 5.00000000E+000, 1.00000000E+001, 1.00000000E+001
25, 5.00000000E+000, 5.00000000E+000, 0.00000000E+000
26, 5.00000000E+000, 5.00000000E+000, 1.00000000E+001
27, 5.00000000E+000, 5.00000000E+000, 5.00000000E+000
**
** Elements ++++++++++++++++++++++++++++++++++++++++++++++++
**
*Element, Type=C3D10, Elset=Solid_part-2
1, 4, 2, 5, 3, 11, 19, 27, 10, 9, 20
2, 4, 6, 5, 1, 23, 14, 27, 12, 22, 25
3, 5, 8, 4, 7, 16, 24, 27, 17, 18, 26
4, 5, 7, 4, 3, 17, 26, 27, 20, 21, 10
5, 4, 5, 2, 1, 27, 19, 11, 12, 25, 13
6, 4, 5, 6, 8, 27, 14, 23, 24, 16, 15
**
** Node sets +++++++++++++++++++++++++++++++++++++++++++++++
**
*Nset, Nset=FixedSet
1, 2, 5, 6, 13, 14, 19, 22, 25
** Steps +++++++++++++++++++++++++++++++++++++++++++++++++++
**
**
** Step-1 ++++++++++++++++++++++++++++++++++++++++++++++++++
**
*Step
*Static
**
** Output frequency ++++++++++++++++++++++++++++++++++++++++
**
*Output, Frequency=1
**
** Boundary conditions +++++++++++++++++++++++++++++++++++++
**
*Boundary, op=New
** Name: Fixed-1
*Boundary
FixedSet, 1, 6, 0
**
** Loads +++++++++++++++++++++++++++++++++++++++++++++++++++
**
*Cload, op=New
*Dload, op=New
**
** Defined fields ++++++++++++++++++++++++++++++++++++++++++
**
**
** History outputs +++++++++++++++++++++++++++++++++++++++++
**
**
** Field outputs +++++++++++++++++++++++++++++++++++++++++++
**
*Node file
RF, U
*El file
S, E
**
** End step ++++++++++++++++++++++++++++++++++++++++++++++++
**
*End step
Regards,
Bhavita