I’ve modelled a simple RC wall with elastic boundaries at top and bottom. Is it possible to make the elastic boundaries only active in compression? I’m trying to represent a precast RC wall on unreinforced mortar.
+PROG SOFIMSHA urs:3
HEAD #wall_ID
SYST TYPE GDIV GDIR
3D 10E4 NEGZ
GRP NO 1
NODE NO X Y Z
101 0 0 0
102 #L 0 0
201 0 0 #H
202 #L 0 #H
QUAD NO N1 N2 N3 N4 MNO MRF T KR M N
MESH 101 102 202 201 11 12 #t[m] POSZ #L/#dx #H/#dx
ECHO OPT SECT VAL NO
BOUN 1 TITL 'BOUN_GRP';
BOUN NA 101 NE 102 NM FIT TYPE CX CA 1E3
BOUN NA 101 NE 102 NM FIT TYPE CY CA 1E3
BOUN NA 101 NE 102 NM FIT TYPE CZ CA 1E3
BOUN NA 201 NE 202 NM FIT TYPE CY CA 1E3
END
Non-linear effects, such as a spring failure load, can not be calculated with an elastic boundary element. You have to use multiple springs with non-linear stress-strain curves or a material with a tensile stress maximum.
Please have a look at the following commands. They will help you understand the workflow.
BMAT CRAC… (AQUA)
SPRI CRAC … (SOFiMSHA)
SPTS CRAC … (SOFiMSHC)
Keep in mind that non-linear effects are not considered within a linear analysis. You have to run a non-linear calculation with ase.
I would advise you to test the program behaviour with SOFiPLUS(-X) / the SSD and export the relevant tasks to .dat. I have created a short example for you that demonstrates a possible workflow.
Thank you for the hints. Unfortunately, I cannot open your example (I’m operating with a 2018 version), but I have tried to model the supports as SPRI-elements as shown below (I’ll try to keep the modelling in SOFiMSHA). However, the springs keep having tensile forces - what am I missing?
+PROG SOFIMSHA
HEAD #wall_ID
SYST TYPE GDIV GDIR
3D 10E4 NEGZ
GRP NO 1
NODE NO X Y Z
101 0 0 0
102 #L 0 0
201 0 0 #H
202 #L 0 #H
QUAD NO N1 N2 N3 N4 MNO MRF T KR M N
MESH 101 102 202 201 11 12 #t[m] POSZ #L/#dx #H/#dx
ECHO OPT SECT VAL NO
SPRI NO FIT NA 101 NE 102 DX -1 DY 0 DZ 0 CP 1E3
SPRI NO FIT NA 101 NE 102 DX 0 DY -1 DZ 0 CP 1E5
SPRI NO FIT NA 101 NE 102 DX 0 DY 0 DZ -1 CP 1E3 CRAC 0
SPRI NO FIT NA 201 NE 202 DX 0 DY -1 DZ 0 CP 1E5
END
+PROG ASE urs:7
HEAD Structural analysis
LC ALL
SYST NMAT YES
NSTR
END