Hi all,
For a Stress intensity factor calculation i need to mesh a 2d surface. I have the problem i get alot of triangle elements, but i want quad only. On the other hand i need singular elements at the crack tip, this location is variable.
How can i get singular elements at the tip, but not in the rest of the plane? i used KSCON to get the singular ones at the tip, and free mapping for the rest.
here a minimal working example:
finish
/clear
/title, cracktip
/PREP7
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
!!!!!!!!!!!!! define parameters !!!!!!!!!!!!!!!!
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
b=0.5 !width plate
h=0.5 !hight plate
r_s=0.125 !radius spill
scon=b/100 !kscon element size
a=0.095 !half crack length
KXX=60 !thermal conductivity
C=300 !heat capacity
DENS=7850 !density
!!!create geometry, 1/4 of the plate is modelled
k,1,0,0
k,2,0,h/2
k,3,b/2,h/2
k,4,b/2,0
k,99,a,0
l,1,2
l,2,3
l,3,4
l,4,99
l,99,1
LSEL,ALL
KSCON,99,scon,1,8,0, !cracktip KP
AL,1,2,3,4,5
AESIZE,ALL,b/25,
!!!PLANE55 for thermal problem and surf152 for convection
ET,1,PLANE55
MP,KXX,1,KXX
MP,C,1,C
MP,DENS,1,DENS
AMESH,ALL
As you can see the mesh looks terrible, all help appreciated!
Cheers,
Bram
For a Stress intensity factor calculation i need to mesh a 2d surface. I have the problem i get alot of triangle elements, but i want quad only. On the other hand i need singular elements at the crack tip, this location is variable.
How can i get singular elements at the tip, but not in the rest of the plane? i used KSCON to get the singular ones at the tip, and free mapping for the rest.
here a minimal working example:
finish
/clear
/title, cracktip
/PREP7
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
!!!!!!!!!!!!! define parameters !!!!!!!!!!!!!!!!
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
b=0.5 !width plate
h=0.5 !hight plate
r_s=0.125 !radius spill
scon=b/100 !kscon element size
a=0.095 !half crack length
KXX=60 !thermal conductivity
C=300 !heat capacity
DENS=7850 !density
!!!create geometry, 1/4 of the plate is modelled
k,1,0,0
k,2,0,h/2
k,3,b/2,h/2
k,4,b/2,0
k,99,a,0
l,1,2
l,2,3
l,3,4
l,4,99
l,99,1
LSEL,ALL
KSCON,99,scon,1,8,0, !cracktip KP
AL,1,2,3,4,5
AESIZE,ALL,b/25,
!!!PLANE55 for thermal problem and surf152 for convection
ET,1,PLANE55
MP,KXX,1,KXX
MP,C,1,C
MP,DENS,1,DENS
AMESH,ALL
As you can see the mesh looks terrible, all help appreciated!
Cheers,
Bram