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August 24, 2024 at 5:45 pmAnsys BegineerBbp_participant
Hi
I am doing buckling analysis on a curved panel whose schematic I have attached. I have been trying to do buckling analysis on this geometry for different cases but results dont seem to be matching with theoretical. Can someone please guide me whats wrong in my code? Lets consider this case
a=b=50mm, Theta=180 degrees, E= 200MPa, t=0.5, poisson ratio=0.3. Thank you very much.
/CLEARÂ Â Â Â
/PREP7 Â
smrt,off
ANTYPE,STATIC Â
ET,1,SHELL63,,Â
R,1,0.5 Â
MP,EX,1,200e9Â
MP,NUXY,1,0.3 Â Â
R1 = 31.38
L = 25
PI = 4*ATAN(1)
T=PI/2
THETA =T*180/PI
CSYS,1Â
K,2,R1,90,L
K,3,R1,(90-THETA),L
K,5,R1,90,-L
K,6,R1,(90+THETA),L
K,7,R1,(90-THETA),-L
K,8,R1,(90+THETA),-L
l,3,2 Â Â
l,2,6 Â Â
l,3,7 Â Â
l,7,5 Â Â
l,5,8 Â Â
l,6,8
lcomb,1,2
lcomb,4,5
al,1,3,4,6
LESIZE,ALL, , ,24, ,1, , ,1,
amesh,1
lsel,s,line,,3
lsel,A,line,,6
nsll,,1
D,ALL, , , , , ,UY, , , , ,
lsel,s,line,,4
nsll,,1
D,ALL,, , , , ,, , , , ,UZ
lsel,s,line,,4
local,11,1,0,0,0, Â Â
nsll,,1 Â Â Â Â Â
nrotate,all     Â
D,ALL, uX, , , , ,, , , , , Â Â
lsel,s,line,,1
local,11,1,0,0,0, Â Â
nsll,,1 Â Â Â Â Â
nrotate,all    Â
D,ALL,, , , , ,UX, , , , , Â Â
F,ALL,FZ,-1/25
/sol
PSTRES,1
solve
finish
/sol
ANTYPE,1 Â
BUCOPT,LANB,2,0,0,CENTER
solve
finish
/post1
set,list -
August 25, 2024 at 12:11 pmSampat KumarAnsys Employee
It seems you have created a duplicate question.Â
I will close this forum query and for additional discourse on this topic, please access the link below.
https://innovationspace.ansys.com/forum/forums/topic/buckling-analysis-on-a-curved-panel/
Thanks,
Sampat
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