finish
/clear
/UNITS, SI
/Title, "Rahmen, Belastung auf Rahmen"
/prep7

MP,EX,1,21E10
MP,DENS,1,7800
MP,PRXY,1,0.3

K,1,0,0,0
K,2,0,0,2.5
K,3,0,5.0,2.5
K,4,0,5.0,0
K,5,3,0,0
K,6,3,0,2
K,7,3,5.0,2
K,8,3,5.0,0

!Fläche
K,30,0,0,2.8
K,31,0,5.0,2.8
K,32,3,5.0,2.8
K,33,3,0.0,2.8

/triad,off
!Steher
L,1,2
L,4,3
L,8,7
L,5,6
L,6,7 !Längsträger vorne
L,2,3 !Längsträger hinten
!Querträger
L,2,6
L,3,7

A,30,31,32,33 !Fläche

ET,1,BEAM189
KEYOPT,1,1,1
KEYOPT,1,2,1
keyopt,1,4,2 ! output both torsional and flexural shear stress
keyopt,1,6,3 ! extrapolate section forces, etc. to nodes
keyopt,1,7,2 ! maximize output data ...
keyopt,1,9,3 ! maximize output data ...
SECTYPE,1,BEAM,ASEC,60x60
SECDATA,0.0013481,5.45E-7,0,5.45E-7,0.9E-12,1.09E-6,0.03,0.03,0.03,0.03,0.06,0.06

!Auswahl Linien Profil 60x60
LSEL,S,LOC,Z,0,2.5
LATT, 1,,1,,,,1 !Profilzuweisung
LESIZE, ALL,,,10
LMESH,ALL

ET,2,SHELL281
keyopt,2,1,2
SECTYPE,3,SHELL
SECDATA,0.01,1 !Platte mit 0.01m Dicke

LSEL,S,LOC,Z,0,2.8
ASEL,ALL
AATT,1,,2,,3
LESIZE,ALL,,,10
AMESH, ALL

!Last
LSEL,S,LOC,Z,2.0,2.5
NSLL,S,1
F,ALL,FZ,-1

!Randbedingungen
nsel,s,loc,z,0
d,all,uz,0
d,all,uy,0
d,all,ux,0
d,all,rotz,0
d,all,roty,0
d,all,rotx,0

ALLSEL
finish

/SOLU
time,1.0
nsubst,1,100,1
outres,all,last
outpr,all,last
ANTYPE,static
NLGEOM,OFF
NROPT,FULL
solve
finish