Chapter 8:
Main Toolbar Features
VSP User Manual
61
Version 1.7.92
Figure 58
shows the stress results for Calculix for the wing mesh generated in
VSP. Listed below is the input file for this run:
*INCLUDE,INPUT=feageom.dat
*INCLUDE,INPUT=fixed.nam
*BOUNDARY
NFIXED,1,3
*MATERIAL,NAME=AL
*ELASTIC
70000.0,0.33,20.0
*DENSITY
1.894e-9
*SHELL SECTION,ELSET=Eallquads,MATERIAL=AL
0.05
*SHELL SECTION,ELSET=Ealltris,MATERIAL=AL
0.05
*INCLUDE,INPUT=feanodethick.dat
**
*STEP, INC=100
*STATIC
**DLOAD
**Eallquads,GRAV,98100.,0.,0.,-1.0
*DLOAD
Ealltris,GRAV,98100.,0.,0.,-1.0
*NODE FILE,NSET=Nall,OUTPUT=3D,
U
*EL FILE, NSET=Eallquads, OUTPUT=3D,
S
*EL FILE, NSET=Ealltris, OUTPUT=3D,
S
*END STEP
Link
Figure 59: Link option under the Geometry menu.