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Index

*attention
mej : 9.5.1
2DSORT option : 37.3.2
3POINTS option : 15.1.1
4POINTS option : 8.1.1 | 15.1.1 | 17.1.1 | 23.1.1 | 30.1.1
ABOVE option : 7.4.3
abrisc example : 33.
ABS rule : 9.5.4
Acceleration
frequency response analysis : 9.3.3
Accuracy
linear static analysis : 7.2.3
nonlinear iteration : 12.5.2.3
optimization analysis : 5.2.3.3
ADD option
results stack : 14.3.5
ALPHA parameter
transient heat flow : 26.2 | 27.2.1
Aluminum : 12.
ANALYSE command : 1.2 | 5.2.2
Analysis commands : see Commands
Analysis dialog : 2.2.1
Analysis examples : Preface
Analysis results : 1.3
Analysis Settings dialog : 2.2.2
Analysis Setup dialog : 1.2 | 2.2.1
ANGLE option
view angle : 5.2.1
ANIMATE option
drawing : 14.3.4 | Animation.
Animation
mode shape : Animation.
stress development : 14.3.4
Append analysis results : 12.3
Append input : 5.2.3.3
APPEND option
input reading : 7.2 | 8.3.2 | 14.2
output selection : 8.3.2 | 15.3.3
parts to set : 11.1.1
postprocessing output : 12.3 | 27.2.2
ARC option
line : 1.1.2.2 | 12.1.1
Arc-length control
nonlinear buckling : 20.4
arch example : 16.
Aspect Ratio test : 13.1.3
ATTACH option : 1.1.3 | 3.1.2 | 4.1.3 | 7.1.3 | 20.1.3 | 22.1.3 | 23.1.3
load mask : 1.1.5
AUTOCAD : 37.
AUTOMATIC option
drawing : 14.3.5
meshing division : 11.1.2 | 15.1.1 | 23.1.2 | 34.1.3 | 37.2.2
AVERAGE option : 7.2.4 | Stress | 36.3.2
Averaging results : 7.2.4 | Stress | 36.3.2
AXES option
display position : 23.2
graph display : Graphs | 18.4.1 | Postbuckling
mesh labeling : 6.3
B2HT element
staggered analysis : 31.1
steady-state flow analysis : 23.1.2 | 25.1
*BALANC command : 5.2.3.3
Base excitation
dynamic analysis : 9.1.4
BASE load class : 9.1.4
BASE option
quadrilateral surface : 15.1.1 | 18.1.1 | 38.1.2
Batch command file
nonlinear analysis : 12.3
Batch commands : see Commands
Batch interface : 19.1 | 25.1
Batch output : 5.2.3.3
BC3HT element : 24.1 | 24.1.2
BCL6S3 element : 11.1
BE elements
structural : 9.1.2
Beam elements : 1.1.2.5 | 34.1.3
linear static analysis : 2.1.2 | 3. | 4.1
mobile load analysis : 5.1
phased analysis : 32.1 | 33.
stability analysis : 19.1
beam example : 19.
BEAMS option : 4.1.4 | 5.1.4
BELOW option : 7.4.3
belt example : 13.
Bending moments
beam elements : 2.3.2
diagram : 3.2.2
influence line : 5.4.3
Bit Map format : 1.3.4
BLEFT option : 38.2.2
BLUE option : 17.1.1
Body : 36.1.2.2
BODY option : 36.1.2.2
BOTTOM option
multi-surface results : 38.2.2
'BOUNDA' table : 25.1 | 27.1
Boundary case : 26.1.4
Boundary conditions
generation : 20.1.4 | 22.1.4
potential flow : 24.1.4
Boundary constraints : 1.1.4
display : 1.1.4 | 22.1.7
Boundary elements
potential flow : 23.1.2 | 25.1
steady-state heat flow : 24.1
BOUNDARY option : 4.1.2 | 5.1.3 | 20.1.4 | 22.1.4
bplate example : 17.
Bridge
loads optimization : 5.2
mobile load analysis : 5.
phased analysis : 33.
bridge example : 5.
BRIGHT option : 38.2.2
BUCKLI command : 19.2
Buckling analysis : 16.2 | 17. | 18.2 | 22.2
nonlinear : 18.5.1.2 | 19.3 | 20.4
Buckling modes : 17.3.1 | 20.3.2 | 21.3.2 | 22.2.2
Buckling values : 18.2 | 20.3.1 | 21.3.1
CALCUL option
steady-state heat flow : 25.2
CALCULATE option : 1.3.1 | 4.3.1 | 12.2.1 | 36.3.2 | 37.3.2
Calculating dialog : 1.2 | 2.2.3
Cantil example : 2.
Cantilever beam : 2.
CAPACI command : 27.2.1
CAPACI input
solidification : 27.1
Capacitance
heat flow : 26.1.3
solidification : 27.1
CAPATT input : 26.1.3
Cauchy stress : 13.3.2
linear static analysis : 2.3.3
cbeam example : 32.
Cement-sand screed : 23.
chimney example : 4.
CIRCLE option : 14.1.1
CL18B element : 34.1.3
stability analysis : 19.1
CL24I element : 38.1.2
CL9BE element
phased analysis : 32.1
CL9PE element : 9.1.2
Class-I beams : 1.1.2.5
Class-II beams : 2.1.2
cross-section : 2.1.3
Class-III beams
phased analysis : 32.1
CLEAR option : Stress | Stress | 14.3.5
CLOCK option : 21.1.1
viewing rotation : 22.1.1 | 22.2.2
CLOSE option
model document : 1.1.6 | 5.4.1
CoFloor example : 1.
Cohesion : 15.3.1.2
Mohr-Coulomb plasticity : Plasticity.
vs. internal state : 15.3.2.5
Color assignment
preprocessing : 23.1.3
Color filled elements : 20.1.6
Color modulation
mesh properties : 4.1.4 | 5.1.4 | 13.1.4
mesh quality : 12.1.4
sets in mesh : 1.1.2.5 | 13.1.3
COLOUR option
hidden surface view : 23.1.3
mesh quality : 12.1.4
model attributes : 5.1.4 | 21.1.5 | 23.1.3
properties : 4.1.4
Combination of load cases : 1.3.1 | 4.3.1
COMBINE option : 1.3.1 | 4.3.1 | 5.5.4
Combined line : 13.1.1 | 17.1.1
Command Browser : 1.1.2
Command Input : 1.1.2.1
Commands
buckling analysis : 17.3 | 18.2 | 19.2
cross-section analysis : 29.2 | 30.2
direct response analysis : 9.3
eigenvalue analysis : 9.2 | 10.5.2
linear static analysis : 3.2 | 4.2
lubrication analysis : 28.2
modal response analysis : 9.4
nonlinear buckling analysis : 19.3
nonlinear heat flow : 31.4
phased analysis : 32.2
postbuckling analysis : 21.4
spectral response analysis : 9.5.2
stability analysis : 21.3
static nonlinear analysis : 13.3
steady-state heat flow : 23.2 | 25.2 | 31.2
transient heat flow : 26.2 | 27.2.1
transient nonlinear analysis : 10.6.3
COMPOS command
element evaluation : 32.3
'COMPOS' table
beam elements : 32.3
Composed beams : 32.
generation : 32.3
Compressibility : 13.1.4
Compressive strength
concrete : Plasticity.
Concentrated load : 5.
Concrete : 38.
cracking : Cracking.
dynamic analysis : 10.
Concrete floor : 1.
CONDIS input
heat flow : 26.1.3
solidification : 27.1
CONDUC input
solidification : 27.1
Conductivity
heat flow : 24. | 26.1.3
solidification : 27.1
CONNEC subtable of 'ELEMEN' : 37.3
Connectivity : 10.6.6
Constant shear
plane stress elements : 7.4
Constrained Minimization : 14.3
CONSTRAINT option : 4.1.2 | 5.1.3 | 6.1.1
Constraints : 1.1.4
labeling : 17.1.3 | 34.1.2
CONSTRNT option
node labeling : 4.1.4 | 5.1.4 | 17.1.3
CONSTRUCT command : 4.1.1 | 5.1.1 | 5.4.3 | 6.1.1 | 20.1.1 | 22.1.4 | 36.1.1.1
Contact analysis : 14.
Contact elements : Modeling
CONTENTS option : 14.3.4 | 21.1.6 | 23.2
CONTIN command
postbuckling analysis : 18.4 | 21.4 | 22.3
Continuation analysis : 18.4 | 21.4 | 22.3
CONTOUR option : 5.5.4 | 7.2.2 | 12.2.1 | 20.2.1 | 23.2.1 | 24.2.1 | 36.3.1
Contour plots
displacement : 1.3.2 | 20.2.1 | 36.3.1
fatigue failure : 8.3.3
influence field : 6.3
plastic strain : 12.3.3
pressure : 28.2.2
stress : 2.3.3 | 7.2.2 | 12.3.4 | 21.2.2
temperature : 23.2.1 | 24.2.1
truss and beam elements : 2.3.3 | 5.5.4
CONVEC input
boundary elements : 25.1
Convection : 24.
CONVER command
nonlinear iteration : 12.3
CONVER parameter : 18.4 | 21.4
Convergence
steady-state flow analysis : Convergence.
transient flow analysis : Convergence.
transient heat flow : Convergence.
Convergence rate : 40.1.4 | 40.2.4 | 41.1.4 | 41.2.3 | 42.4
CONVTT input
boundary elements : 25.1
COORD option : 23.1.1
'COORDI' table
phased analysis : 33.
Coordinate systems : Local
COORDSYS option : Local | 20.1.5 | 20.3.2
COPY option
geometry : The | 36.1.1.2
model : 5.4.1 | 12.4
CORNERS option : 28.1.3
Coulomb friction : see Friction
Coupled flow-stress analysis : VII.
CQ16E element : 40. | 42.1
fluid-structure interaction : 11.1
nonlinear analysis : 13.
CQ16M element
fatigue failure : 8.1.2
nonlinear analysis : 12.1.4
staggered analysis : 31.1
CQ22E element
nonlinear analysis : 13.
CQ24P element
free vibration : 35.1
CQ40S element : 34.1.3 | 38.1.2
stability analysis : 17.1 | 22.1
transient nonlinear analysis : 10.3
CQ48I element : 34.1.3
CQ8HT element : 24.1.2
fluid-structure interaction : 11.1
steady-state heat flow : 24.1
transient flow analysis : 27.1
CQ8RE element : 28.1 | 28.1.2
CQ8TO element : 30.1.2
Crack pattern : 10.6.7
Crack strain : 10.6.7
crackpl example : 8.
crosels example : 30.
crosrec example : 29.
Cross-section analysis : 29. | 30.
Cross-section view : 36.3.2
Curved shell elements : 38.1.2
stability analysis : 20.1
transient nonlinear analysis : 10.3.1
CUTAWAY option : 36.3.2
Cutaway view : 36.3.2
Cylinder
shape : 36.1.1.1 | 38.1.1.1
CYLINDER option
shape : 20.1.1 | 36.1.1.1
CYLINDRIC option
coordinate system : 20.1.5 | 20.3.2
results transformation : 20.3.2
Cylindrical coordinates : 20.1.5 | 38.1.3
D output
buckling analysis : 16.2 | 19.1
linear static analysis : 3.2.1
Damage : 42.
Damage example : 42.
Damping
modal : 9.4
Rayleigh : 10.6.1
viscous : 41.
DEFAULT option
meshing divisions : 5.1.1 | 17.1.1 | 21.1.1 | 35.1
DEFORM option : 7.2.2 | 13.3.1 | 20.3.2 | 21.2.2 | 37.3.1
Deformed mesh : 2.3.1 | 3.2.2 | 4.3.2 | 15.2.1 | 36.3.1 | 37.3.1
results plot : 1.3.3 | 2.3.3 | 7.2.2 | 20.2.1 | 21.2.2
Delaunay meshing : 1.1.2.2 | 36.1.2.1
DELAUNAY option : 36.1.2.1
DELETE option
item : 5.4.1 | 37.2.1
loads : 5.3 | 32.3
Deleting model entities : 5.3
Diagram
bending moment : 3.2.2 | 5.5.5
DIAGRAM option : 3.2.2 | 5.5.5
DIANA option
file writing : 3.2
Dilatancy angle : Plasticity.
Direct response analysis : 9.3
DIRECTION option
viewing : 4.1.1 | 20.1.1 | 21.1.1 | 36.1.1.1
DISC option : 10.6.7
Disc plot : 10.6.7
DISMOM option : 6.2
DISPLA command
buckling analysis : 16.2 | 20.3 | 21.3
linear static analysis : 37.3
postbuckling analysis : 21.4
DISPLACE load class : 4.1.2 | 12.1.3 | 13.1.5 | 14.1.4
Displacement
damped : 41.2.4
linear static analysis : 1.3.1 | 2.3.1
prescribed : 12.1.3
DISPLAY option : 14.3.5 | 37.2.1
DISPX input
loads optimization : 5.2.3.1
DISPY input
loads optimization : 5.2.3.1
DISTANCE option
measure : 37.2.2
DIVISION option : The | 3.1.3 | 5.1.1 | 5.1.4 | 6.1.2 | 12.1.4 | 23.1.2 | 37.2.2
Divisions for mesh : The
Divisions for meshing : 5.1.1 | 6.1.2 | 11.1.2 | 12.1.4 | 34.1.3
DRAWING command : 3.1.3 | 4.1.4 | 23.2 | Animation.
dtest_w utility : B.
DXF format file
reading : 37.1
DXF option : 37.1
Dynamic analysis
linear : III. | 9.
load factor : 10.5.1
transient nonlinear : 10.6
earthq example : 9.
Earthquake : 9.
Edge representation : 13.3.2 | 36.3.1 | 36.3.1
EDGES option
edge representation view : 13.3.2 | 36.3.1
mesh display : 21.1.5 | 36.3.1
*EIGEN command : 10.5.2 | 11.3.3 | 35.2
buckling analysis : 16.2
fluid-structure interaction : 11.2
Eigenfrequency
explosion : 10.5.3
fluid-structure interaction : 11.3.1
free vibration : 35.2.1
Eigenmode : 9.2.2 | 35.2.2
explosion : 10.5.4
fluid-structure interaction : 11.3.2
Eigenvalue analysis : 9.2
explosion : 10.5
fluid-structure interaction : 11.2
free vibration : 35.
EL-RESULT option : 10.6.6
Elasticity : 1.1.3 | 31. | 31.
Elastoplasticity
return mapping : 12.5.1
'ELEMEN' table
phased analysis : 33.
ELEMENT option
results selection : 5.5.4 | 36.3.2
Element types : A.
ELEMENTS option
line : Stress
number labeling : 17.1.1
ELSEUS user-supplied subroutine : 40.1.2
ELSGUS user-supplied subroutine : 40.1.2
ELSIZE option : 1.1.2.2 | 3.1.3 | 20.1.6 | 23.1.2 | 26.1.2 | 29.1.2 | 30.1.2 | 37.2.2
ENCASTRE option : 4.1.2 | 9.1.4 | 20.1.4
ENTHAL input : 27.1
Enthalpy : 27.
ESTIMA command
loads optimization : 5.2.3.3
steady-state heat flow : 25.2
Estimation report
loads optimization : 5.2.3.3
Euler buckling : 16.2 | 17. | 19.2 | 20.
*EULER command : 16.2 | 19.2
Euler stability : see Stability analysis
European codes : see CEB-FIP
Evaporation : 27.
EXECUT command
buckling analysis : 16.2 | 19.2
nonlinear analysis : 12.3
transient heat flow : 26.2 | 27.2.1
Expansion
element mesh : The
Explosion : 10.
effective pressure : 10.1
Export a Picture dialog : 1.3.4
exptank example : 10.
EXTEMP input : 25.1
External data
material properties : 12.4 | 12.5.3
EXTRAPOLATE option : Stress
Extrapolation of results : 7.2.4 | Stress
Extreme result
in monitor : 7.4.2 | 21.2.1
EXTTEMP load class : 23.1.2 | 24.1.4
EYE command : 5.4.3
viewing : 21.1.1 | 22.1.1 | 38.1.1.1
FACTOR option
zooming : 21.1.6
Fatigue failure : 8.3
FB output
linear static analysis : 3.2.1
FEMGEN command : 5.1 | 12.1
FEMVIE output device
linear static analysis : 3.2.2
transient heat flow : 26.2 | 27.2.1
FEMVIEW command : 12.2 | 28.2.1
FILE command : 5.4.1
FILE option
global space curve : 20.1.5
FILL option
hidden surface view : 23.1.3
*FILOS command : 31.2
FILOS file : 1.2
FIXED command : 5.2.3.3
FIXPOT load class : 11.1.4
'FIXTEM' table : 25.1 | 27.1
FIXTEMP load class : 24.1.4
Flat shell elements
stability analysis : 18.1.1
Floor : 1.
Flow analysis : VI.
Flow elements : 26.1
material : 25.1
Flow-stress analysis : VII.
Fluid-structure interaction : 11.
Fluid-structure interface : 11.1
Flux
steady-state flow analysis : 23.2.2
FLUX load class : 26.1.4
FORCE command
nonlinear iteration : Questions
FORCE input
beam elements : 5.4.2
FORCE load class : 11.1.4 | 21.1.4
*FORTRAN command : 12.5.4 | 15.3.3
FORTRAN compiler : 39.1.2 | 39.2.2
Fraction model : 12.4
Fracture mechanics : 8.
frame example : 3.
FRAME option
picture : 5.1.1 | 24.1.1
Free vibration : 9.2 | 35.
Frequency response analysis : 9.
Friction
Coulomb : 15.3
FROM option
contour plot : 12.3.3 | 14.3.4
FULL option
viewport configuration : 38.2.2
Galerkin integration
transient flow analysis : 27.2.1
transient heat flow : 26.2
GAUSSIAN option
local axes display : 6.3
results selection : 4.3.2 | 23.2.2
Gaussian results
contact force : 14.3.2
flux : 23.2.2 | 24.2.2
status variables : 15.3.7
stress : 4.3.2 | 30.2.2
General body : 36.1.2.2
General connections : Symmetry
GENERAL option
body : 36.1.2.2
GENERATE option : 3.1.3 | 3.1.3 | 4.1.4 | 5.1.4
GEOMET command : 19.3
Geometric nonlinearity
buckling analysis : 20.4
rubber : 13.3.2
Geometric parts
naming : 1.1.2.1
GEOMETRY command : 3.1.1 | 4.1.1 | 5.1.1
GEOMETRY option
copying : 12.4
labeling : 4.1.1
GLOBAL option
space curve : 20.1.5
translation : 21.1.2 | 22.1.2
Grading of line divisions : 11.1.2 | 12.1.4 | 13.1.1
GRAPH option : 1.3.5 | 12.3.2 | Stress | Stress | 14.3.5 | 18.4.1 | 21.4.1 | 22.3.1 | 28.2.2
axes style and labeling : 18.4.1
influence line : 5.4.3
time or space curve : 20.1.5 | 26.1.4
time response : Graph.
Graph plotting : Graphs | Stress | 14.3.5 | 18.4.1 | 21.4.1 | 22.3.1
display style : 18.4.1
history : 10.6.6 | Graph. | 41.1.5
influence line : 5.4.3
overlaid : Overlaid
result along a line : 1.3.5 | 2.3.1
result along line : 10.4.4 | Stress | 28.2.2
result vs. result : 12.3.2
strain path : 42.5
time or space curve : 26.1.4
Graphics cursor : The
Gravity : 1.1.5
GRAVITY load class : 1.1.5
optimization analysis : 5.2.1
structural analysis : 4.1.2
Grid reinforcement
nonlinear analysis : 10.3.3
'GROUPS' table
phased analysis : 33.
GTC subroutine : 12.5.2.2 | 15.3.2.2 | 40.2.2
Hardening
decaying factor : 12.5.2.7
user-supplied function : 15.3.2.6
Von Mises plasticity : 12. | 18.5
HARDIA input
Von Mises plasticity : 18.5
Heat flow analysis : 23. | 23.1 | 24. | 25. | 26. | 31.
Heat transfer : 31.
*HEATSS command
staggered analysis : 31.2
*HEATTR command : 26.2 | 27.2.1
HIDDEN option : 4.1.4 | 20.1.6 | 20.3.2 | 22.1.6 | 23.1.3 | 36.1.2.1
view algorithm : 5.1.4
Hidden view : 20.1.6 | 36.1.2.1
deformed : 20.3.2
History plot
transient nonlinear analysis : 10.6.6
hook example : 37.
Hyperelasticity : 13.
iDIANA : 1.1.1
IL elements
fluid-structure interaction : 11.1.2
IMPERF command : 19.2
Imperfections : 18.5.2 | 19.2
Import of deformations : 33.2
IMPORT option : 33.2
Infinite shell elements : 9.1.2
INFLUE subtable of 'LOADS' : 5.4.2 | 6.1.3
INFLUENC load class : 5.4.1 | 6.1.3
Influence field
linear static analysis : 6.3
mobile load analysis : 5.
INITIA command
transient heat flow : 27.2.1
'INIVAR' table
potential flow analysis : 27.1
*INPUT command : 31.2
Input data : 41.1.1
buckling analysis : 16.1 | 19.1
heat flow analysis : 25.1 | 27.1
staggered analysis : 31.1
Input file : 1.1.6 | 2.1.4
INPUT option
transient heat flow : 27.2.1
Insulation : 27.
Interaction analysis : 11.
Interface
user-supplied subroutine : 15.3.2.1
Interface elements
modeling : Modeling | Modeling | 38.
nonlinear analysis : 15.1
structural : 34.1.3 | 38.1.2
INTERSECT option
line : 20.1.2
surface : 36.1.1.1 | 38.1.1.3
Intersection line : 20.1.2
Intersection surface : 20.1.2 | 36.1.1.1 | 38.1.1.3
INTPNT option : 12.2
INV3 subroutine : 12.5.2.3
Isolines : see Contour plots
ITERAT command
nonlinear analysis : 12.3 | 41.2.2
nonlinear heat flow : 27.2.1
Keywords : Nature | B.
Kinematic hardening : 12.4
Kuhn-Tucker conditions : 12.5.1.3
L12BE element : 1.1.2.5
linear static analysis : 4.1
L2TRU element : 16.1
linear static analysis : 4.1
mobile load analysis : 5.1
L4CT element : 14.1
L4TRU element : 41.1.1
stability analysis : 16.1
L6BEN element
linear static analysis : 3.
mobile load analysis : 5.1
phased analysis : 33.
L7BEN element : 2.1.2
L8IF element
nonlinear analysis : 15.1.1
LABEL command : 3.1.1 | 3.1.3 | 4.1.1 | 5.1.1 | 23.1.2
Labeling the model : The
element numbers : 3.1.3
loads : 17.1.3
node numbers : 3.1.3
supports : 17.1.3
LAMBDA parameter : 18.4
Large deformations : 19.3
LEFM : see Fracture mechanics
LEVELS option
contour plot : 23.2.1
LIMITS option
append to set : 34.1.2
Line
properties assignment : 4.1.3
LINE option : 4.1.1 | 5.1.1
graph : 1.3.5 | 5.4.3 | 5.4.3 | Stress | Stress | 14.3.5 | 28.2.2
line through mesh : 1.3.5 | Stress | 14.3.5 | 28.2.2
Line Search : 15.3.3
Line through mesh : Stress | 14.3.5 | 28.2.2
Linear constraints : see Tyings
Linear static analysis : 2.2.1 | II.
LINES option
graph : 18.4.1
LIST option
polyline : 10.4.4 | 14.3.5
space curve : 7.1.2 | 20.1.5 | 38.1.4
time curve : 26.1.4
Load change : 32.3
Load combinations : 1.3.1
Load cycles to failure : 8.3.1
Load mask : 1.1.5
LOAD parameter : 17.3
buckling analysis : 16.2 | 19.2
Load-displacement trajectory : 18.4.1
LOADCASE option
results selection : 4.3.2 | 23.2
LOADCASES option
tabulation : 9.2.2 | 11.2.2 | 16.2.1 | 35.2.2
LOADFA parameter : 18.3
Loading : 1.1.5
labeling : 1.1.5 | 17.1.3 | 22.1.7 | 23.1.2
LOADS option : 4.1.2 | 4.1.4 | 5.5.1 | 23.1.2
deletion : 5.3 | 5.4.1 | 32.3
labeling : 5.2.1 | 17.1.3 | 23.1.2
'LOADS' table
linear static analysis : 3.3.1
phased analysis : 33.
remade : 31.3
stability analysis : 20.1.7
staggered analysis : 31.1
LOCAL option
extreme results : 36.3.2
results transformation : 20.3.2
LOCATE option : 5.4.3
Location points of reinforcement : 10.3.3
Logarithmic scale for graph : Graphs
lubric example : 28.
Lubrication : 28.
Lubrication analysis : 28.2
LUMPED option
transient heat flow : 27.2.1
M output
linear static analysis : 3.2.1
MAGNITUDE option
complex result : 9.3.1
Mass
added : 11.
Mass density : 4.1.3
Material properties
externally specified : 18.5
specification : 1.1.3
MATERIALS option
colored elements : 5.1.4 | 23.1.3
edge display : 15.2.2
MATRIX command
transient heat flow : 27.2.1
MAX option
graph : Postbuckling
MEASURE option : 37.2.2
mems example : 7.
Menu Bar : 1.1.1
Merge
mesh : 32.1.4
MERGE option
mesh : 32.1.4
Mesh display : The
Mesh generation : see Meshing
Mesh labeling : 3.1.3
MESH option
display : 4.1.4
shrunken view : 4.1.4 | 17.1.1 | 35.1
Mesh quality : 13.1.3 | 37.2.2
labeling : 1.1.2.2 | 12.1.4
Meshing : The
algorithm : 1.1.2.2
plane strain model : 15.1
plate bending model : 6.1
shell model : 20.1 | 22.1
spline elements : 21.1
tetrahedral automatic : 36.1.2.2
triangular automatic : 36.1.2.1
two-dimensional model : 12.1 | 23.1.2
MESHING command : 3.1.3 | 4.1.4 | 5.1.1 | 5.1.4 | 6.1.2 | 12.1.4 | 20.1.6 | 21.1.5 | 22.1.6 | 23.1.2 | 23.1.2 | 37.2.2
MIDDLE option : 38.2.2
MIDNODES option : 12.1.4
Midside nodes position : 12.1.4
MIN option
graph : Postbuckling
MINANG option : 1.1.2.2
Minimum Angle test
labeling : 12.1.4
MIRROR option
geometry copy : 1.1.2.4 | 15.1.1
transformation : 36.1.1.2
Mirror transformation : 36.1.1.2
Mirroring : 1.1.2.4 | 15.1.1 | 36.1.1.2
Mobile load : 5.4
Mobile load analysis : 5.
Modal response analysis : 9.4
Model Code material libraries : 38.1.5
MODEL command
eigenvalue analysis : 35.3
modal response analysis : 11.3.3
transient heat flow : 27.2.1
MODES command
buckling analysis : 18.3
postbuckling analysis : 21.4
MODESHAPE option : Animation.
MODULATE option
value colors : 5.3.1 | 5.5.4 | 15.2.2
vector colors : 23.2.2
Mohr-Coulomb plasticity : Plasticity.
Monitor : 2.3.1
extreme result : 7.4.2 | 21.2.1
results variation : 14.3.3
switch off : 21.1.6
MONITOR option : 7.1 | 21.1.6 | 29.1
Mooney-Rivlin hyperelasticity : 13.1.4
MOVE option : 11.1.2 | 15.1.4
MPC option : 13.1.5 | 15.1.3
Multi-point constraints : 13.1.5 | 15.1.3
Multiple viewports : 3.1.3 | 4.1.4 | 5.3.1 | 21.1.6 | 38.2.2
N output
linear static analysis : 3.2.1
NAFEMS benchmark
free vibration : 35.
heat transfer : 24. | 25.
nafet2 example : 25.
nafet4 example : 24.
NEN 6720 code : Cracking.
concrete : 38.1.5
Neutral file
plotting : 18.4.1
NEUTRAL option
plot file : 18.4.1
Newton-Raphson iteration
nonlinear analysis : 12.3 | Load-displacement
NFATIG command : 8.3.2
NMODES parameter
buckling analysis : 16.2 | 17.3 | 19.2
eigenvalue analysis : 11.2 | 35.2 | 35.3
NOCSHE input
plane stress elements : 7.2 | 14.2
NODAL option
results selection : 4.3.2 | 5.4.3 | 23.2.1
NODAL subtable of 'BOUNDA' : 25.1 | 27.1
Node numbers
labeling : 2.3.1 | 3.1.3
NODE option
graph : 18.4.1 | 21.4.1 | 22.3.1
NODES option
line : Stress | 14.3.5
polyline : 5.4.3
NonEla example : 40.
NONLIN command : 13.3
transient heat flow : 27.2.1
Nonlinear analysis : IV. | 13.3
dynamic : 10.6
heat flow : 31.4
user-supplied friction : 15.3.1
Nonlinear buckling : 16.1 | 18.5.2 | 20.4
Nonlinear elasticity : 40.
NORM command : 18.4 | 21.4
NORMAL option
loading : 8.1.4
NSTEPS parameter
postbuckling analysis : 18.4 | 21.4
NUMERIC option
color modulation : 5.3.1 | 5.5.4
numeric display : 5.3.1 | 5.5.4 | 7.2.4 | 14.3.2
Numerical values
results display : 2.3.3 | 5.5.4 | 7.2.4 | 14.3.2
NWOEHL input : 8.3.1
OBSERV subtable of 'TARGET' : 5.2.3.1
Observables : 5.2.3.1
OLD option
graph along line : Stress | Stress
ON-LINE option : 12.1.4
ONLINE option : 6.1.1
OPTIONS option
graph plotting : 18.4.1
results presentation : 18.4.1 | Postbuckling
viewing : 4.1.4
OUTLINE option
postprocessing : 36.3.1 | 37.3.1
preprocessing : 21.1.5 | 21.1.5
OUTPUT command
linear static analysis : 3.2
stability analysis : 16.2
Output selection : 2.2.2
OVERLAY option : Overlaid
P option : 28.1.4 | 29.1.2 | 30.1.2
P-ESTRAIN option : 31.3.1
P-STRESS option : 12.2.1 | 15.2.2 | 37.3.2
P1 option : 37.3.2
Parameter estimation : 5.2.3.3
Paving meshing : 1.1.2.3 | 11.1.2 | 14.1.2
PERSPECT option : 22.1.6
Perspective view : 22.1.6 | 38.1.1.1
Perturbation analysis : 18.3 | 21.4 | 22.3
displacements : 21.4.2 | 22.3.2
Phased analysis : VIII.
composed beam : 32.
linear : 33.
nonlinear : 34.2
tunnel section : 34.
PHYSIC command
nonlinear analysis : 12.3
PHYSICAL option
assignment : 3.1.2
beam display : 4.1.4 | 5.1.4
colored elements : 5.1.4 | 21.1.5
hidden view : 5.1.4
Physical properties
specification : 1.1.3
PINNED option : 4.1.2 | 6.1.1
Piola-Kirchhoff stress (2nd) : 13.3.2
PLANE option
shape : 20.1.1 | 38.1.1.2
Plane shape : 20.1.1 | 38.1.1.2
Plane strain elements : 40. | 42.1
fluid-structure interaction : 11.1
nonlinear analysis : 13. | 15.1.1
Plane stress elements : 37.3
contact analysis : 14.1
fatigue failure : 8.1.2
stress smoothing : 7.
user-supplied material failure : 12.5
PLASTI command : 12.3
Plasticity : 12.
postbuckling analysis : 18.5
Plasticity status : 12.3.3
Plate bending elements : The
free vibration : 35.1
linear static analysis : 6.1
plate example : 12.
PLOTFILE option
animation : 14.3.4
writing : 18.4.1
Point : 1.1.2.1
POINT option : 4.1.1
POINT-ID option
graph : 10.6.6
POINTS option
graph : Graphs | 18.4.1
Poisson's ratio
linear elasticity : 4.1.3 | 5.1.2 | 36.1.3
Polystyrene foam : 23.
Portable Network Graphics format : 1.3.4
POSTBU option : 18.4 | 21.4
Postbuckling
load factor : 18.4.2
Postbuckling analysis : 18. | 21.4 | 22.3
Potential flow analysis : VI.
Predefined shapes for beam elements : 1.1.3 | 2.1.3 | 4.1.3 | 5.1.2
Prefab concrete
heat flow : 23.
prefab example : 23.
Prescribed displacements : 4.1.2
PRESENT command : 3.2.2 | 4.3.2 | 5.5.3 | 16.2.1 | 23.2.1
Pressure : 1.1.5
lubrication analysis : 28.2.2
PRESSURE load class : 1.1.5 | 4.1.2 | 7.1.2 | 8.1.4 | 15.1.3 | 17.1.3 | 22.1.5 | 37.2.3
PRESTRES load class
optimization analysis : 5.2.1
Prestress
optimization : 5.2 | 5.2
PRGERR subroutine : 12.5.2.1 | 15.3.2.1
Principal stress : 12.2.1 | 15.2.2 | 37.3.2
PROPERTY command : 4.1.2 | 5.1.3
Property Manager : 1.1.3
Property Manager dialog : 2.1.3
PT1CR element : 8.1.2
PTE output
heat flow : 24.2.1 | 25.2.1 | Numerical
lubrication analysis : 28.2.1
Q12PL element : The
linear static analysis : 6.1
Q20SH element
stability analysis : 20.1
Q48SPL element : 21.1
Q4HT element
staggered analysis : 31.2.1
steady-state flow analysis : 23.1.2 | 25.1
transient heat flow : 26.1
Q4TO element : 29.1.2
Q56SPL element : 18.1
Q8EPS element
nonlinear analysis : 15.1.1
Q8MEM element : 37.3
contact analysis : 14.1
stress smoothing : 7.1
QU elements
cross-section : 30.1.2
lubrication : 28.1.2
structural : The | 13.1.3 | 20.1.6 | 22.1.6
Quadrilateral meshing : 37.2.2
QUALITY option : 1.1.2.2 | 12.1.4 | 37.2.2
color modulation : 12.1.4
QUICK option
local axes display : 6.3
RAB subroutine : 12.5.2.3 | 15.3.2.3
Radiation : 25.
RANGE option
results selection : 7.4.3 | 10.6.6 | 36.3.2 | 38.2.2
Rate of flow : see Discharge
Rate-dependent elasticity : 41.
Rayleigh damping : see Damping
RBEAM option : 13.1.5 | 15.1.3
RdepEla example : 41.
READ command : 13.2 | 22.2
READ option : 37.1
Reading Input dialog : 2.2.1
RECOVER option
drawing : Overlaid
RECTANGUL option
coordinate system : Local
REDUCE command
postbuckling analysis : 18.3 | 21.4 | 22.3
REGION option
meshing algorithm : 1.1.2.3
surface definition : 11.1.1 | 14.1.1 | 23.1.1 | 36.1.1.1 | 37.2.2
Regular Newton-Raphson iteration
nonlinear buckling : 20.4
transient heat flow : 26.2
Reinforcement
nonlinear analysis : 10.
REMAKE command : 32.3
staggered analysis : 31.3
Remaking input : 32.3
REMOVE option
geometric part : 37.2.2
RESPON command
modal response analysis : 11.3.1
Response analysis : 9.3
RESULTS command : 4.3.1 | 23.2 | 33.1
Results environment : 1.2
RESULTS option
graph : 12.3.2 | Load-displacement
Results Selection dialog : 2.2.2
Return-mapping : 12.5.1
*REYNOL command : 28.2
Reynolds flow : see Lubrication
Rigid Beam MPC : 13.1.5 | 15.1.3
Rigid body modes : 35.2.2
RMOVE subroutine : 12.5.2.3 | 15.3.2.3
RO input
structural analysis : 33.10
Rock : 15.
rodht example : 26.
ROTATE option
viewing : 4.1.1 | 5.1.4 | 20.1.1 | 21.1.1
RSET subroutine : 15.3.2.5
Rubber : see Hyperelasticity
vulcanization : see Vulcanization
RX option : 21.1.4
S output
linear static analysis : 7.2.1
SAVE command : 12.1.5
SAVE option
drawing : 18.4.1
SCURVE option : 7.1.2 | 20.1.5 | 28.1.3 | 38.1.4
graph : 20.1.5
SECMOD option : 18.3
SECOND option : 12.3
Select Analysis Type dialog : 2.2.1
Set : 1.1.2.5 | 5.1.1 | 6.1.1 | 14.1.1 | 22.1.4 | 23.1.1
SET option : 1.1.2.5 | 4.1.1 | 5.1.1 | 6.1.1 | 22.1.4 | 23.1.1
SETUP option
multiple viewport : 21.1.6
SHADE option : 4.1.4 | 5.1.4 | 20.1.6 | 20.3.2 | 22.1.6 | 36.1.2.1
Shaded view : 4.1.4 | 5.1.4 | 36.1.2.1
Shape : 20.1.1 | 36.1.1
display : 20.1.1
labeling : 20.1.1
SHAPE option : 20.1.1 | 36.1.1.1
deformation : 3.2.2 | 4.3.2 | 5.5.3 | 16.2.1 | 36.3.1
display : 20.1.1
labeling : 20.1.1
surface : Correcting
Shear retention : Cracking.
Shear stress : 29.2.2 | 30.2.2
Shell elements : 34.1.3
curved : 38.1.2
interfaces : 38.
stability analysis : 17.1 | 20.1 | 22.1
shell example : 20.
Shift
eigenvalues : 35.2
SHIFT parameter
buckling analysis : 21.3 | 22.2
eigenvalue analysis : 35.2
SHRINK option : 4.1.4 | 5.1.4 | 11.1.2 | 22.1.6 | 23.1.2
Shrunken elements view : The | 1.1.2.5 | 3.1.3 | 4.1.4 | 5.1.4 | 17.1.1 | 22.1.6 | 23.1.2 | 35.1
SIGDIS input : 38.1.5
SIGNIF option : Postbuckling
SIZE option
workbox : 7.1 | 13.1 | 23.1 | 29.1
SIZE parameter : 18.4 | 21.4
SIZES command
transient heat flow : 26.2 | 27.2.1
skewpl example : 6.
SMOOTH option : 7.3
Smoothing
stress output : 7.
Solid elements : 36.1.2.2
Solid model : 36.1.2.2
cutaway view : 36.3.2
solidi example : 27.
Solidification : 27.
Solution methods : IX.
SOLVE command
linear static analysis : 3.3.2
SP elements : 18.1.1 | 21.1.5
SP1TR element
transient nonlinear analysis : 10.3
Space curve : 28.1.3
graph : 7.1.2 | 20.1.5
load : 7.1.2 | 20.1.5 | 38.1.4
local coordinate system : 38.1.4
SPACE option : 14.1.1 | 28.1.1
*SPECTR command : 9.5.2
Spectral response analysis : 9.5
Spherical Path : 20.4
splin example : 18.
Spline elements : 18.1 | 21.1
SPLIT option : 1.1.2.2 | 32.1.3
Spring stiffness : 10.3.2
sqdisc example : 14.
sqtube example : 22.
SRSS rule : 9.5.4
STABIL command : 16.2 | 19.2
Stability analysis : V.
Euler buckling : 16.2 | 17. | 22.2
nonlinear buckling : 19. | 20.
postbuckling : 18. | 21.4 | 22.3
STACK option : Stress | Stress | 14.3.5
Staggered analysis
heat transfer : 31.
Standard output file : 2.2.3
buckling values : 20.3.1 | 21.3.1 | 22.2.1
cross-section properties : 29.2.1 | 30.2.1
eigenfrequencies : 10.5.3 | 35.2.1
estimation report : 5.2.3.3
log lines : 10.6.5 | 12.3 | Convergence.
total mass : 35.2.1
START command
postbuckling analysis : 18.4
Status : 12.3.3
Status variables
user-defined : 15.3.7
Stay optimization : 5.2
Steady-state flow analysis : 23.
linear : 24.2 | 31.2
nonlinear : 25.2 | 31.4
Steady-state heat flow : 23.2 | 24.2
Stefan problem : 27.
Stefan-Boltzmann constant : Radiation.
STEPS command : 18.4
STEPS option : Animation.
Stick-slip : 15.3.2.6
STOP command : 28.2
Straight line : 23.1.1
STRAIGHT option
line definition : 11.1.1 | 23.1.1
Strain path : 42.5
Stress
linear static analysis : 37.3.2
nonlinear analysis : 15.2.2
STRESS command
linear static analysis : 37.3
Structural analysis : 4.1
loading : 4.1.2
SUPERP command : 33.2
'SUPPOR' table
phased analysis : 33.
staggered analysis : 31.1
Supports : 1.1.4 | 20.1.4
graphic display : 1.1.4 | 5.1.4 | 17.1.3
removal : 33.
Surface : The
SURFACE option : 38.1.1.3
division : 6.1.2
results : 38.2.2
space curve : 28.1.3
SURFACES option
labeling : 29.1.1
SWAP option : 18.4.1
SWEEP option : 13.1.1 | 21.1.2 | 22.1.2 | 26.1.1 | 36.1.1.3
Sweeping parts : 13.1.1 | 21.1.2 | 22.1.2 | 26.1.1 | 34.1.1.1 | 34.1.1.2
SWOEHL input : 8.3.1
SYMBOL option
results presentation : 4.3.2
Symbols for results presentation : 4.3.2
SYMBOLS option
graph : Graphs | 18.4.1
Symbols, glossary of : Glossary
Symmetry : Symmetry | Symmetry.
t2le example : 31.
T6EPS element
nonlinear analysis : 15.1.1
T9PLA element : 1.1.2.2
Tabbed Output : 1.3.1 | 2.3
Table input : 16.1 | 27.1
TABULA output device
linear static analysis : 3.2.1
transient heat flow : 26.2 | 27.2.1
Tabular output
linear static analysis : 3.2.1 | 7.2.1 | 19.1
lubrication analysis : 28.2.1
phased analysis : 32.2.1 | 32.3.1
stability analysis : 16.2
transient flow analysis : 27.2.1
transient heat flow : 26.2 | Solidification
transient nonlinear analysis : 40.1.5
TABULATE option : 11.2.2
buckling modes : 16.2.1
eigenmodes : 9.2.2 | 35.2.2
load cases : 1.3.1
Tabulation tab : 1.3.1 | 2.3
TAKE command : 12.5.4
Tapered thickness : 28.1 | 28.1.3
Target data
loads optimization : 5.2.3.1
'TARGET' table
loads optimization : 5.2.3.1
tbeam example : 21.
TCURVE option : 26.1.4
graph : 26.1.4
TD output : 19.3
TE elements
structural : 36.1.2.2
TE12L element : 36.1.2.2
TEMPER command
steady-state heat flow : 25.2
transient heat flow : 27.2.1
TEMPER input
heat flow : 25.1 | 26.1.3
solidification : 27.1
Temperature analysis
linear steady-state : 23. | 31.2
Temperature load
staggered analysis : 31.3 | 31.5
tensil example : 36.
Tensile strength
concrete : Cracking.
Tensile test specimen : 36.
Tension softening : Cracking.
Thermoelastic analysis : 40.2
THICK option
line thickness : 18.4.1
Thickness
curved shell : 34.1.5
curved shell elements : 20.1.3
plate bending elements : 1.1.3 | 17.1.2 | 35.1
THREE-HORIZ option : 21.1.6 | 38.2.2
THREE-VERT option : 4.1.4
THROUGH option : 28.2.2
graph : 5.4.3 | Stress
Time curve : 26.1.4
graph : 26.1.4
Time steps
nonlinear analysis : 10.6.4
Time-load diagram
nonlinear analysis : 10.6.3
'TIMEBO' table : 27.1
'TIMELO' table
nonlinear analysis : 10.6.3 | 41.1.1
TO option
contour plot : 12.3.3
TOP option
multi-surface results : 38.2.2
TR elements
structural : 1.1.2.2
TRANSFORM option
results : 20.3.2
Transformation
displacements : 20.3.2
TRANSFRM option : 36.1.1.2
Transient analysis
nonlinear : 10.6 | IV.
Transient flow analysis
nonlinear : 26.2 | 27.2
TRANSLATE option
geometry sweep : 21.1.2 | 22.1.2 | 36.1.1.3
Translation transformation : The
Triangular meshing : 36.1.2.1
TRUNCATE option
cylinder : 20.1.1
Truss elements
linear static analysis : 4.1
mobile load analysis : 5.1
stability analysis : 16.1
viscous material : 41.
Tunnel
phased analysis : 34.
Tunnel lining : 38.
TunSec example : 34.
tunseg example : 38.
TWO-HORIZ option : 5.3.1 | 5.4.3
TWO-VERT option : 4.1.4
Tyings
flat plane : 22.1.8
skew symmetry : Symmetry
'TYINGS' table : Symmetry | 22.1.8
phased analysis : 33.
TYPE command
nonlinear analysis : 12.3
TYPES option
element meshing : 3.1.3 | 4.1.4 | 12.1.4 | 13.1.3 | 23.1.2
Units : 12.1 | 13.1 | 15.1 | 17.1 | 23.1
UNIX
user-suplied subroutines : 39.1
USE option : 4.1.4
User-supplied subroutines : 12.5 | 39.
Coulomb friction : 15.3.1
damage : 42.
nonlinear elasticity : 40.
rate-dependent elasticity : 41.1.2
Von Mises material : 12.5
USING option : 20.3.2 | 21.2.2
USRIFC user-supplied subroutine : 15. | 15.3.2
USRMAT user-supplied subroutine : 12.5.2 | 41.1.2 | 42.2
USRSTA input
user-supplied material : 12.5.3
USRVAL input
user-supplied material : 12.5.3 | 41.1.1
UTILITY command : 3.2
UV subroutine : 12.5.2.5
UVMW subroutine : 12.5.2.3 | 15.3.2.3
UVPW subroutine : 12.5.2.3 | 15.3.2.3
UVPWS subroutine : 12.5.2.4
UVS subroutine : 12.5.2.3 | 15.3.2.5
VALUES option
contour plot : Solidification
results : 7.4.3
Vector plots : 12.3.4
flux : 23.2.2 | 24.2.2
principal stress : 12.2.1 | 37.3.2
VECTORS option : 12.2.1 | 24.2.2 | 37.3.2
color and style : 15.2.2 | 23.2.2
Velocity
frequency response analysis : 9.3.2
lubrication : 28.1.4
VELOCITY load class : 28.1.4
Vibration mode : 35.3.1
VIEW command
color option : 23.1.3
mesh : 3.1.1 | 5.1.4 | 20.1.6 | 21.1.5
shrink option : 3.1.3 | 4.1.4 | 23.1.2
Viewport control : 3.1.3 | 21.1.6
VIEWPORT option : 3.1.3 | 4.1.4 | 5.5.4
viplate example : 35.
Viscosity
dynamic : 28.1.3 | 41.1.1
Viscous damping : 41.
VONMISES option : 4.3.2 | 12.2.1 | 14.3.3 | 37.3.2
Von Mises plasticity : 12.
postbuckling analysis : 18.5
user-supplied : 12.5
Von Mises strain
nonlinear analysis : 12.3.3
Von Mises stress
contour plot : 14.3.3 | 37.3.2
linear static analysis : 12.2.1
nonlinear analysis : 12.3.4
symbol plot : 4.3.2
VOSB code : 5.5.1
wallst example : 11.
wedge example : 15.
Weight load : 1.1.5
structural analysis : 3.3 | 4.1.2
WEIGHT subtable of 'LOADS' : 3.3.1
WHITE option : 11.1.1 | 21.1.2
Windows (MS-)
user-supplied subroutines : 39.2
Wöhler diagram : 8.3
WORK-BOX option : 7.1 | 13.1 | 14.1.1 | 23.1 | 28.1.1 | 29.1
Workbox
framing : 38.1.1.1
Working directory : 1.1.1
WRITE option : 1.1.6 | 3.2
X option
boundary conditions : 12.1.3 | 21.1.4
plane : 38.1.1.2
XSECTION option
extreme results : 36.3.2
model view : 36.3.2
XSYMM option : 22.1.4
Y option
boundary conditions : 12.1.3 | 21.1.4
plane : 38.1.1.2
Yielding, metal : 12.
YLINEAR option : Graphs
YLOG option : Graphs
Young's modulus
isotropic : 4.1.3 | 5.1.2 | 36.1.3
YSYMM option : 20.1.4 | 22.1.4
Z option
boundary conditions : 21.1.4
plane : 38.1.1.2
Zone in beam element : 32.1.2
ZOOM option : 20.1.7 | 21.1.6

DIANA-9.3 User's Manual - Analysis Examples
First ed.

Copyright (c) 2008 by TNO DIANA BV.