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Name: Analysis Data
Status: Current
Owner: Simulation
Revision Date: 3-OCT-1994
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Record 1: FORMAT(1I10)
Field 1 -- Analysis dataset label
Record 2: FORMAT(40A2)
Field 1 -- Analysis dataset name
Record 3: FORMAT (1I10)
Field 1: -- Dataset location
1: Data at nodes
2: Data on elements
3: Data at nodes on elements
5: Data at points
Record 4: FORMAT (40A2)
Field 1: -- ID line 1
Record 5: FORMAT (40A2)
Field 1: -- ID line 2
Record 6: FORMAT (40A2)
Field 1: -- ID line 3
Record 7: FORMAT (40A2)
Field 1: -- ID line 4
Record 8: FORMAT (40A2)
Field 1: -- ID line 5
Record 9: FORMAT (6I10)
Field 1: -- Model type
0: Unknown
1: Structural
2: Heat transfer
3: Fluid flow
Field 2: -- Analysis type
0: Unknown
1: Static
2: Normal mode
3: Complex eigenvalue first order
4: Transient
5: Frequency response
6: Buckling
7: Complex eigenvalue second order
9: Static non-linear
10: Craig-Bampton constraint modes
11: Equivalent attachment modes
12: Effective mass modes
13: Effective mass matrix
14: Effective mass matrix
Field 3: -- Data characteristic
0: Unknown
1: Scalar
2: 3 DOF global translation vector
3: 6 DOF global translation & rotation
vector
4: Symmetric global tensor
6: Stress resultants
Field 4: -- Result type
2:Stress
3:Strain
4:Element Force
5:Temperature
6:Heat Flux
7:Strain Energy
8:Displacement
9:Reaction Force
10:Kinetic Energy
11:Velocity
12:Acceleration
13:Strain Energy Density
14:Kinetic Energy Density
15:Hydrostatic Pressure
16:Heat Gradient
17:Code Check Value
18:Coefficient of Pressure
19:Ply Stress
20:Ply Strain
21:Failure Index for Ply
22:Failure Index for Bonding
23:Reaction Heat Flow
24:Stress Error Density
25:Stress Variation
27:Element Stress Resultant
28:Length
29:Area
30:Volume
31:Mass
32:Constraint Force
34:Plastic Strain
35:Creep Strain
36:Strain Energy Error Norm
37:Dynamic Stress At Nodes
38:Heat Transfer Coefficient
39:Temperature Gradient
40:Kinetic Energy Dissipation Rate
41:Strain Energy Error
42:Mass Flow
43:Mass Flux
44:Heat Flow
45:View Factor
46:Heat Load
47:Stress Component
48:Green Strain
49:Contact Forces
50:Contact Pressure
51:Contact Stress
52:Contact Friction Stress
53:Velocity Component
54:Heat Flux Component
55:Infrared Heat Flux
56:Diffuse Solar Heat Flux
57:Collimated Solar Heat Flux
58:Safety Factor
59:Fatigue Damage
60:Fatigue Damage With Direction
61:Fatigue Life
62:Quality Index
94:Unknown Scalar
95:Unknown 3DOF Vector
96:Unknown 6DOF Vector
97:Unknown Symmetric Tensor
98:Unknown General Tensor
99:Unknown Stress Resultant
101:Gap Thickness
102:Solid Layer (+ surface)
103:Solid Layer (- surface)
104:Total Solid Layer
105:Flow Vector at Fill
106:Bulk Flow Vector
107:Core Displacement
108:Layered Shear Strain Rate
109:Shear Stress
110:Heat Flux (+ surface)
111:Heat Flux (- surface)
112:Layered Temperature
113:Bulk Temperature
114:Peak Temperature
115:Temperature at Fill
116:Mass Density
117:Pressure
118:Volumetric Skrinkage
119:Filling Time
120:Ejection Time
121:No-flow Time
122:Weld Line Meeting Angle
123:Weld Line Underflow
124:Original Runner Diameter
125:Optimized Runner Diameter
126:Change in Runner Diameter
127:Averaged Layered Cure
128:Layered Cure
129:Cure Rate
130:Cure Time
131:Induction Time
132:Temperature at Cure
133:Percent Gelation
134:Part Heat Flux (+ surface)
135:Part Heat Flux (- surface)
136:Part-Wall Temperature (+ surface)
137:Part-Wall Temperature (- surface)
138:Part Ejection Time
139:Part Peak Temperature
140:Part Average Temperature
141:Parting Temperature (+ surface)
142:Parting Temperature (- surface)
143:Parting Heat Flux (- surface)
144:Parting Heat Flux (+ surface)
145:Wall Temperature Convergence
146:Wall Temperature (- surface)
147:Wall Temperature (+ surface)
148:Line Heat Flux
149:Line Pressure
150:Reynold's Number
151:Line Film Coefficient
152:Line Temperature
153:Line Bulk Temperature
154:Mold Temperature
155:Mold Heat Flux
156:Rod Heater Temperature
157:Rod Heater Flux
158:Original Line Diameter
159:Optimized Line Diameter
160:Change in Line Diameter
161:Air Traps
162:Weld Lines
163:Injection Growth
164:Temp Diff (Celcius)
165:Shear Rate
166:Viscosity
167:Percentage
168:Time
169:Flow Direction
170:Speed
171:Flow Rate
172:Thickness Ratio
301:Sound Pressure
302:Sound Power
303:Sound Intensity
304:Sound Energy
305:Sound Energy Density
>1000: User defined result type
Field 5: -- Data type
1: Integer
2: Single precision floating point
4: Double precision floating point
5: Single precision complex
6: Double precision complex
Field 6: -- Number of data values for the data
component (NVALDC)
Record 10: FORMAT (8I10)
Field 1: -- Integer analysis type specific data (1-8)
Record 11: FORMAT (8I10)
Field 1: -- Integer analysis type specific data (9,10)
Record 12: FORMAT (6E13.5)
Field 1: -- Real analysis type specific data (1-6)
Record 13: FORMAT (6E13.5)
Field 1: -- Real analysis type specific data (7-12)
Note: See chart below for specific analysis type information.
Dataset class: Data at nodes
Record 14: FORMAT (I10)
Field 1: -- Node number
Record 15: FORMAT (6E13.5)
Fields 1-N: -- Data at this node (NDVAL real or complex
values)
Note: Records 14 and 15 are repeated for each node.
Dataset class: Data at elements
Record 14: FORMAT (2I10)
Field 1: -- Element number
Field 2: -- Number Of data values For this element(NDVAL)
Record 15: FORMAT (6E13.5)
Fields 1-N: -- Data on element(NDVAL Real Or Complex Values)
Note: Records 14 and 15 are repeated for all elements.
Dataset class: Data at nodes on elements
RECORD 14: FORMAT (4I10)
Field 1: -- Element number
Field 2: -- Data expansion code (IEXP)
1: Data present for all nodes
2: Data present for only 1st node -All other
nodes the same.
Field 3: -- Number of nodes on elements (NLOCS)
Field 4: -- Number of data values per node (NVLOC)
RECORD 15: FORMAT (6E13.5)
Fields 1-N: -- Data Values At Node 1 (NVLOC Real Or
Complex Values)
Note: Records 14 And 15 Are repeated For each Element.
For Iexp = 1 Record 15 Is repeated NLOCS Times
For Iexp = 2 Record 15 appears once
Dataset class: Data at points
RECORD 14: FORMAT (5I10)
Field 1: -- Element number
Field 2: -- Data expansion code (IEXP)
1: Data present for all points
2: Data present for only 1st point -All other
points the same.
Field 3: -- Number of points on elements (NLOCS)
Field 4: -- Number of data values per point (NVLOC)
Field 5: -- Element order
RECORD 15: FORMAT (6E13.5)
Fields 1-N: -- Data Values At point 1 (NVLOC Real Or
Complex Values)
Note: Records 14 And 15 Are repeated For each Element.
For Iexp = 1 Record 15 Is repeated NLOC Times
For Iexp = 2 Record 15 appears once
Notes: 1. ID lines may not be blank. If no information
is required, the word "NONE" must appear in
columns 1-4.
2. The data is store in
"node-layer-data charateristic" format.
Loc1 layer1 component1, Loc1 layer1 component2, ...
Loc1 layer1 componentN, Loc1 layer2 component1, ...
Loc1 Layer2 componentN, ...Loc1 layerN componentN
Loc2 layer1 component1, ...Loc2 layerN componentN
LocN layer1 component1, ...LocN layerN componentN
3. For complex data there Will Be 2*NDVAL data items. The
order is real part for value 1, imaginary part for
value 1, real part for value 2, imaginary part for
value 2, etc.
4. The order of values for various data
characteristics is:
3 DOF Global Vector: X, Y, Z
6 DOF Global Vector: X, Y, Z, Rx, Ry, Rz
Symmetric Global Tensor: Sxx, Sxy, Syy,
Sxz, Syz, Szz
Shell and Plate Element Resultant: Fx, Fy, Fxy,
Mx, My, Mxy,
Vx, Vy
5. ID line 1 always appears on plots in output
display.
6. If result type is an "UNKNOWN" type, id line 2
is displayed as data type in output display.
7. Data Characteristic values (Record 9, Field 3)
imply the following values Of NDVALDC (Record 9,
Field 6)
Scalar: 1
3 DOF Global Vector: 3
6 DOF Global Vector: 6
Symmetric Global Tensor: 6
General Global Tensor: 9
Shell and Plate Resultant:8
Since this value can also be derived from the Results
Type (Record 9, Field 4), this is redundant data, and
should be kept consistent. Some data was kept for
compatibility with older files.
8. No entry is NOT the same as a 0. entry: all 0s must
be specified.
9. A direct result of 8 is that if no records 14 and
15 appear for a node or element, this entity has
no data and will not be contoured, etc.
10. Dataloaders use the following id line convention:
1. (80A1) MODEL IDENTIFICATION
2. (80A1) RUN IDENTIFICATION
3. (80A1) RUN DATE/TIME
4. (80A1) LOAD CASE NAME
For static:
5. (17H LOAD CASE NUMBER;, I10)
For normal mode:
5. (10H MODE SAME, I10, 10H FREQUENCY, E13.5)
11. For situations with reduced # DOF'S, use 6 DOF
translation and rotation with unused values = 0.
12. The integer associated data "number retained" will
=0 unless the result set is created by sorting for
extremes. The maximum number of values to retain is 6.
Specifed values:
NDVAL - Number of data values for the element.
NLOCS - Number of location on the element data is stored for.
NVALDC - Number of values for the data component.
Derived values:
NLAY - Number of location through the thickness data is stored for
= NDVAL / ( NLOCS * NDVALC)
NVLOC - Number of values per location.
= NLAY * NVALDC
The following is always true:
NDVAL = NLOCS * NLAY * NVALDC
Dataset class: Data at nodes
1. NLOCS = 1
NLAY = 1
NDVAL = NVALDC
2. Typical fortran I/O statements for the data
sections are:
READ(LUN,1000)NUM
WRITE
1000 FORMAT (I10)
READ(LUN,1010) (VAL(I),I=1,NDVAL)
WRITE
1010 FORMAT (6E13.5)
Where: VAL is real or complex data array
NUM is element number
Dataset class: Data at elements
1. Data on 2D type elements may have multiple values
through the element thickness. In these cases:
NLOCS =1
NLAY =Number of layers of data through the thickness.
NDVAL = NLAY * NVALDC
For solid elements:
NLOCS = 1
NLAY = 1
NDVAL = NVALDC
The order of the nodes defines an outward normal which
specifies the order from position 1 to NPOS.
2. Maximum Value For NVALDC Is 9.
No Maximum Value For NDVAL.
No Maximum Value For NLAY.
3. Typical fortran I/O statements for the data
sections are:
READ (LUN, 1000) NUM, NDVAL
WRITE
1000 FORMAT (2I10)
READ (LUN, 1010) (VAL(I),I=1,NDVAL)
WRITE
1010 FORMAT (6E13.5)
Where: VAL is real or complex data array
NUM is element number
Dataset class: Data at nodes on elements
1. Data on 2D type elements may have multiple values
through the element thickness. In these cases:
NLOCS =Number of nodes for the element.
NLAY =Number of layers of data through the thickness.
NDVAL = NLOCS * NLAY * NVALDC
For solid elements:
NLOCS = Number of nodes for the element.
NLAY = 1
NDVAL = NLOCS * NVALDC
The order of the nodes defines an outward normal which
specifies the order from position 1 to NPOS.
2. Maximum Value For NVALDC Is 9.
No Maximum Value For NDVAL.
No Maximum Value For NLAY.
3. Typical Fortran I/O statements for the data sections
are:
READ (LUN,1000) NUM, IEXP, NLOCS, NVLOC
WRITE
1000 FORMAT (4I10)
C
C Process Expansion Code 1
C
IF (IEXP.NE.1) GO TO 20
NSTRT = 1
DO 10 I=1, NLOCS
NSTOP = NSTRT + NVLOC - 1
READ (LUN,1010) (VAL(J),J=NSTRT,STOP)
WRITE
1010 FORMAT (6E13.5)
NSTRT = NSTRT + NVLOC
10 CONTINUE
GO TO 50
C
C PROCESS EXPANSION CODE 2
C
20 READ (LUN,1010) (VAL(I),I=1,NVLOC)
NOFF = 0
DO 40 I=1,NLOCS
NOFF = NOFF +NVLOC
DO 30 J=1, NVLOC
VAL (NOFF+J) = VAL(J)
30 CONTINUE
40 CONTINUE
C
50 NDVAL = NVLOC*NLOCS
Where: NUM is element number.
IEXP is the element expansion code
VAL is real or complex data array.
Dataset class: Data at points
1. Only Tetrahedral elements will be supported.
2. For solid elements:
NLOCS = Number of points on the element data is stored
for. Determined from the element type and
order.
NLAY = 1
NDVAL = NLOCS * NVALDC
3. Maximum Value For NVALDC Is 9.
No Maximum Value For NDVAL.
4. The element order is equal to the P-order of the element
5. The number of points per element is calculated from
the element order as follows:
Number_of_Points = sum(i= 1 to P-Order+1)
[sum(j = 1 to i)[1 + i - j) )]]
6. Typical Fortran I/O statements for the data sections
are:
READ (LUN,1000) NUM, IEXP, NLOCS, NVLOC, IORDER
WRITE
1000 FORMAT (4I10)
.
.
.
(See 3. for Data at Nodes on Elements)
Analysis Type
S
t
a
C C t
o F o i
N m r m c
o p e p
r l q l N
m e T e o
a x r R B x n
U l a e u
n S E n s c E L
k t M i s p k i i
n a o g i o l g n
o t d e e n i e e
w i e n n s n n a
n c s 1 t e g 2 r
Design set ID X X X X X X X X X
Iteration number X X
Solution set ID X X X X X X X X X
I
N Boundary condition X X X X X X X X X
T
E Load set X X X X X X
G
E Mode number X X X X
R
Time step number X X
Frequency number X
Creation option X X X X X X X X X
Number retained X X X X X X X X X
Time X X
Frequency X X
Eigenvalue X
Modal Mass X
Viscous damping ratio X
Hysteretic damping ratio X
R Real part eigenvalue X X
E
A Imaginary part eingenvalue X X
L
Real part of modal A X
Real part of mass X
Imaginary part of modal A X
Imaginary part of mas X
Real part of modal B X
Real part of stiffnes X
Imaginary part of modal B X
Imaginary part of stiffness X
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(c) 2000 Structural Dynamics Research Corporation