1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
|
*DECK TRIDFH
SUBROUTINE TRIDFH (ISPLH,IPTRK,IDIM,LX,LZ,LL4,NUN,SIDE,ZZZ,ZZ,
1 KN,QFR,IQFR,VOL,MAT,IDL,NCODE,ICODE,ZCODE,IMPX)
*
*-----------------------------------------------------------------------
*
*Purpose:
* Numbering corresponding to a mesh centered finite difference
* discretization of a 3-D hexagonal geometry.
*
*Copyright:
* Copyright (C) 2002 Ecole Polytechnique de Montreal
* This library is free software; you can redistribute it and/or
* modify it under the terms of the GNU Lesser General Public
* License as published by the Free Software Foundation; either
* version 2.1 of the License, or (at your option) any later version
*
*Author(s): A. Benaboud
*
*Parameters: input
* IMPX print parameter.
* ISPLH type of mesh-splitting: =1 for complete hexagons; =2 for
* triangular mesh-splitting.
* IPTRK L_TRACK pointer to the tracking information.
* IDIM number of dimensions (2 or 3).
* LX number of hexagons.
* LZ number of axial planes.
* SIDE side of an hexagon.
* ZZZ Z-coordinates of the axial planes.
* NCODE type of boundary condition applied on each side (I=1: hbc):
* NCODE(I)=1: VOID; =2: REFL; =6: ALBE;
* =5: SYME; =7: ZERO.
* ICODE physical albedo index on each side of the domain.
* ZCODE albedo corresponding to boundary condition 'VOID' on each
* side (ZCODE(I)=0.0 by default).
* MAT mixture index assigned to each element.
*
*Parameters: output
* LL4 order of the system matrices.
* NUN number of unknowns per energy group.
* VOL volume of each element.
* KN element-ordered unknown list.
* QFR element-ordered boundary conditions.
* IQFR element-ordered physical albedo indices.
* IDL position of the average flux component associated with each
* volume.
* ZZ Z-sides of each hexagon.
*
*-----------------------------------------------------------------------
*
USE GANLIB
*----
* SUBROUTINE ARGUMENTS
*----
TYPE(C_PTR) IPTRK
INTEGER ISPLH,IDIM,LX,LZ,LL4,NUN,KN(8*LX*LZ),IQFR(8*LX*LZ),
1 MAT(LX*LZ),IDL(LX*LZ),NCODE(6),ICODE(6),IMPX
REAL SIDE,ZZZ(LZ+1),ZZ(LX*LZ),QFR(8*LX*LZ),VOL(LX*LZ),ZCODE(6)
*----
* LOCAL VARIABLES
*----
LOGICAL LL1,LL2
INTEGER, DIMENSION(:), ALLOCATABLE :: I1,KN1,KN2,KN3,KN4
ALB(X)=0.5*(1.0-X)/(1.0+X)
*----
* MAIN LOOP OVER THE FINITE ELEMENTS
*----
ALLOCATE(I1(LX*LZ),KN4(8*LX*LZ))
MEL=0
DO 10 KXZ=1,LX*LZ
I1(KXZ) = 0
IF(MAT(KXZ).LE.0) GO TO 10
MEL=MEL+1
I1(KXZ) = MEL
10 CONTINUE
IDEB = 0
IFIN = 0
IVAL=0
NUM1=0
MEL = MEL/LZ
KEL =0
DO 45 KZ=1,LZ
LL1 = .FALSE.
LL2 = .FALSE.
DO 40 KX=1,LX
KEL = KEL + 1
ZZ(KEL) = 0.0
IF(MAT(KEL).LE.0) GO TO 40
ZZ(KEL) = ZZZ(KZ+1)-ZZZ(KZ)
DO 20 IC=1,8
QFR(NUM1+IC) = 0.0
IQFR(NUM1+IC) = 0
20 CONTINUE
DO 30 IX=1,6
KN4(NUM1+IX) = 0
N1 = NEIGHB (KX,IX,9,LX,POIDS)
IF(N1.GT.0) N1 = N1+(KZ-1)*LX
IF(N1.GT.(LX+(KZ-1)*LX)) THEN
IF((NCODE(1).EQ.1).AND.(ICODE(1).EQ.0)) THEN
N1 = -1
QFR(NUM1+IX)=ALB(ZCODE(1))
ELSE IF(NCODE(1).EQ.1) THEN
N1 = -1
QFR(NUM1+IX)=1.0
IQFR(NUM1+IX)=ICODE(1)
ELSE IF(NCODE(1).EQ.2) THEN
N1 = -2
ELSE IF(NCODE(1).EQ.7) THEN
N1 = -3
ENDIF
ELSE IF(MAT(N1).LE.0) THEN
IF((NCODE(1).EQ.1).AND.(ICODE(1).EQ.0)) THEN
N1 = -1
QFR(NUM1+IX)=ALB(ZCODE(1))
ELSE IF(NCODE(1).EQ.1) THEN
N1 = -1
QFR(NUM1+IX)=1.0
IQFR(NUM1+IX)=ICODE(1)
ELSE IF(NCODE(1).EQ.2) THEN
N1 = -2
ELSE IF(NCODE(1).EQ.7) THEN
N1 = -3
ENDIF
ENDIF
IF(N1.GT.0) N1 = I1(N1)
KN4(NUM1+IX) = N1
30 CONTINUE
KK7 = I1(KEL) - MEL
KK8 = I1(KEL) + MEL
*
* VOID, REFL OR ZERO BOUNDARY CONDITIONS.
IF(KZ.EQ.1) THEN
LL1 = .TRUE.
ENDIF
IF(LL1) THEN
IF((NCODE(5).EQ.1).AND.(ICODE(5).EQ.0)) THEN
KK7=-1
QFR(NUM1+7)=ALB(ZCODE(5))
ELSE IF(NCODE(5).EQ.1) THEN
KK7=-1
QFR(NUM1+7)=1.0
IQFR(NUM1+7)=ICODE(5)
ELSE IF(NCODE(5).EQ.2) THEN
KK7=-2
ELSE IF(NCODE(5).EQ.7) THEN
KK7=-3
ENDIF
ENDIF
*
IF(KZ.EQ.LZ) THEN
LL2 = .TRUE.
ENDIF
IF(LL2) THEN
IF((NCODE(6).EQ.1).AND.(ICODE(6).EQ.0)) THEN
KK8=-1
QFR(NUM1+8)=ALB(ZCODE(6))
ELSE IF(NCODE(6).EQ.1) THEN
KK8=-1
QFR(NUM1+8)=1.0
IQFR(NUM1+8)=ICODE(6)
ELSE IF(NCODE(6).EQ.2) THEN
KK8=-2
ELSE IF(NCODE(6).EQ.7) THEN
KK8=-3
ENDIF
ENDIF
*
* TRAN BOUNDARY CONDITION.
IF((KZ.EQ.1).AND.(NCODE(5).EQ.4)) THEN
KK7=-2
ELSE IF((KZ.EQ.LZ).AND.(NCODE(6).EQ.4)) THEN
KK8=-2
ENDIF
*
* SYME BOUNDARY CONDITION.
IF((KZ.EQ.1).AND.(NCODE(5).EQ.5)) THEN
KK7=-2
ZZ(KEL)=0.5*ZZ(KEL)
ELSE IF((KZ.EQ.LZ).AND.(NCODE(6).EQ.5)) THEN
KK8=-2
ZZ(KEL)=0.5*ZZ(KEL)
ENDIF
*
IF(KZ.EQ.1) IDEB = KK7
IF(KZ.EQ.LZ) IFIN = KK8
KN4(NUM1+7) = KK7
KN4(NUM1+8) = KK8
NUM1=NUM1+8
40 CONTINUE
45 CONTINUE
* END OF THE MAIN LOOP OVER FINITE ELEMENTS.
*
*----
* VOLUME CALCULATION
*----
DO 55 KZ=1,LZ
DO 50 KX=1,LX
KEL = KX+(KZ-1)*LX
IF(MAT(KEL).EQ.0) THEN
VOL0 = 0.0
ELSE
VOL0 = 2.59807621*SIDE*SIDE*ZZ(KEL)
ENDIF
VOL(KEL) = VOL0
50 CONTINUE
55 CONTINUE
IF(IMPX.NE.0) THEN
WRITE(6,222) 'ZZ ',(ZZ(I),I=1,LX*LZ)
WRITE(6,222) 'VOL',(VOL(I),I=1,LX*LZ)
ENDIF
LL4=0
DO 60 KXZ=1,LX*LZ
IF(MAT(KXZ).GT.0) LL4=LL4+1
60 CONTINUE
*
IF(ISPLH.EQ.1) THEN
IVAL = 8
DO 70 I=1,8*LL4
KN(I) = 0
KN(I) = KN4(I)
70 CONTINUE
DEALLOCATE(KN4)
ELSE IF(ISPLH.GE.2) THEN
IVAL =18*(ISPLH-1)**2+8
CALL TRINTR(ISPLH,IPTRK,LX,LL4,9,MAT)
ALLOCATE(KN1(LL4),KN2(LL4),KN3(LL4))
CALL LCMGET (IPTRK,'IKN',KN1)
NUM1 = 0
NUM3 = 0
DO 80 I=1,LZ*LX*IVAL
KN(I) = 0
80 CONTINUE
DO 90 I=1,LL4
KN2(I) = IDEB
KN3(I) = IFIN
90 CONTINUE
DO 115 K=1,LZ
NUM2 = 0
DO 110 I=1,LX
IF(MAT(I+(K-1)*LX).LE.0) GO TO 110
DO 100 J=1,6*(ISPLH-1)**2
IVAL1 = KN1(NUM2+J) + (K-1)*LL4
IVAL2 = KN2(NUM2+J)
IVAL3 = KN3(NUM2+J)
IF(IDIM.EQ.3.AND.K.GT.1) IVAL2 = IVAL1 - LL4
IF(IDIM.EQ.3.AND.K.LT.LZ) IVAL3 = IVAL1 + LL4
KN(NUM1+J ) = IVAL1
KN(NUM1+J+ 6*(ISPLH-1)**2) = IVAL2
KN(NUM1+J+12*(ISPLH-1)**2) = IVAL3
100 CONTINUE
DO 105 KX=1,6
KN(NUM1+KX+18*(ISPLH-1)**2) = KN4(NUM3+KX)
105 CONTINUE
KN(NUM1+IVAL-1) = KN4(NUM3+7)
KN(NUM1+IVAL ) = KN4(NUM3+8)
NUM1 = NUM1 + IVAL
NUM2 = NUM2 + 6*(ISPLH-1)**2
NUM3 = NUM3 + 8
110 CONTINUE
115 CONTINUE
LL4 = LZ * LL4
DEALLOCATE(KN3,KN2,KN1,KN4)
ENDIF
IF(IMPX.GE.1) THEN
NUM1=0
NUM2=0
IF(ISPLH.EQ.1) THEN
WRITE (6,570)
DO 130 KZ=1,LZ
WRITE(6,'(/13H PLANE NUMBER,I6)') KZ
WRITE (6,520)
DO 120 KX=1,LX
KEL = KX+(KZ-1)*LX
IF(MAT(KEL).LE.0) GO TO 120
WRITE (6,530) I1(KEL),(KN(NUM1+I),I=1,IVAL),
> (QFR(NUM2+I),I=1,8),VOL(KEL)
NUM1 = NUM1 + IVAL
NUM2 = NUM2 + 8
120 CONTINUE
130 CONTINUE
ELSE
WRITE (6,570)
DO 160 KZ=1,LZ
WRITE(6,'(/13H PLANE NUMBER,I6)') KZ
WRITE (6,575)
DO 140 KX=1,LX
KEL = KX+(KZ-1)*LX
IF(MAT(KEL).LE.0) GO TO 140
WRITE (6,580) I1(KEL),(KN(NUM1+I),I=1,IVAL-8)
NUM1 = NUM1 + IVAL
140 CONTINUE
WRITE (6,585)
DO 150 KX=1,LX
KEL = KX+(KZ-1)*LX
IF(MAT(KEL).LE.0) GO TO 150
WRITE (6,590) I1(KEL),(QFR(NUM2+I),I=1,8),
* VOL(KEL)
NUM2 = NUM2 + 8
150 CONTINUE
160 CONTINUE
ENDIF
WRITE (6,560) LL4
ENDIF
DEALLOCATE(I1)
*----
* APPEND THE AVERAGED FLUXES AT THE END OF UNKNOWN VECTOR
*----
NUN=0
IF(ISPLH.GT.1) NUN=LL4
DO 190 I=1,LX*LZ
IF(MAT(I).EQ.0) THEN
IDL(I)=0
ELSE
NUN=NUN+1
IDL(I)=NUN
ENDIF
190 CONTINUE
RETURN
*
222 FORMAT(1X,A3,/,7(2X,E12.5))
520 FORMAT (/8H ELEMENT,6X,10HNEIGHBOURS,37X,20HVOID BOUNDARY CONDIT,
1 3HION,28X,6HVOLUME)
530 FORMAT (1X,I6,2X,8I6,2X,8F6.2,5X,E13.6)
560 FORMAT (/40H NUMBER OF NON VIRTUAL FINITE ELEMENTS =,I6/)
570 FORMAT (/22H NUMBERING OF UNKNOWNS/1X,21(1H-))
575 FORMAT (/8H ELEMENT,44X,10HNEIGHBOURS)
580 FORMAT (1X,I6,2X,20I6/(9X,20I6))
585 FORMAT (/8H ELEMENT,3X,23HVOID BOUNDARY CONDITION,28X,6HVOLUME)
590 FORMAT (1X,I6,2X,8F6.2,5X,E13.6)
END
|