There are many errors, but they are mainly related to the part of the code where FORMAT is written. In this part, I separated some of the words “_”, since they were highlighted in color, which means the compiler perceived them not as explanations, but as a call to some action, I also replaced “=" with “equals”, removed the dots, so how the compiler cursed at them. If anyone has the opportunity, please help me correct the errors. I believe they are the same type. I use the 2012 code compiler in Code::Blocks so that it doesn't complain about "GO TO".
Source code link: https://acrobat.adobe.com/id/urn:aaid:sc:VA6C2:e77e5821-8991-4144-9711-d2ffcf868c0a
List of errors:
|296| 296 .130:|||Error: Unexpected element 'Q' in format string |
|297| 297 .50:|||Error: Unexpected end of format string in format string |
|298| 298 .73:|||Error: Positive width required in format specifier E |
|299| 299 .39:|||Error: Unexpected element 'Y' in format string |
|300| 300 .75:|||Error: Positive width required in format specifier E |
|301| 301 .38:|||Error: Unexpected element 'U' in format string |
|302| 302 .95:|||Error: Unexpected element 'Q' in format string |
|303| 303 .132:|||Error: Unexpected end of format string in format string |
|306| 306 .171:|||Error: Positive width required in format specifier E |
|308| 308 .132:|||Error: Unexpected end of format string in format string |
|353| 353 .6:|||Error: Unclassifiable statement |
|15| 15 .16:|||Error: FORMAT label 6 not defined|
|17| 17 .16:|||Error: FORMAT label 7 not defined|
|19| 19 .16:|||Error: FORMAT label 8 not defined|
|21| 21 .16:|||Error: FORMAT label 9 not defined|
|23| 23 .17:|||Error: FORMAT label 10 not defined|
|26| 26 .17:|||Error: FORMAT label 11 not defined|
|27| 27 .17:|||Error: FORMAT label 12 not defined|
|58| 58 .17:|||Error: FORMAT label 13 not defined|
|351| 351 .14:|||Error: Label 20 referenced is never defined|
|157| 157 .17:|||Error: FORMAT label 16 not defined|
|221| 221 .17:|||Error: FORMAT label 18 not defined|
||=== Build finished: 24 errors, 0 warnings (0 minutes, 0 seconds) ===|
Code with numbered lines:
1 PROGRAM TWOFS
2
3 COMMON/S1/PI,PR,PR1,PR2,PR3,CON,COND
4 COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
5 COMMON/S3/C(100,100),B(100),P(100)
6 !
7 DIMENSION XM(50),YM(50),A(50),COSBET(50),SINBET(50),KOD(50)
8 DIMENSION TITLE(20)
9 !
10 READ (5,1) (TITLE(I),I=1,20)
11 WRITE (6,2) (TITLE(I),I=1,20)
12 READ (5,3) NUMBS,NUMOS,KSYM
13 READ (5,4) PR,E,XSYM,YSYM
14 READ (5,5) PXX,PYY,PXY
15 WRITE (6,6) NUMBS,NUMOS
16 GO TO (80,85,90,95), KSYM
17 80 WRITE (6,7)
18 GO TO 100
19 85 WRITE (6,8) XSYM
20 GO TO 100
21 90 WRITE (6,9) YSYM
22 GO TO 100
23 95 WRITE (6,10) XSYM,YSYM
24 !
25 100 CONTINUE
26 WRITE (6,11) PR,E
27 WRITE (6,12) PXX,PYY,PXY
28 !
29 PI=4.*ATAN(1.)
30 CON=1./(4.*PI*(1.-PR))
31 COND=(1.+PR)/E
32 PR1=1.-2.*PR
33 PR2=2.*(1.-PR)
34 PR3=3.-4.*PR
35 !
36 ! DEFINE LOCATIONS,SIZES,ORIENTATIONS AND BOUNDARY CONDITIONS OF BOUNDARY ELEMENTS
37 !
38 NUMBE=0
39 DO 110 N=1,NUMBS
40 READ (5,14) NUM,XBEG,YBEG,XEND,YEND,KODE,BVS,BVN
41 XD=(XEND-XBEG)/NUM
42 YD=(YEND-YBEG)/NUM
43 SW=SQRT(XD*XD+YD*YD)
44 !
45 DO 110 NE=1,NUM
46 NUMBE=NUMBE+1
47 M=NUMBE
48 XM(M)=XBEG+0.5*(2.*NE-1.)*XD
49 YM(M)=YBEG+0.5*(2.*NE-1.)*YD
50 A(M)=0.5*SW
51 SINBET(M)=YD/SW
52 COSBET(M)=XD/SW
53 KOD(M)=KODE
54 MN=2*M
55 MS=MN-1
56 B(MS)=BVS
57 110 B(MN)=BVN
58 WRITE (6,13)
59 DO 115 M=1,NUMBE
60 SIZE=2.*A(M)
61 ANGLE=180.*ATAN2(SINBET(M),COSBET(M))/PI
62 WRITE (6,15) M,KOD(M),XM(M),YM(M),SIZE,ANGLE,B(2*M-1),B(2*M)
63 115 CONTINUE
64 !
65 ! ADJUST STRESS BOUNDARY VALUES TO ACCOUNT FOR INITIAL STRESSES.
66 !
67 DO 150 N=1,NUMBE
68 NN=2*N
69 NS=NN-1
70 COSB=COSBET(N)
71 SINB=SINBET(N)
72 SIGS=(PYY-PXX)*SINB*COSB+PXY*(COSB*COSB-SINB*SINB)
73 SIGN=PXX*SINB*SINB-2.*PXY*SINB*COSB+PYY*COSB*COSB
74 GO TO (120,150,130,140),KOD(N)
75 120 B(NS)=B(NS)-SIGS
76 B(NN)=B(NN)-SIGN
77 GO TO 150
78 130 B(NN)=B(NN)-SIGN
79 GO TO 150
80 140 B(NS)=B(NS)-SIGS
81 150 CONTINUE
82 !
83 ! COMPUTE INFLUENCE COEFFICIENTS AND SET UP SYSTEM OF ALGEBRAIC EQUATIONS.
84 !
85 DO 300 I=1,NUMBE
86 IN=2*I
87 IS=IN-1
88 XI=XM(I)
89 YI=YM(I)
90 COSBI=COSBET(I)
91 SINBI=SINBET(I)
92 KODE=KOD(I)
93 !
94 DO 300 J=1,NUMBE
95 JN=2*J
96 JS=JN-1
97 CALL INITL
98 XJ=XM(J)
99 YJ=YM(J)
100 COSBJ=COSBET(J)
101 SINBJ=SINBET(J)
102 AJ=A(J)
103 CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,SINBJ,+1)
104 GO TO (240,210,220,230),KSYM
105 !
106 210 XJ=2.*XSYM-XM(J)
107 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
108 GO TO 240
109 !
110 220 YJ=2.*YSYM-YM(J)
111 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
112 GO TO 240
113 !
114 230 XJ=2.*XSYM-XM(J)
115 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
116 XJ=XM(J)
117 YJ=2.*YSYM-YM(J)
118 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
119 XJ=2.*XSYM-XM(J)
120 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
121 !
122 240 CONTINUE
123 GO TO (250,260,270,280),KODE
124 !
125 250 C(IS,JS)=(SYYS-SXXS)*SINBI*COSBI+SXYS*(COSBI*COSBI-SINBI*SINBI)
126 C(IS,JN)=(SYYN-SXXN)*SINBI*COSBI+SXYN*(COSBI*COSBI-SINBI*SINBI)
127 C(IN,JS)=SXXS*SINBI*SINBI-2.*SXYS*SINBI*COSBI+SYYS*COSBI*COSBI
128 C(IN,JN)=SXXN*SINBI*SINBI-2.*SXYN*SINBI*COSBI+SYYN*COSBI*COSBI
129 GO TO 300
130 !
131 260 C(IS,JS)=UXS*COSBI+UYS*SINBI
132 C(IS,JN)=UXN*COSBI+UYN*SINBI
133 C(IN,JS)=-UXS*SINBI+UYS*COSBI
134 C(IN,JN)=-UXN*SINBI+UYN*COSBI
135 GO TO 300
136 !
137 270 C(IS,JS)=UXS*COSBI+UYS*SINBI
138 C(IS,JN)=UXN*COSBI+UYN*SINBI
139 C(IN,JS)=SXXS*SINBI*SINBI-2.*SXYS*SINBI*COSBI+SYYS*COSBI*COSBI
140 C(IN,JN)=SXXN*SINBI*SINBI-2.*SXYN*SINBI*COSBI+SYYN*COSBI*COSBI
141 GO TO 300
142 !
143 280 C(IS,JS)=(SYYS-SXXS)*SINBI*COSBI+SXYS*(COSBI*COSBI-SINBI*SINBI)
144 C(IS,JN)=(SYYN-SXXN)*SINBI*COSBI+SXYN*(COSBI*COSBI-SINBI*SINBI)
145 C(IN,JS)=-UXS*SINBI+UYS*COSBI
146 C(IN,JN)=-UXN*SINBI+UYN*COSBI
147 !
148 300 CONTINUE
149 !
150 ! SOLVE SYSTEM OF ALGEBRAIC EQUATIONS.
151 !
152 N=2*NUMBE
153 CALL SOLVE(N)
154 !
155 ! COMPUTE BOUNDARY DISPLACEMENTS AND STRESSES.
156 !
157 WRITE (6,16)
158 DO 600 I=1,NUMBE
159 XI=XM(I)
160 YI=YM(I)
161 COSBI=COSBET(I)
162 SINBI=SINBET(I)
163 !
164 UX=0.
165 UY=0.
166 SIGXX=PXX
167 SIGYY=PYY
168 SIGXY=PXY
169 !
170 DO 570 J=1,NUMBE
171 JN=2*J
172 JS=JN-1
173 CALL INITL
174 XJ=XM(J)
175 YJ=YM(J)
176 AJ=A(J)
177 COSBJ=COSBET(J)
178 SINBJ=SINBET(J)
179 CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,SINBJ,+1)
180 GO TO (540,510,520,530),KSYM
181 !
182 510 XJ=2.*XSYM-XM(J)
183 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
184 GO TO 540
185 !
186 520 YJ=2.*YSYM-YM(J)
187 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
188 GO TO 540
189 !
190 530 XJ=2.*XSYM-XM(J)
191 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
192 XJ=XM(J)
193 YJ=2.*YSYM-YM(J)
194 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
195 XJ=2.*XSYM-XM(J)
196 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
197 !
198 540 CONTINUE
199 !
200 UX=UX+UXS*P(JS)+UXN*P(JN)
201 UY=UY+UYS*P(JS)+UYN*P(JN)
202 SIGXX=SIGXX+SXXS*P(JS)+SXXN*P(JN)
203 SIGYY=SIGYY+SYYS*P(JS)+SYYN*P(JN)
204 SIGXY=SIGXY+SXYS*P(JS)+SXYN*P(JN)
205 !
206 570 CONTINUE
207 !
208 US=UX*COSBI+UY*SINBI
209 UN=-UX*SINBI+UY*COSBI
210 SIGS=(SIGYY-SIGXX)*SINBI*COSBI+SIGXY*(COSBI*COSBI-SINBI*SINBI)
211 SIGN=SIGXX*SINBI*SINBI-2.*SIGXY*SINBI*COSBI+SIGYY*COSBI*COSBI
212 SIGT=SIGXX*COSBI*COSBI-2.*SIGXY*COSBI*SINBI+SIGYY*SINBI*SINBI
213 !
214 WRITE (6,17) I,UX,UY,US,UN,SIGXX,SIGYY,SIGXY,SIGS,SIGN,SIGT
215 !
216 600 CONTINUE
217 !
218 ! COMPUTE DISPLACEMENTS AND STRESSES AT SPECIFIED POINTS IN BOD
219 !
220 IF (NUMOS.LE.0) GO TO 900
221 WRITE (6,18)
222 NPOINT=0
223 DO 890 N=1,NUMOS
224 READ (5,19) XBEG,YBEG,XEND,YEND,NUMPB
225 NUMP=NUMPB+1
226 DELX=(XEND-XBEG)/NUMP
227 DELY=(YEND-YBEG)/NUMP
228 IF (NUMPB.GT.0) NUMP=NUMP+1
229 IF (DELX**2+DELY**2.EQ.0.) NUMP=1
230 !
231 DO 890 NI=1,NUMP
232 XP=XBEG+(NI-1)*DELX
233 YP=YBEG+(NI-1)*DELY
234 !
235 UX=0.
236 UY=0.
237 SIGXX=PXX
238 SIGYY=PYY
239 SIGXY=PXY
240 !
241 DO 880 J=1,NUMBE
242 JN=2*J
243 JS=JN-1
244 CALL INITL
245 XJ=XM(J)
246 YJ=YM(J)
247 AJ=A(J)
248 !
249 IF (SQRT((XP-XJ)**2+(YP-YJ)**2).LT.2.*AJ) GO TO 890
250 !
251 COSBJ=COSBET(J)
252 SINBJ=SINBET(J)
253 CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,SINBJ,+1)
254 GO TO (840,810,820,830),KSYM
255 !
256 810 XJ=2.*XSYM-XM(J)
257 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
258 GO TO 840
259 !
260 820 YJ=2.*YSYM-YM(J)
261 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
262 GO TO 840
263 !
264 830 XJ=2.*XSYM-XM(J)
265 CALL KOEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
266 XJ=XM(J)
267 YJ=2.*YSYM-YM(J)
268 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
269 XJ=2.*XSYM-XM(J)
270 CALL KOEFF(XI,YI,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
271 !
272 840 CONTINUE
273 !
274 UX=UX+UXS*P(JS)+UXN*P(JN)
275 UY=UY+UYS*P(JS)+UYN*P(JN)
276 SIGXX=SIGXX+SXXS*P(JS)+SXXN*P(JN)
277 SIGYY=SIGYY+SYYS*P(JS)+SYYN*P(JN)
278 SIGXY=SIGXY+SXYS*P(JS)+SXYN*P(JN)
279 !
280 880 CONTINUE
281 !
282 NPOINT=NPOINT+1
283 WRITE (6,20) NPOINT,XP,YP,UX,UY,SIGXX,SIGYY,SIGXY
284 !
285 890 CONTINUE
286 !
287 900 CONTINUE
288 !
289 ! FORMAT STATEMENTS.
290 !
291 1 FORMAT (20A4)
292 2 FORMAT (1H1,/,25X,20A4,/)
293 3 FORMAT (3I4)
294 4 FORMAT (F6.2,E11.4,2F12.4)
295 5 FORMAT (3E11.4)
296 6 FORMAT (/,109H NUMBE_R OF STRAIGHT-LINE SEGMENTS (EACH COUNTING AT LEAST ONE BOUNDARY ELEMENT) USED T_O DEFINE BOUNDARIES equals,I3,//,12 23H NUMBE_R OF STRAIGHT-LINE SEGMENTS USED T_O SPECIFY OTHER LOCATIONS (I E, NO_T ON A BOUNDARY) WHER_E RESULTS ARE T_O BE FOUND =,I3)
297 7 FORMAT (/,32H NOSYMMETRY CONDITIONS IMPOSED)
298 8 FORMAT (/,18H THE LINE X equals XS equals, F12.4,23H I_S A LINE OF SYMMETRY)
299 9 FORMAT (/,18H THE LINE Y equals YS equals, F12.4,23H I_S A LINE OF SYMMETRY)
300 10 FORMAT (/,19H THE LINES X equals XS equals,F12.4,13H AND Y equals YS equals, F12.4,23H ARE LINES OF SYMMETRY)
301 11 FORMAT (/,18H POISSONS RATIO equals,F6.2,//,18H YOUNGS MODULUS equals,E11.14)
302 12 FORMAT (/,31H XX-COMPONENT OF FIELD STRESS -,E11.4,//,31H YY-COMPONENT OF FIELD STRESS equals,E11.4,//,31H XY COMPONENTOF FIELD STRESS equals,E11.4)
303 13 FORMAT (1H1,/,27H BOUNDARY ELEMENT DAT_A,//,96H ELEMENT KODE X (CENTER) Y (CENTER) LENGTH ANGLE US OR SIGMA-S UN OR SIGMA-N,/)
304 14 FORMAT (I4,4F12.4,I4,2E11.4)
305 15 FORMAT (2I9,3F12.4,F12.2,2E15.4)
306 16 FORMAT (1H1,/,66H DISPLACEMENTS AND STRESS AT MIDPOINTS OF BOUNDARY ELEMENTS,//,40H ELEMENT UX UY US,60H UN SIGXX SIGYY SIGXY SIGMA-S SIGMA-N,10H SIGMA-T,/)
307 17 FORMAT (I10,4F10.6,6F10.1)
308 18 FORMAT (1H1,/,64H DISPLACEMENTS AND STRESSES AT SPECIFIED POINTS I_N THE BODY,//,93H POINT X CO-ORD Y CO-ORD UX UY SIGXX SIGYY SIGXY,/)
309 19 FORMAT (4F12.4,I4)
310 20 FORMAT (I9,2F12.4,2F12.6,3F12.1)
311 !
312 END
313
314 SUBROUTINE INITL
315 !
316 COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
317 !
318 SXXS=0.
319 SXXN=0.
320 SYYS=0.
321 SYYN=0.
322 SXYS=0.
323 SXYN=0.
324 !
325 UXS=0.
326 UXN=0.
327 UYS=0.
328 UYN=0.
329 !
330 RETURN
331 END
332
333 SUBROUTINE COEFF(X,Y,CX,CY,A,COSB,SINB,MSYM)
334 !
335 COMMON/S1/PI,PR,PR1,PR2,PR3,CON,COND
336 COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
337 !
338 COS2B=COSB*COSB-SINB*SINB
339 SIN2B=2.*SINB*COSB
340 XB=(X-CX)*COSB+(Y-CY)*SINB
341 YB=-(X-CX)*SINB+(Y-CY)*COSB
342 !
343 R1S=(XB-A)*(XB-A)+YB*YB
344 R2S=(XB+A)*(XB+A)+YB*YB
345 FL1=0.5*ALOG(R1S)
346 FL2=0.5*ALOG(R2S)
347 FB2=CON*(FL1-FL2)
348 IF (YB.NE.0.) GO TO 10
349 FB3=0.
350 IF (ABS(XB).LT.A) FB3=CON*PI
351 GO TO 20
352 10 FB3=-CON*(ATAN((XB+A)/YB)-ATAN((XB-A)/YB))
353 20 FB1=YB*FB3+CON*(XB-A)*FL1-(XB+A)*FL2)
354 FB4=CON*(YB/R1S-YB/R2S)
355 FB5=CON*((XB-A)/R1S-(XB+A)/R2S)
356 !
357 UXPS=COND*(PR3*COSB*FB1+YB*(SINB*FB2+COSB*FB3))
358 UXPN=COND*(-PR3*SINB*FB1-YB*(COSB*FB2-SINB*FB3))
359 UYPS=COND*(PR3*SINB*FB1-YB*(COSB*FB2-SINB*FB3))
360 UYPN=COND*(PR3*COSB*FB1-YB*(SINB*FB2+COSB*FB3))
361 !
362 SXXPS=FB2+PR2*(COS2B*FB2-SIN2B*FB3)+YB*(COS2B*FB4+SIN2B*FB5)
363 SXXPN=FB3-PR1*(SIN2B*FB2+COS2B*FB3)+YB*(SIN2B*FB4-COS2B*FB5)
364 SYYPS=FB2-PR2*(COS2B*FB2-SIN2B*FB3)-YB*(COS2B*FB4+SIN2B*FB5)
365 SYYPN=FB3+PR1*(SIN2B*FB2+COS2B*FB3)-YB*(SIN2B*FB4-COS2B*FB5)
366 SXYPS=PR2*(SIN2B*FB2+COS2B*FB3)+YB*(SIN2B*FB4-COS2B*FB5)
367 SXYPN=PR1*(COS2B*FB2-SIN2B*FB3)-YB*(COS2B*FB4+SIN2B*FB5)
368 !
369 UXS=UXS+MSYM*UXPS
370 UXN=UXN+UXPN
371 UYS=UYS+MSYM*UYPS
372 UYN=UYN+UYPN
373 !
374 SXXS=SXXS+MSYM*SXXPS
375 SXXN=SYYN+SXXPN
376 SYYS=SYYS+MSYM*SYYPS
377 SYYN=SYYN+SYYPN
378 SXYS=SXYS+MSYM*SXYPS
379 SXYN=SXYN+SXYPN
380 !
381 RETURN
382 END
383 SUBROUTINE SOLVE(N)
384 !
385 COMMON/S3/A(100,100),B(100),X(100)
386 !
387 NB=N-1
388 DO 20 J=1,NB
389 L=J+1
390 DO 20 JJ=L,N
391 XM=A(JJ,J)/A(J,J)
392 DO 10 I=J,N
393 10 A(JJ,I)=A(JJ,I)-A(J,I)*XM
394 20 B(JJ)=B(JJ)-B(J)*XM
395 !
396 X(N)=B(N)/A(N,N)
397 DO 40 J=1,NB
398 JJ=N-J
399 L=JJ+1
400 SUM=0.
401 DO 30 I=L,N
402 30 SUM=SUM+A(JJ,I)*X(I)
403 40 X(JJ)=(B(JJ)-SUM)/(A(JJ,JJ))
404 !
405 RETURN
406 END
Updated code:
PROGRAM TWOFS
!
COMMON/S1/PI,PR,PR1,PR2,PR3,CON,COND
COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
COMMON/S3/C(100,100),B(100),P(100)
!
DIMENSION XM(50),YM(50),A(50),COSBET(50),SINBET(50),KOD(50)
DIMENSION TITLE(20)
!
READ (5,1) (TITLE(I),I=1,20)
WRITE (6,2) (TITLE(I),I=1,20)
READ (5,3) NUMBS,NUMOS,KSYM
READ (5,4) PR,E,XSYM,YSYM
READ (5,5) PXX,PYY,PXY
WRITE (6,6) NUMBS,NUMOS
GO TO (80,85,90,95), KSYM
80 WRITE (6,7)
GO TO 100
85 WRITE (6,8) XSYM
GO TO 100
90 WRITE (6,9) YSYM
GO TO 100
95 WRITE (6,10) XSYM,YSYM
!
100 CONTINUE
WRITE (6,11) PR,E
WRITE (6,12) PXX,PYY,PXY
!
PI=4.*ATAN(1.)
CON=1./(4.*PI*(1.-PR))
COND=(1.+PR)/E
PR1=1.-2.*PR
PR2=2.*(1.-PR)
PR3=3.-4.*PR
!
! DEFINE LOCATIONS,SIZES,ORIENTATIONS AND BOUNDARY CONDITIONS OF BOUNDARY ELEMENTS
!
NUMBE=0
DO 110 N=1,NUMBS
READ (5,14) NUM,XBEG,YBEG,XEND,YEND,KODE,BVS,BVN
XD=(XEND-XBEG)/NUM
YD=(YEND-YBEG)/NUM
SW=SQRT(XD*XD+YD*YD)
!
DO 110 NE=1,NUM
NUMBE=NUMBE+1
M=NUMBE
XM(M)=XBEG+0.5*(2.*NE-1.)*XD
YM(M)=YBEG+0.5*(2.*NE-1.)*YD
A(M)=0.5*SW
SINBET(M)=YD/SW
COSBET(M)=XD/SW
KOD(M)=KODE
MN=2*M
MS=MN-1
B(MS)=BVS
110 B(MN)=BVN
WRITE (6,13)
DO 115 M=1,NUMBE
SIZE=2.*A(M)
ANGLE=180.*ATAN2(SINBET(M),COSBET(M))/PI
WRITE (6,15) M,KOD(M),XM(M),YM(M),SIZE,ANGLE,B(2*M-1),B(2*M)
115 CONTINUE
!
! ADJUST STRESS BOUNDARY VALUES TO ACCOUNT FOR INITIAL STRESSES.
!
DO 150 N=1,NUMBE
NN=2*N
NS=NN-1
COSB=COSBET(N)
SINB=SINBET(N)
SIGS=(PYY-PXX)*SINB*COSB+PXY*(COSB*COSB-SINB*SINB)
SIG_N=PXX*SINB*SINB-2.*PXY*SINB*COSB+PYY*COSB*COSB
GO TO (120,150,130,140),KOD(N)
120 B(NS)=B(NS)-SIGS
B(NN)=B(NN)-SIG_N
GO TO 150
130 B(NN)=B(NN)-SIG_N
GO TO 150
140 B(NS)=B(NS)-SIGS
150 CONTINUE
!
! COMPUTE INFLUENCE COEFFICIENTS AND SET UP SYSTEM OF ALGEBRAIC EQUATIONS.
!
DO 300 I=1,NUMBE
IN=2*I
IS=IN-1
XI=XM(I)
YI=YM(I)
COSBI=COSBET(I)
SINBI=SINBET(I)
KODE=KOD(I)
!
DO 300 J=1,NUMBE
JN=2*J
JS=JN-1
CALL INITL
XJ=XM(J)
YJ=YM(J)
COSBJ=COSBET(J)
SINBJ=SINBET(J)
AJ=A(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,SINBJ,+1)
GO TO (240,210,220,230),KSYM
!
210 XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
GO TO 240
!
220 YJ=2.*YSYM-YM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
GO TO 240
!
230 XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
XJ=XM(J)
YJ=2.*YSYM-YM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
!
240 CONTINUE
GO TO (250,260,270,280),KODE
!
250 C(IS,JS)=(SYYS-SXXS)*SINBI*COSBI+SXYS*(COSBI*COSBI-SINBI*SINBI)
C(IS,JN)=(SYYN-SXXN)*SINBI*COSBI+SXYN*(COSBI*COSBI-SINBI*SINBI)
C(IN,JS)=SXXS*SINBI*SINBI-2.*SXYS*SINBI*COSBI+SYYS*COSBI*COSBI
C(IN,JN)=SXXN*SINBI*SINBI-2.*SXYN*SINBI*COSBI+SYYN*COSBI*COSBI
GO TO 300
!
260 C(IS,JS)=UXS*COSBI+UYS*SINBI
C(IS,JN)=UXN*COSBI+UYN*SINBI
C(IN,JS)=-UXS*SINBI+UYS*COSBI
C(IN,JN)=-UXN*SINBI+UYN*COSBI
GO TO 300
!
270 C(IS,JS)=UXS*COSBI+UYS*SINBI
C(IS,JN)=UXN*COSBI+UYN*SINBI
C(IN,JS)=SXXS*SINBI*SINBI-2.*SXYS*SINBI*COSBI+SYYS*COSBI*COSBI
C(IN,JN)=SXXN*SINBI*SINBI-2.*SXYN*SINBI*COSBI+SYYN*COSBI*COSBI
GO TO 300
!
280 C(IS,JS)=(SYYS-SXXS)*SINBI*COSBI+SXYS*(COSBI*COSBI-SINBI*SINBI)
C(IS,JN)=(SYYN-SXXN)*SINBI*COSBI+SXYN*(COSBI*COSBI-SINBI*SINBI)
C(IN,JS)=-UXS*SINBI+UYS*COSBI
C(IN,JN)=-UXN*SINBI+UYN*COSBI
!
300 CONTINUE
!
! SOLVE SYSTEM OF ALGEBRAIC EQUATIONS.
!
N=2*NUMBE
CALL SOLVE(N)
!
! COMPUTE BOUNDARY DISPLACEMENTS AND STRESSES.
!
WRITE (6,16)
DO 600 I=1,NUMBE
XI=XM(I)
YI=YM(I)
COSBI=COSBET(I)
SINBI=SINBET(I)
!
UX=0.
UY=0.
SIGXX=PXX
SIGYY=PYY
SIGXY=PXY
!
DO 570 J=1,NUMBE
JN=2*J
JS=JN-1
CALL INITL
XJ=XM(J)
YJ=YM(J)
AJ=A(J)
COSBJ=COSBET(J)
SINBJ=SINBET(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,SINBJ,+1)
GO TO (540,510,520,530),KSYM
!
510 XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
GO TO 540
!
520 YJ=2.*YSYM-YM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
GO TO 540
!
530 XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
XJ=XM(J)
YJ=2.*YSYM-YM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
XJ=2.*XSYM-XM(J)
CALL COEFF(XI,YI,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
!
540 CONTINUE
!
UX=UX+UXS*P(JS)+UXN*P(JN)
UY=UY+UYS*P(JS)+UYN*P(JN)
SIGXX=SIGXX+SXXS*P(JS)+SXXN*P(JN)
SIGYY=SIGYY+SYYS*P(JS)+SYYN*P(JN)
SIGXY=SIGXY+SXYS*P(JS)+SXYN*P(JN)
!
570 CONTINUE
!
US=UX*COSBI+UY*SINBI
UN=-UX*SINBI+UY*COSBI
SIGS=(SIGYY-SIGXX)*SINBI*COSBI+SIGXY*(COSBI*COSBI-SINBI*SINBI)
SIG_N=SIGXX*SINBI*SINBI-2.*SIGXY*SINBI*COSBI+SIGYY*COSBI*COSBI
SIGT=SIGXX*COSBI*COSBI+2.*SIGXY*COSBI*SINBI+SIGYY*SINBI*SINBI
!
WRITE (6,17) I,UX,UY,US,UN,SIGXX,SIGYY,SIGXY,SIGS,SIG_N,SIGT
!
600 CONTINUE
!
! COMPUTE DISPLACEMENTS AND STRESSES AT SPECIFIED POINTS IN BOD
!
IF (NUMOS.LE.0) GO TO 900
WRITE (6,18)
NPOINT=0
DO 890 N=1,NUMOS
READ (5,19) XBEG,YBEG,XEND,YEND,NUMPB
NUMP=NUMPB+1
DELX=(XEND-XBEG)/NUMP
DELY=(YEND-YBEG)/NUMP
IF (NUMPB.GT.0) NUMP=NUMP+1
IF (DELX**2+DELY**2.EQ.0.) NUMP=1
!
DO 890 NI=1,NUMP
XP=XBEG+(NI-1)*DELX
YP=YBEG+(NI-1)*DELY
!
UX=0.
UY=0.
SIGXX=PXX
SIGYY=PYY
SIGXY=PXY
!
DO 880 J=1,NUMBE
JN=2*J
JS=JN-1
CALL INITL
XJ=XM(J)
YJ=YM(J)
AJ=A(J)
!
IF (SQRT((XP-XJ)**2+(YP-YJ)**2).LT.2.*AJ) GO TO 890
!
COSBJ=COSBET(J)
SINBJ=SINBET(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,COSBJ,SINBJ,+1)
GO TO (840,810,820,830),KSYM
!
810 XJ=2.*XSYM-XM(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
GO TO 840
!
820 YJ=2.*YSYM-YM(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
GO TO 840
!
830 XJ=2.*XSYM-XM(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,COSBJ,-SINBJ,-1)
XJ=XM(J)
YJ=2.*YSYM-YM(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,-COSBJ,SINBJ,-1)
XJ=2.*XSYM-XM(J)
CALL COEFF(XP,YP,XJ,YJ,AJ,-COSBJ,-SINBJ,+1)
!
840 CONTINUE
!
UX=UX+UXS*P(JS)+UXN*P(JN)
UY=UY+UYS*P(JS)+UYN*P(JN)
SIGXX=SIGXX+SXXS*P(JS)+SXXN*P(JN)
SIGYY=SIGYY+SYYS*P(JS)+SYYN*P(JN)
SIGXY=SIGXY+SXYS*P(JS)+SXYN*P(JN)
!
880 CONTINUE
!
NPOINT=NPOINT+1
WRITE (6,20) NPOINT,XP,YP,UX,UY,SIGXX,SIGYY,SIGXY
!
890 CONTINUE
!
900 CONTINUE
!
! FORMAT STATEMENTS.
!
1 FORMAT (20A4)
2 FORMAT (1H1,/,25X,20A4,/)
3 FORMAT (3I4)
4 FORMAT (F6.2,E11.4,2F12.4)
5 FORMAT (3E11.4)
6 FORMAT (/,109H NUMBE_R OF STRAIGHT-LINE SEGMENTS (EACH COUNTING A&
T LEAST ONE BOUNDARY ELEMENT) USED T_O DEFINE BOUNDARIES =,I3,//,12&
6H NUMBE_R OF STRAIGHT-LINE SEGMENTS USED T_O SPECIFY OTHER LOCATION&
S (IE, NO_T ON A BOUNDARY) WHER_E RESULTS ARE T_O BE FOUND =,I3)
7 FORMAT (/,31H NO SYMMETRY CONDITIONS IMPOSED)
8 FORMAT (/,18H THE LINE X = XS =, F12.4,23H I_S A LINE OF SYMMETRY)
9 FORMAT (/,18H THE LINE Y = YS =, F12.4,23H I_S A LINE OF SYMMETRY)
10 FORMAT (/,19H THE LINES X = XS =,F12.4,13H AND Y = YS =, F12.4,&
22H ARE LINES OF SYMMETRY)
11 FORMAT (/,17H POISSONS RATIO =,F6.2,//,17H YOUNGS MODULUS =,E11.&
4)
12 FORMAT (/,31H XX-COMPONENT OF FIELD STRESS =,E11.4,//,31H YY-COMPO&
NENT OF FIELD STRESS =,E11.4,//,31H XY-COMPONENT OF FIELD STRESS =&
,E11.4)
13 FORMAT (1H1,/,27H BOUNDARY ELEMENT DAT_A,//,96H ELEMENT K&
ODE X (CENTER) Y (CENTER) LENGTH ANGLE US OR SIGMA-S&
UN OR SIGMA-N,/)
14 FORMAT (I4,4F12.4,I4,2E11.4)
15 FORMAT (2I9,3F12.4,F12.2,2E15.4)
16 FORMAT (1H1,/,65H DISPLACEMENTS AND STRESSES AT MIDPOINTS OF B&
OUNDARY ELEMENTS,//,40H ELEMENT UX UY US,&
60H UN SIGXX SIGYY SIGXY SIGMA-S SIGMA-N,&
10H SIGMA-T,/)
17 FORMAT (I10,4F10.6,6F10.1)
18 FORMAT (1H1,/,64H DISPLACEMENTS AND STRESSES AT SPECIFIED POIN&
TS I_N THE BODY,//,93H POINT X CO-ORD Y CO-ORD U&
X UY SIGXX SIGYY SIGXY,/)
19 FORMAT (4F12.4,I4)
20 FORMAT (I9,2F12.4,2F12.6,3F12.1)
!
END
!
SUBROUTINE INITL
!
COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
!
SXXS=0.
SXXN=0.
SYYS=0.
SYYN=0.
SXYS=0.
SXYN=0.
!
UXS=0.
UXN=0.
UYS=0.
UYN=0.
!
RETURN
END
!
SUBROUTINE COEFF(X,Y,CX,CY,A,COSB,SINB,MSYM)
!
COMMON/S1/PI,PR,PR1,PR2,PR3,CON,COND
COMMON/S2/SXXS,SXXN,SYYS,SYYN,SXYS,SXYN,UXS,UXN,UYS,UYN
!
COS2B=COSB*COSB-SINB*SINB
SIN2B=2.*SINB*COSB
!
XB=(X-CX)*COSB+(Y-CY)*SINB
YB=-(X-CX)*SINB+(Y-CY)*COSB
!
R1S=(XB-A)*(XB-A)+YB*YB
R2S=(XB+A)*(XB+A)+YB*YB
FL1=0.5*ALOG(R1S)
FL2=0.5*ALOG(R2S)
FB2=CON*(FL1-FL2)
IF (YB.NE.0.) GO TO 10
FB3=0.
IF (ABS(XB).LT.A) FB3=CON*PI
GO TO 20
10 FB3=-CON*(ATAN((XB+A)/YB)-ATAN((XB-A)/YB))
20 FB1=YB*FB3+CON*((XB-A)*FL1-(XB+A)*FL2)
FB4=CON*(YB/R1S-YB/R2S)
FB5=CON*((XB-A)/R1S-(XB+A)/R2S)
!
UXPS=COND*(PR3*COSB*FB1+YB*(SINB*FB2+COSB*FB3))
UXPN=COND*(-PR3*SINB*FB1-YB*(COSB*FB2-SINB*FB3))
UYPS=COND*(PR3*SINB*FB1-YB*(COSB*FB2-SINB*FB3))
UYPN=COND*(PR3*COSB*FB1-YB*(SINB*FB2+COSB*FB3))
!
SXXPS=FB2+PR2*(COS2B*FB2-SIN2B*FB3)+YB*(COS2B*FB4+SIN2B*FB5)
SXXPN=FB3-PR1*(SIN2B*FB2+COS2B*FB3)+YB*(SIN2B*FB4-COS2B*FB5)
SYYPS=FB2-PR2*(COS2B*FB2-SIN2B*FB3)-YB*(COS2B*FB4+SIN2B*FB5)
SYYPN=FB3+PR1*(SIN2B*FB2+COS2B*FB3)-YB*(SIN2B*FB4-COS2B*FB5)
SXYPS=PR2*(SIN2B*FB2+COS2B*FB3)+YB*(SIN2B*FB4-COS2B*FB5)
SXYPN=PR1*(COS2B*FB2-SIN2B*FB3)-YB*(COS2B*FB4+SIN2B*FB5)
!
UXS=UXS+MSYM*UXPS
UXN=UXN+UXPN
UYS=UYS+MSYM*UYPS
UYN=UYN+UYPN
!
SXXS=SXXS+MSYM*SXXPS
SXXN=SXXN+SXXPN
SYYS=SYYS+MSYM*SYYPS
SYYN=SYYN+SYYPN
SXYS=SXYS+MSYM*SXYPS
SXYN=SXYN+SXYPN
!
RETURN
END
!
SUBROUTINE SOLVE(N)
!
COMMON/S3/A(100,100),B(100),X(100)
!
NB=N-1
DO 20 J=1,NB
L=J+1
DO 20 JJ=L,N
XM=A(JJ,J)/A(J,J)
DO 10 I=J,N
10 A(JJ,I)=A(JJ,I)-A(J,I)*XM
20 B(JJ)=B(JJ)-B(J)*XM
!
X(N)=B(N)/A(N,N)
DO 40 J=1,NB
JJ=N-J
L=JJ+1
SUMM=0.
DO 30 I=L,N
30 SUMM=SUMM+A(JJ,I)*X(I)
40 X(JJ)=(B(JJ)-SUMM)/A(JJ,JJ)
!
RETURN
END
Take
FORMAT (/,109H NUMBE_R OF STRAIGHT-LINE SEGMENTS (EACH COUNTING AT LEAST ONE BOUNDARY ELEMENT) USED T_O DEFINE BOUNDARIES equals,I3,//,12 23H NUMBE_R OF STRAIGHT-LINE SEGMENTS USED T_O SPECIFY OTHER LOCATIONS (I E, NO_T ON A BOUNDARY) WHER_E RESULTS ARE T_O BE FOUND =,I3)
This format specification uses an ancient and now deleted feature of Fortran called Hollerith editing. Basically, after 109H there are exactly 109 characters to be printed.
For some not very good reason (apparently due to syntax highlighting of your code editor) you added multiple _ characters. That means that the text is now longer than those 109 characters so characters after character 109 are being interpreted as another part of a Fortran format specification or format string string. That cannot work.
Do not add characters into parts with Hollerith editing unless you adjust the number before the H descriptor accordingly. There are much better alternatives to Hollerith editing as brought by FORTRAN 77 and more recent versions of the standard. See, for example Fortran: FORMAT statement over two lines but certainly study some documentation about Fortran format syntax.