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[求助]
Compaq Visual Fortran v6.6 Professional运行后提示这样的信息，怎么办？求助
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 各位大神，Compaq Visual Fortran v6.6 Professional运行后提示这样的信息，怎么办？求指导。 附上程序代码 C ***** TETRA3D ***** C *** Three Dimensional Stress Analysis *** C *** Tetrahedral Elements *** DIMENSION X(100,3),NOC(100,4),MAT(100),PM(10,3),NU(50),U(50) DIMENSION S(300,50),F(300),D(6,6),B(6,12),DB(6,12),QT(12) DIMENSION SE(12,12),STR(6),MPC(20,2),BT(20,3),DT(100) CHARACTER*16 FILE1, FILE2 CHARACTER*81 DUMMY,TITLE IMAX = 300 PRINT *, '******* PROGRAM TETRA3D *******' PRINT *, '* Three Dimensional Stress Analysis *' PRINT *, '* Tetrahedral Elements *' PRINT *, '* T.R.Chandrupatla and A.D.Belegundu *' PRINT *, '*******************************************' PRINT *, 'File Name for Input Data ' READ '(A)', FILE1 LINP=10 OPEN (UNIT = 10, FILE = FILE1, STATUS = 'OLD') PRINT *, 'Give Name of Output File ' READ '(A)', FILE2 READ(LINP,'(A)') DUMMY READ(LINP,'(A)') TITLE READ(LINP,'(A)') DUMMY READ(LINP,*) NN, NE, NM, NDIM, NEN, NDN READ(LINP,'(A)') DUMMY READ(LINP,*) ND, NL, NMPC C --- Material properties E, Nu, Alpha NPR = 3 C ----- Total dof is NQ NQ = NDN * NN C ============ READ DATA FROM FILE =========== C ----- Coordinates ----- READ(LINP,'(A)') DUMMY DO 900 I = 1, NN 900 READ (LINP, *) N, X(N,1), X(N,2), X(N,3) C ----- Connectivity, Material, Temp-change ----- READ(LINP,'(A)') DUMMY DO 1000 I=1,NE READ (LINP, *) N,NOC(N,1),NOC(N,2),NOC(N,3),NOC(N,4),MAT(N),DT(N) 1000 CONTINUE C ----- Specified Displacements ----- READ(LINP,'(A)') DUMMY DO 1010 I = 1, ND 1010 READ (LINP, *) NU(I), U(I) C ----- Component Loads ----- READ(LINP,'(A)') DUMMY C ----- First initialize and then read loads ----- DO 1015 I=1, NQ 1015 F(I) = 0 DO 1020 I = 1, NL 1020 READ (LINP, *) N, F(N) C ----- Material Properties ----- READ(LINP,'(A)') DUMMY DO 1030 I = 1, NM 1030 READ (LINP, *) N, (PM(N, J), J = 1, NPR) C ----- Multi-point Constraints B1*Qi+B2*Qj=B0 IF (NMPC .GT. 0) THEN READ(LINP,'(A)') DUMMY DO 1040 I = 1, NMPC 1040 READ (LINP,*) BT(I,1),MPC(I,1),BT(I,2),MPC(I,2),BT(I,3) END IF CLOSE(LINP) C ----- Bandwidth Evaluation ----- NBW = 0 DO 1050 I = 1, NE NMIN = NOC(I, 1) NMAX = NOC(I, 1) DO 1045 J = 2, NEN IF (NMIN .GT. NOC(I, J)) NMIN = NOC(I, J) IF (NMAX .LT. NOC(I, J)) NMAX = NOC(I, J) 1045 CONTINUE NTMP = NDN * (NMAX - NMIN + 1) IF (NBW .LT. NTMP) NBW = NTMP 1050 CONTINUE DO 1060 I = 1, NMPC NABS = ABS(MPC(I, 1) - MPC(I, 2)) + 1 IF (NBW .LT. NABS) NBW = NABS 1060 CONTINUE PRINT *, 'Bandwidth = ', NBW C ----- First initialize stiffness and Mass matrices DO 1070 I = 1, NQ DO 1070 J = 1, NBW 1070 S(I,J) = 0 C ----- Global Stiffness Matrix ----- DO 1090 N = 1, NE PRINT *, 'Forming Stiffness Matrix of Element ', N CALL DBMAT(N,B,D,DB,MAT,PM,X,NOC,DJ,AL,PNU) C --- Element Stiffness DO 1072 I = 1, 12 DO 1072 J = 1, 12 SE(I, J) = 0 DO 1072 K = 1, 6 SE(I, J) = SE(I, J) + B(K, I) * DB(K, J) * ABS(DJ) / 6 1072 CONTINUE C --- Temperature Load Vector QT() C = AL * DT(N) DO 1074 I = 1, 12 DSUM = DB(1, I) + DB(2, I) + DB(3, I) QT(I) = C * ABS(DJ) * DSUM / 6 1074 CONTINUE PRINT *, '.... Placing in Global Locations' DO 1090 II = 1, NEN NRT = NDN * (NOC(N, II) - 1) DO 1090 IT = 1, NDN NR = NRT + IT I = NDN * (II - 1) + IT DO 1080 JJ = 1, NEN NCT = NDN * (NOC(N, JJ) - 1) DO 1080 JT = 1, NDN J = NDN * (JJ - 1) + JT NC = NCT + JT - NR + 1 IF (NC .GT. 0) THEN S(NR, NC) = S(NR, NC) + SE(I, J) END IF 1080 CONTINUE F(NR) = F(NR) + QT(I) 1090 CONTINUE C ----- Decide Penalty Parameter CNST ----- CNST = 0 DO 1100 I = 1, NQ IF (CNST .LT. S(I, 1)) CNST = S(I, 1) 1100 CONTINUE CNST = CNST * 10000 C ----- Modify for Boundary Conditions ----- C --- Displacement BC --- DO 1110 I = 1, ND N = NU(I) S(N, 1) = S(N, 1) + CNST F(N) = F(N) + CNST * U(I) 1110 CONTINUE C --- Multi-point Constraints --- DO 1120 I = 1, NMPC I1 = MPC(I, 1) I2 = MPC(I, 2) S(I1, 1) = S(I1, 1) + CNST * BT(I, 1) * BT(I, 1) S(I2, 1) = S(I2, 1) + CNST * BT(I, 2) * BT(I, 2) IR = I1 IF (IR .GT.I2) IR = I2 IC = ABS(I2 - I1) + 1 S(IR, IC) = S(IR, IC) + CNST * BT(I, 1) * BT(I, 2) F(I1) = F(I1) + CNST * BT(I, 1) * BT(I, 3) F(I2) = F(I2) + CNST * BT(I, 2) * BT(I, 3) 1120 CONTINUE C ----- Equation Solving PRINT *, '.... Solving Equations' CALL BAND(S, F, IMAX, NBW, NQ) LOUT = 11 OPEN (UNIT = 11, FILE = FILE2) WRITE(LOUT,'(1X,2A)') 'Output for Input Data from File ', FILE1 PRINT *, 'Output for Input Data from File ', FILE1 WRITE(LOUT,'(1X,A)') TITLE PRINT *, TITLE PRINT *, 'Node# X-Displ Y-Displ Z-Displ' WRITE(LOUT,'(1X,A)') 'Node# X-Displ Y-Displ Z-Displ' WRITE(LOUT,'(1X,I4,3E15.4)') (I,F(3*I-2),F(3*I-1),F(3*I),I=1,NN) WRITE(*,'(1X,I4,3E15.4)') (I,F(3*I-2),F(3*I-1),F(3*I),I=1,NN) C ----- Reaction Calculation ----- PRINT *, 'DOF# Reaction' WRITE(LOUT,'(1X,A)') 'DOF# Reaction' DO 1140 I = 1, ND N = NU(I) R = CNST * (U(I) - F(N)) WRITE(*,'(1X,I4,E15.4)') N, R WRITE(LOUT,'(1X,I4,E15.4)') N, R 1140 CONTINUE C --- Stress Calculations PI = 3.141593 DO 1150 N = 1, NE CALL DBMAT(N,B,D,DB,MAT,PM,X,NOC,DJ,AL,PNU) CALL STRESS(F,AL,NOC,DT,N,D,DB,STR) C --- Principal Stress Calculations AI1 = STR(1) + STR(2) + STR(3) AI21 = STR(1) * STR(2) + STR(2) * STR(3) + STR(3) * STR(1) AI22 = STR(4) * STR(4) + STR(5) * STR(5) + STR(6) * STR(6) AI2 = AI21 - AI22 AI31 = STR(1) * STR(2) * STR(3) + 2 * STR(4) * STR(5) * STR(6) AI32 = STR(1)*STR(4)**2 + STR(2)*STR(5)**2 + STR(3)*STR(6)**2 AI3 = AI31 - AI32 C1 = AI2 - AI1**2 / 3 C2 = -2 * (AI1 / 3)**3 + AI1 * AI2 / 3 - AI3 C3 = 2 * SQRT(-C1 / 3) TH = -3 * C2 / (C1 * C3) TH2 = ABS(1 - TH * TH) IF (TH .EQ. 0) TH = PI / 2 IF (TH .GT. 0) TH = ATAN(SQRT(TH2) / TH) IF (TH .LT. 0) TH = PI - ATAN(SQRT(TH2) / TH) TH = TH / 3 C --- Principal Stresses P1 = AI1 / 3 + C3 * COS(TH) P2 = AI1 / 3 + C3 * COS(TH + 2 * PI / 3) P3 = AI1 / 3 + C3 * COS(TH + 4 * PI / 3) WRITE(LOUT,*) ' ELEMENT NO. ' WRITE(LOUT,'(I5)') N WRITE(LOUT,*) ' SX SY SZ' WRITE(LOUT,'(3E15.4)') STR(1), STR(2), STR(3) WRITE(LOUT,*) ' TYZ TXZ TXY' WRITE(LOUT,'(3E15.4)') STR(4), STR(5), STR(6) WRITE(LOUT,*) ' Principal Stresses' WRITE(LOUT,*) ' P1 P2 P3' WRITE(LOUT,'(3E15.4)') P1, P2, P3 1150 CONTINUE CLOSE(LOUT) PRINT *, 'Results are in the file ',FILE2 END SUBROUTINE DBMAT(N,B,D,DB,MAT,PM,X,NOC,DJ,AL,PNU) DIMENSION X(100,3),NOC(100,4),MAT(100),PM(10,3) DIMENSION D(6,6),B(6,12),DB(6,12) C ----- D(), B() and DB() matrices C --- First the D-Matrix M = MAT(N) E = PM(M, 1) PNU = PM(M, 2) AL = PM(M, 3) C4 = E / ((1 + PNU) * (1 - 2 * PNU)) C1 = C4 * (1 - PNU) C2 = C4 * PNU C3 = .5 * E / (1 + PNU) DO 3000 I = 1, 6 DO 3000 J = 1, 6 D(I, J) = 0 3000 CONTINUE D(1, 1) = C1 D(1, 2) = C2 D(1, 3) = C2 D(2, 1) = C2 D(2, 2) = C1 D(2, 3) = C2 D(3, 1) = C2 D(3, 2) = C2 D(3, 3) = C1 D(4, 4) = C3 D(5, 5) = C3 D(6, 6) = C3 C --- Strain-Displacement Matrix B() I1 = NOC(N, 1) I2 = NOC(N, 2) I3 = NOC(N, 3) I4 = NOC(N, 4) X14 = X(I1, 1) - X(I4, 1) X24 = X(I2, 1) - X(I4, 1) X34 = X(I3, 1) - X(I4, 1) Y14 = X(I1, 2) - X(I4, 2) Y24 = X(I2, 2) - X(I4, 2) Y34 = X(I3, 2) - X(I4, 2) Z14 = X(I1, 3) - X(I4, 3) Z24 = X(I2, 3) - X(I4, 3) Z34 = X(I3, 3) - X(I4, 3) DJ1 = X14 * (Y24 * Z34 - Z24 * Y34) DJ2 = Y14 * (Z24 * X34 - X24 * Z34) DJ3 = Z14 * (X24 * Y34 - Y24 * X34) DJ = DJ1 + DJ2 + DJ3 A11 = (Y24 * Z34 - Z24 * Y34) / DJ A21 = (Z24 * X34 - X24 * Z34) / DJ A31 = (X24 * Y34 - Y24 * X34) / DJ A12 = (Y34 * Z14 - Z34 * Y14) / DJ A22 = (Z34 * X14 - X34 * Z14) / DJ A32 = (X34 * Y14 - Y34 * X14) / DJ A13 = (Y14 * Z24 - Z14 * Y24) / DJ A23 = (Z14 * X24 - X14 * Z24) / DJ A33 = (X14 * Y24 - Y14 * X24) / DJ C --- B Matrix DO 3010 I = 1, 6 DO 3010 J = 1, 12 3010 B(I, J) = 0 B(1, 1) = A11 B(1, 4) = A12 B(1, 7) = A13 B(1, 10) = -A11 - A12 - A13 B(2, 2) = A21 B(2, 5) = A22 B(2, 8) = A23 B(2, 11) = -A21 - A22 - A23 B(3, 3) = A31 B(3, 6) = A32 B(3, 9) = A33 B(3, 12) = -A31 - A32 - A33 B(4, 2) = A31 B(4, 3) = A21 B(4, 5) = A32 B(4, 6) = A22 B(4, 8) = A33 B(4, 9) = A23 B(4, 11) = B(3, 12) B(4, 12) = B(2, 11) B(5, 1) = A31 B(5, 3) = A11 B(5, 4) = A32 B(5, 6) = A12 B(5, 7) = A33 B(5, 9) = A13 B(5, 10) = B(3, 12) B(5, 12) = B(1, 10) B(6, 1) = A21 B(6, 2) = A11 B(6, 4) = A22 B(6, 5) = A12 B(6, 7) = A23 B(6, 8) = A13 B(6, 10) = B(2, 11) B(6, 11) = B(1, 10) C --- DB Matrix DB = D*B DO 3020 I = 1, 6 DO 3020 J = 1, 12 DB(I, J) = 0 DO 3020 K = 1, 6 3020 DB(I, J) = DB(I, J) + D(I, K) * B(K, J) RETURN END SUBROUTINE STRESS(F,AL,NOC,DT,N,D,DB,STR) DIMENSION F(300),NOC(100,4),D(6,6),DB(6,12),QT(12),STR(6),DT(100) C --- Stress Evaluation (Element Nodal Displacements stored in QT() ) DO 4000 I = 1, 4 IN = 3 * (NOC(N, I) - 1) II = 3 * (I - 1) DO 4000 J = 1, 3 QT(II + J) = F(IN + J) 4000 CONTINUE C1 = AL * DT(N) DO 4020 I = 1, 6 STR(I) = 0 DO 4010K = 1, 12 4010 STR(I) = STR(I) + DB(I, K) * QT(K) 4020 STR(I) = STR(I) - C1 * (D(I, 1) + D(I, 2) + D(I, 3)) RETURN END SUBROUTINE BAND(A, B, IMAX, NBW, N) C ----- Equation Solving Using Banded Storage DIMENSION A(IMAX,NBW), B(IMAX) N1 = N - 1 PRINT *, '*** FORWARD ELIMINATION ***' DO 2100 K = 1, N1 NK = N - K + 1 IF (NK .GT. NBW) NK = NBW DO 2100 I = 2, NK C1 = A(K, I) / A(K, 1) I1 = K + I - 1 DO 2000 J = I, NK J1 = J - I + 1 2000 A(I1, J1) = A(I1, J1) - C1 * A(K, J) 2100 B(I1) = B(I1) - C1 * B(K) PRINT *, '*** BACK SUBSTITUTION ***' B(N) = B(N) / A(N, 1) DO 2300 KK = 1, N1 K = N - KK C1 = 1 / A(K, 1) B(K) = C1 * B(K) NK = N - K + 1 IF (NK .GT. NBW) NK = NBW DO 2200 J = 2, NK B(K) = B(K) - C1 * A(K, J) * B(K + J - 1) 2200 CONTINUE 2300 CONTINUE RETURN END  QQ Photo20140427183700.jpg |
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