📄 acousticf90.f90
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!INTEGER N, niters!REAL check!N = 128!niters = 128*3!CALL echo_f90(N, niters, check)!PRINT *, check!ENDSUBROUTINE echo_f90(N, niters, check) INTEGER, INTENT( IN ) :: N, niters REAL, INTENT( OUT ) :: check REAL, DIMENSION (N,N) :: P1, P2, P3, c INTEGER iter CALL echo_f90_setupInitialConditions(c, P1, P2, P3, N) CALL checkArray_f90(P2, N) CALL checkArray_f90(c, N) DO iter=1, niters P3(2:N-1,2:N-1) = (2-4*c(2:N-1,2:N-1)) * P2(2:N-1,2:N-1) & + c(2:N-1,2:N-1)*(P2(1:N-2,2:N-1) + P2(3:N,2:N-1) & + P2(2:N-1,1:N-2) + P2(2:N-1,3:N)) - P1(2:N-1,2:N-1) P1 = P2 P2 = P3 END DO check = P1(N/2,7*N/8) RETURNENDSUBROUTINE echo_f90_setupInitialConditions(c, P1, P2, P3, N) INTEGER, INTENT( IN ) :: N REAL, DIMENSION (N,N) :: P1(N,N), P2(N,N), P3(N,N), c(N,N) INTEGER blockLeft, blockRight, blockTop, blockBottom INTEGER channelLeft, channelRight, channel1Height, channel2Height REAL cr, cc INTEGER i, j REAL s2 ! Set the velocity field c = 0.2 ! Solid block with which the pulse collides blockLeft = 1 blockRight = 2 * N / 5.0 blockTop = N / 3.0 blockBottom = 2 * N / 3.0 c(blockTop:blockBottom, blockLeft:blockRight) = 0.5 ! Channel directing the pulse leftwards channelLeft = 4 * N / 5.0 channelRight = N channel1Height = 3 * N / 8.0 channel2Height = 5 * N / 8.0 c(channel1Height,channelLeft:channelRight) = 0.0; c(channel2Height,channelLeft:channelRight) = 0.0; ! Initial pressure distribution: a gaussian pulse inside the channel cr = N / 2.0 cc = 7.0 * N / 8.0 s2 = 64.0 * 9.0 / ((N / 2.0) ** 2) DO j=1,N DO i=1,N P2(i,j) = exp(-((i-cr)**2 + (j-cc)**2) * s2) END DO END DO P1 = 0.0 P3 = 0.0END SUBROUTINE checkArray_f90(A, N) INTEGER N REAL, DIMENSION(N,N) :: A INTEGER i,j REAL check check = 0.0 DO j=1,N DO i=1,N check = check + (i*n+j)*A(i,j) END DO END DO PRINT *, 'Array check: ', check RETURN END
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