📄 acousticf.f
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! INTEGER N, iters! REAL check! N = 128! iters = N*3! CALL echo_f77(N,iters,check)! PRINT *, check! END SUBROUTINE echo_f77(N, niters, check) INTEGER N, niters, iter REAL check REAL P1(N,N), P2(N,N), P3(N,N), C(N,N) INTEGER i, j CALL echo_f77_set(c, P1, P2, P3, N) CALL checkArray(P2, N) CALL checkArray(c, N) DO iter=1, niters DO j=2,N-1 DO i=2,N-1 P3(i,j) = (2-4*c(i,j))*P2(i,j) + c(i,j)*(P2(i,j-1) . + P2(i,j+1) + P2(i-1,j) + P2(i+1,j)) - P1(i,j) END DO END DO DO j=1,N DO i=1,N P1(i,j) = P2(i,j) P2(i,j) = P3(i,j) END DO END DO END DO check = P1(N/2,7*N/8) RETURN END SUBROUTINE echo_f77_set(c, P1, P2, P3, N) INTEGER N REAL c(N,N), P1(N,N), P2(N,N), P3(N,N) INTEGER i, j, blockLeft, blockRight, blockTop, blockBottom INTEGER channelLeft, channelRight, channel1Height, channel2Height INTEGER cr, cc REAL s2! Default velocity in the air DO j=1,N DO i=1,N c(i,j) = 0.2 END DO END DO ! Solid block with which the pulse collids blockLeft = 1 blockRight = 2 * N / 5.0 blockTop = N / 3.0 blockBottom = 2 * N / 3.0 DO j=blockLeft,blockRight DO i=blockTop,blockBottom c(i,j) = 0.5 END DO END DO! Channel directing the pulse leftwards channelLeft = 4 * N / 5.0 channelRight = N channel1Height = 3 * N / 8.0 channel2Height = 5 * N / 8.0 DO j = channelLeft,channelRight c(channel1Height,j) = 0.0 c(channel2Height,j) = 0.0 END DO! Initial pressure distribution: a gaussian pulse inside the channel cr = N / 2 cc = 7 * N / 8.0 s2 = 64.0 * 9.0 / ((N/2.0) ** 2) print *, 'cr = ', cr, ' cc = ', cc, ' s2 = ', s2 DO j=1,N DO i=1,N P1(i,j) = 0.0 P2(i,j) = exp(-((i-cr)**2 + (j-cc)**2) * s2) P3(i,j) = 0.0 END DO END DO RETURN END SUBROUTINE checkArray(A, N) INTEGER N REAL A(N,N) 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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