!-------------------------------------------------------------------------- !---------------------------- compute_NH_geopot ---------------------------------- tau2_g=tau*tau/g g2=g*g gm2 = 1./g2 gamma = 1./(1.-kappa) !$OMP BARRIER ! compute Phi_star DO l = 1,llm+1 DO ij=ij_omp_begin_ext,ij_omp_end_ext Phi_star_il(ij,l) = Phi_il(ij,l) + tau*g2*(W_il(ij,l)/m_il(ij,l)-tau) END DO END DO ! Newton-Raphson iteration : Phi_il contains current guess value DO iter=1,2 ! 2 iterations should be enough ! Compute pressure, A_ik SELECT CASE(caldyn_thermo) CASE(thermo_theta) DO l = 1,llm DO ij=ij_omp_begin_ext,ij_omp_end_ext rho_ij = (g*m_ik(ij,l))/(Phi_il(ij,l+1)-Phi_il(ij,l)) X_ij = (cpp/preff)*kappa*theta(ij,l)*rho_ij p_ik(ij,l) = preff*(X_ij**gamma) c2_mik = gamma*p_ik(ij,l)/(rho_ij*m_ik(ij,l)) ! c^2 = gamma*R*T = gamma*p/rho A_ik(ij,l) = c2_mik*(tau/g*rho_ij)**2 END DO END DO CASE(thermo_entropy) DO l = 1,llm DO ij=ij_omp_begin_ext,ij_omp_end_ext rho_ij = (g*m_ik(ij,l))/(Phi_il(ij,l+1)-Phi_il(ij,l)) X_ij = Treff*exp(theta(ij,l)/cpp) ! theta = Tref.exp(s/Cp) X_ij = (cpp/preff)*kappa*X_ij*rho_ij p_ik(ij,l) = preff*(X_ij**gamma) c2_mik = gamma*p_ik(ij,l)/(rho_ij*m_ik(ij,l)) ! c^2 = gamma*R*T = gamma*p/rho A_ik(ij,l) = c2_mik*(tau/g*rho_ij)**2 END DO END DO CASE DEFAULT PRINT *, 'caldyn_thermo not supported by compute_NH_geopot', caldyn_thermo STOP END SELECT ! NB : A(1), A(llm), R(1), R(llm+1) = 0 => x(l)=0 at l=1,llm+1 => flat, rigid top and bottom ! Solve -A(l-1)x(l-1) + B(l)x(l) - A(l)x(l+1) = R(l) using Thomas algorithm ! Compute residual R_il and B_il DO ij=ij_omp_begin_ext,ij_omp_end_ext ! bottom interface l=1 ml_g2 = gm2*m_il(ij,1) B_il(ij,1) = A_ik(ij,1) + ml_g2 + tau2_g*rho_bot R_il(ij,1) = ml_g2*( Phi_il(ij,1)-Phi_star_il(ij,1)) & + tau2_g*( p_ik(ij,1)-pbot+rho_bot*(Phi_il(ij,1)-PHI_BOT(ij)) ) END DO DO l = 2,llm DO ij=ij_omp_begin_ext,ij_omp_end_ext ! inner interfaces ml_g2 = gm2*m_il(ij,l) B_il(ij,l) = A_ik(ij,l)+A_ik(ij,l-1) + ml_g2 R_il(ij,l) = ml_g2*( Phi_il(ij,l)-Phi_star_il(ij,l)) & + tau2_g*(p_ik(ij,l)-p_ik(ij,l-1)) ! consistency check : if Wil=0 and initial state is in hydrostatic balance ! then Phi_star_il(ij,l) = Phi_il(ij,l) - tau^2*g^2 ! and residual = tau^2*(ml+(1/g)dl_pi)=0 END DO END DO DO ij=ij_omp_begin_ext,ij_omp_end_ext ! top interface l=llm+1 ml_g2 = gm2*m_il(ij,llm+1) B_il(ij,llm+1) = A_ik(ij,llm+1 -1) + ml_g2 R_il(ij,llm+1) = ml_g2*( Phi_il(ij,llm+1)-Phi_star_il(ij,llm+1)) & + tau2_g*( ptop-p_ik(ij,llm+1 -1) ) END DO ! ! Forward sweep : ! C(0)=0, C(l) = -A(l) / (B(l)+A(l-1)C(l-1)), ! D(0)=0, D(l) = (R(l)+A(l-1)D(l-1)) / (B(l)+A(l-1)C(l-1)) DO ij=ij_omp_begin_ext,ij_omp_end_ext X_ij = 1./B_il(ij,1) C_ik(ij,1) = -A_ik(ij,1) * X_ij D_il(ij,1) = R_il(ij,1) * X_ij END DO DO l = 2,llm DO ij=ij_omp_begin_ext,ij_omp_end_ext X_ij = 1./( B_il(ij,l) + A_ik(ij,l-1)*C_ik(ij,l-1) ) C_ik(ij,l) = -A_ik(ij,l) * X_ij D_il(ij,l) = (R_il(ij,l)+A_ik(ij,l-1)*D_il(ij,l-1)) * X_ij END DO END DO DO ij=ij_omp_begin_ext,ij_omp_end_ext X_ij = 1./( B_il(ij,llm+1) + A_ik(ij,llm+1 -1)*C_ik(ij,llm+1 -1) ) D_il(ij,llm+1) = (R_il(ij,llm+1)+A_ik(ij,llm+1 -1)*D_il(ij,llm+1 -1)) * X_ij ! Back substitution : ! x(i) = D(i)-C(i)x(i+1), x(llm+1)=0 ! + Newton-Raphson update ! top interface l=llm+1 x_il(ij,llm+1) = D_il(ij,llm+1) Phi_il(ij,llm+1) = Phi_il(ij,llm+1) - x_il(ij,llm+1) END DO DO l = llm,1,-1 DO ij=ij_omp_begin_ext,ij_omp_end_ext ! Back substitution at lower interfaces x_il(ij,l) = D_il(ij,l) - C_ik(ij,l)*x_il(ij,l+1) Phi_il(ij,l) = Phi_il(ij,l) - x_il(ij,l) END DO END DO IF(debug_hevi_solver) THEN PRINT *, '[hevi_solver] A,B', iter, MAXVAL(ABS(A_ik)),MAXVAL(ABS(B_il)) PRINT *, '[hevi_solver] C,D', iter, MAXVAL(ABS(C_ik)),MAXVAL(ABS(D_il)) DO l=1,llm+1 WRITE(*,'(A,I2.1,I3.2,E9.2)') '[hevi_solver] x_il', iter,l, MAXVAL(ABS(x_il(l,:))) END DO DO l=1,llm+1 WRITE(*,'(A,I2.1,I3.2,E9.2)') '[hevi_solver] R_il', iter,l, MAXVAL(ABS(R_il(l,:))) END DO END IF END DO ! Newton-Raphson !$OMP BARRIER debug_hevi_solver=.FALSE. !---------------------------- compute_NH_geopot ---------------------------------- !--------------------------------------------------------------------------