Flux splitting scheme: AUSM+
!< Flux splitting scheme: AUSM+ module ausmP !< Flux splitting scheme: AUSM+ module ausmP !< !< Reference: Liou, M. S., “A sequel to AUSM: AUSM+,” !< Journal of Computational Physics, vol. 129, pp. 364–382, 1996 !------------------------------------------------------------------- #include "../../../debug.h" #include "../../../error.h" use vartypes use face_interpolant, only: x_qp_left, x_qp_right use face_interpolant, only: y_qp_left, y_qp_right use face_interpolant, only: z_qp_left, z_qp_right implicit none private public :: compute_fluxes contains subroutine compute_flux(Flux, f_qp_left, f_qp_right, faces, flags, flow, bc, dims) !< A generalized subroutine to calculate !< flux through the input direction, :x,y, or z !< which corresponds to the I,J, or K direction respectively !------------------------------------------------------------ implicit none integer, dimension(3), intent(in) :: flags !< flags for direction switch type(extent), intent(in) :: dims !< Extent of the domain:imx,jmx,kmx type(flowtype), intent(in) :: flow !< Information about fluid flow: freestream-speed, ref-viscosity,etc. type(boundarytype), intent(in) :: bc !< boundary conditions and fixed values real(wp), dimension(:, :, :, :), intent(inout) :: Flux !< Store fluxes throught the any(I,J,K) faces type(facetype), dimension(-2:dims%imx+2+flags(1),-2:dims%jmx+2+flags(2),-2:dims%kmx+2+flags(3)), intent(in) :: faces !< Face quantities: area and unit normal real(wp), dimension(1-flags(1):dims%imx-1+2*flags(1), 1-flags(2):dims%jmx-1+2*flags(2), 1-flags(3):dims%kmx-1+2*flags(3), 1:dims%n_var), intent(inout) :: f_qp_left, f_qp_right !< primitve state variable at face integer :: i, j, k !< Integer for DO loop integer :: i_f, j_f, k_f !< Flags to determine face direction real(wp), dimension(1:dims%n_var) :: F_plus !< Right flux through the face real(wp), dimension(1:dims%n_var) ::F_minus !< Left flux through the face real(wp) :: pbar real(wp) :: mass real(wp) :: HL, HR !< Enthalpy real(wp) :: uL, uR !< X-component of velocity real(wp) :: vL, vR !< Y-component of velocity real(wp) :: wL, wR !< Z-component of velocity real(wp) :: pL, pR !< Pressure real(wp) :: rL, rR !< Density real(wp) :: cL, cR !< Speed sound left/right real(wp) :: C !< Speed of sound at face real(wp) :: ML, MR !< Mach number left/right real(wp) :: VnL, VnR !< Face normal velocity left/right real(wp) :: betaL, betaR real(wp) :: alphaL, alphaR real(wp) :: FmL, FmR real(wp) :: Mface real(wp) :: Cs DebugCall('compute_flux '//trim(f_dir)) i_f = flags(1) j_f = flags(2) k_f = flags(3) do k = 1, dims%kmx - 1 + k_f do j = 1, dims%jmx - 1 + j_f do i = 1, dims%imx - 1 + i_f ! -- primitve face state assignment -- ! ---- left face quantities ---- rL = f_qp_left(i,j,k,1) uL = f_qp_left(i,j,k,2) vL = f_qp_left(i,j,k,3) wL = f_qp_left(i,j,k,4) pL = f_qp_left(i,j,k,5) ! ---- right face quantities ---- rR = f_qp_right(i,j,k,1) uR = f_qp_right(i,j,k,2) vR = f_qp_right(i,j,k,3) wR = f_qp_right(i,j,k,4) pR = f_qp_right(i,j,k,5) !-- calculated quntaties -- ! ---- total enthalpy ---- HL = (0.5*(uL*uL + vL*vL + wL*wL)) + ((flow%gm/(flow%gm - 1.))*pL/rL) HR = (0.5*(uR*uR + vR*vR + wR*wR)) + ((flow%gm/(flow%gm - 1.))*pR/rR) ! ---- face normal velocity ---- VnL = uL*faces(i, j, k)%nx + vL*faces(i, j, k)%ny + wL*faces(i, j, k)%nz VnR = uR*faces(i, j, k)%nx + vR*faces(i, j, k)%ny + wR*faces(i, j, k)%nz ! ---- speed of sound ---- cs = sqrt(2.0*(flow%gm-1.0)*(0.5*(HL + HR))/(flow%gm+1.0)) cL = cs*cs/(max(cs, abs(VnL))) cR = cs*cs/(max(cs, abs(VnR))) C = min(cL, CR) ! ---- Mach at face ---- ML = VnL/C MR = VnR/C ! ---- switch for supersonic flow ---- alphaL= max(0, 1-floor(abs(ML))) alphaR= max(0, 1-floor(abs(MR))) ! Compute '+' direction quantities FmL = (0.5*(1.0+sign(1.0,ML))*(1.0-alphaL)*ML) + alphaL*0.25*((1.0+ML)**2) betaL = (0.5*(1.0+sign(1.0,ML))*(1.0-alphaL)) + alphaL*0.25*((1.0+ML)**2) * (2.0 - ML) ! Compute '-' direction quantities FmR = (0.5*(1.0-sign(1.0,MR))*(1.0-alphaR)*MR) - alphaR*0.25*((1.0-MR)**2) betaR = (0.5*(1.0-sign(1.0,MR))*(1.0-alphaR)) + alphaR*0.25*((1.0-MR)**2)*(2.0 + MR) !AUSM+modification ! Compute '+' direction quantities FmL = FmL + alphaL*0.1250*((ML**2-1.0)**2) betaL = betaL + alphaL*0.1875*((ML**2-1.0)**2)*ML ! Compute '-' direction quantities FmR = FmR - alphaR*0.1250*((MR**2-1.0)**2) betaR = betaR - alphaR*0.1875*((MR**2-1.0)**2)*MR ! mass coefficient Mface = FmL + FmR ! -- Pressure coeffient-- pbar = betaL*pL + betaR*pR ! -- mass -- if(Mface>0.0)then mass = Mface*C*rL else mass = Mface*c*rR end if mass = mass *(i_f*bc%make_F_flux_zero(i) & + j_f*bc%make_G_flux_zero(j) & + k_f*bc%make_H_flux_zero(k)) ! F plus mass flux ! Construct other fluxes in terms of the F mass flux F_plus(1) = 0.5*(mass + abs(mass)) F_plus(2) = (F_plus(1) * uL) F_plus(3) = (F_plus(1) * vL) F_plus(4) = (F_plus(1) * wL) F_plus(5) = (F_plus(1) * HL) ! F minus mass flux ! Construct other fluxes in terms of the F mass flux F_minus(1) = 0.5*(mass - abs(mass)) F_minus(2) = (F_minus(1) * uR) F_minus(3) = (F_minus(1) * vR) F_minus(4) = (F_minus(1) * wR) F_minus(5) = (F_minus(1) * HR) !! -- Turbulence variables mass flux -- if(dims%n_var>5) then F_plus(6:) = F_Plus(1) * f_qp_left(i,j,k,6:) F_minus(6:) = F_minus(1) * f_qp_right(i,j,k,6:) end if ! total flux Flux(i, j, k, :) = F_plus(:) + F_minus(:) ! Get the total flux for a face ! -- Pressure flux addition -- Flux(i, j, K, 2) = Flux(i, j, k, 2) + (pbar * faces(i, j, k)%nx) Flux(i, j, K, 3) = Flux(i, j, k, 3) + (pbar * faces(i, j, k)%ny) Flux(i, j, K, 4) = Flux(i, j, k, 4) + (pbar * faces(i, j, k)%nz) Flux(i, j, k, :) = Flux(i, j, k, :)*faces(i,j,k)%A end do end do end do end subroutine compute_flux subroutine compute_fluxes(F,G,H, x_qp_l, x_qp_r, y_qp_l, y_qp_r, z_qp_l, z_qp_r, Ifaces, Jfaces, Kfaces, flow, bc, dims) !subroutine compute_fluxes(F,G,H, flow, dims) !< Call to compute fluxes throught faces in each direction implicit none type(extent), intent(in) :: dims !< Extent of the domain:imx,jmx,kmx type(flowtype), intent(in) :: flow !< Information about fluid flow: freestream-speed, ref-viscosity,etc. real(wp), dimension(:, :, :, :), intent(inout) :: F !< Store fluxes throught the I faces real(wp), dimension(:, :, :, :), intent(inout) :: G !< Store fluxes throught the J faces real(wp), dimension(:, :, :, :), intent(inout) :: H !< Store fluxes throught the K faces type(facetype), dimension(-2:dims%imx+3,-2:dims%jmx+2,-2:dims%kmx+2), intent(in) :: Ifaces !< Store face quantites for I faces type(facetype), dimension(-2:dims%imx+2,-2:dims%jmx+3,-2:dims%kmx+2), intent(in) :: Jfaces !< Store face quantites for J faces type(facetype), dimension(-2:dims%imx+2,-2:dims%jmx+2,-2:dims%kmx+3), intent(in) :: Kfaces !< Store face quantites for K faces real(wp), dimension(0:dims%imx+1,1:dims%jmx-1,1:dims%kmx-1,1:dims%n_var), intent(inout) :: x_qp_l, x_qp_r !< Store primitive state at the I-face real(wp), dimension(1:dims%imx-1,0:dims%jmx+1,1:dims%kmx-1,1:dims%n_var), intent(inout) :: y_qp_l, y_qp_r !< Store primitive state at the J-face real(wp), dimension(1:dims%imx-1,1:dims%jmx-1,0:dims%kmx+1,1:dims%n_var), intent(inout) :: z_qp_l, z_qp_r !< Store primitive state at the K-face type(boundarytype), intent(in) :: bc !< boundary conditions and fixed values integer, dimension(3) :: flags DebugCall('compute_fluxes') flags=(/1,0,0/) call compute_flux(F, x_qp_l, x_qp_r, Ifaces, flags, flow, bc, dims) if (any(isnan(F))) then Fatal_error end if flags=(/0,1,0/) call compute_flux(G, y_qp_l, y_qp_r, Jfaces, flags, flow, bc, dims) if (any(isnan(G))) then Fatal_error end if if(dims%kmx==2) then H = 0. else flags=(/0,0,1/) call compute_flux(H, z_qp_l, z_qp_r, Kfaces, flags, flow, bc, dims) end if if (any(isnan(H))) then Fatal_error end if end subroutine compute_fluxes end module ausmP