! Copyright (c) 2015 Nikhil Anand <nikhil.anand@uni-siegen.de> ! Copyright (c) 2016-2017, 2020 Peter Vitt <peter.vitt2@uni-siegen.de> ! Copyright (c) 2016 Tobias Girresser <tobias.girresser@student.uni-siegen.de> ! Copyright (c) 2017 Daniel Petró <daniel.petro@student.uni-siegen.de> ! ! Permission to use, copy, modify, and distribute this software for any ! purpose with or without fee is hereby granted, provided that the above ! copyright notice and this permission notice appear in all copies. ! ! THE SOFTWARE IS PROVIDED "AS IS" AND THE AUTHORS DISCLAIM ALL WARRANTIES ! WITH REGARD TO THIS SOFTWARE INCLUDING ALL IMPLIED WARRANTIES OF ! MERCHANTABILITY AND FITNESS. IN NO EVENT SHALL THE AUTHORS BE LIABLE FOR ! ANY SPECIAL, DIRECT, INDIRECT, OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES ! WHATSOEVER RESULTING FROM LOSS OF USE, DATA OR PROFITS, WHETHER IN AN ! ACTION OF CONTRACT, NEGLIGENCE OR OTHER TORTIOUS ACTION, ARISING OUT OF ! OR IN CONNECTION WITH THE USE OR PERFORMANCE OF THIS SOFTWARE. ! **************************************************************************** ! !> author: Jens Zudrop !! Collects all functions related to the physical fluxes of the compressible Navier-Stokes equations. module atl_physFluxFilNvrStk_module ! Treelm modules use env_module, only: rk use tem_aux_module, only: tem_abort use atl_eqn_nvrstk_module, only: atl_Navier_stokes_rans_type use atl_eqn_filNvrStk_var_module, & & only: atl_get_pointwise_velocity_gradient_2D, & & atl_get_pointwise_visc_stress_tensor_2D, & & atl_get_lower_bound_turb_disscipation implicit none private public :: atl_viscPhysFluxRans public :: atl_PhysFluxRans public :: atl_PhysFluxRans_2d public :: atl_viscPhysFluxRans_2d, & & atl_mult_nu11_Rans_2d, atl_mult_nu21_Rans_2d, & & atl_mult_nu12_Rans_2d, atl_mult_nu22_Rans_2d contains !> Physical flux calculation along x direction for the ! filtered Navier Stokes equation. function atl_physFluxRans(state, isenCoeff, penalty_char, porosity) & & result(physFlux) ! --------------------------------------------------------------------------- !> The state in nodal space. Dimension is the number of vars, i.e. 5 for Euler ! and here =7 for renolds averaged navier stokes real(kind=rk), intent(in) :: state(:) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> The value of the characteristic function (stemming from penalization) real(kind=rk), intent(in) :: penalty_char !> The porosity at the current point real(kind=rk), intent(in) :: porosity !> The physical flux along the x axis for all variables real(kind=rk) :: physFlux(7) ! --------------------------------------------------------------------------- real(kind=rk) :: pressure, velocity(1:3), pressure_eff ! --------------------------------------------------------------------------- ! calculate pressure pressure = (isenCoeff-1.0_rk) * ( & & state(5) - 0.5_rk*(sum(state(2:4)**2))/state(1) & - state(6) ) pressure_eff = pressure + 2.0_rk * state(6) / 3.0_rk !> @todo JZ: here, we divide by a polynomial, we should be careful! We are leaving !! the polynomial space here! velocity(1:3) = state(2:4)/state(1) ! calculate the nonlinear term for different varibales now. ! ... density physFlux(1) = (1.0_rk + ((1.0_rk/porosity)-1.0_rk)*penalty_char) * state(2) ! ... x-velocity physFlux(2) = pressure_eff + state(2)*velocity(1) ! ... y-velocity physFlux(3) = state(2)*velocity(2) ! ... z-velocity physFlux(4) = state(2)*velocity(3) ! ... total energy physFlux(5) = velocity(1) * ( state(5) + pressure_eff ) ! ... turbulent KE physFlux(6) = state(2)*state(6)/ state(1) ! ... spec dissipation rate physFlux(7) = state(2)*state(7)/ state(1) end function atl_physFluxRans function atl_physFluxRans_2d(state, isenCoeff, penalty_char, porosity) & & result(physFlux) ! --------------------------------------------------------------------------- !> The state in nodal space. Dimension is the number of vars, i.e. 5 for Euler ! and here =7 for renolds averaged navier stokes real(kind=rk), intent(in) :: state(:) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> The value of the characteristic function (stemming from penalization) real(kind=rk), intent(in) :: penalty_char !> The porosity at the current point real(kind=rk), intent(in) :: porosity !> The physical flux along the x axis for all variables real(kind=rk) :: physFlux(6) ! --------------------------------------------------------------------------- real(kind=rk) :: pressure, velocity(1:2), pressure_eff ! --------------------------------------------------------------------------- ! calculate pressure pressure = (isenCoeff-1.0_rk) * ( & & state(4) - 0.5_rk*(sum(state(2:3)**2))/state(1) & - state(5) ) pressure_eff = pressure + 2.0_rk * state(5) / 3.0_rk !> @todo JZ: here, we divide by a polynomial, we should be careful! We are leaving !! the polynomial space here! velocity(1:2) = state(2:3)/state(1) ! calculate the nonlinear term for different varibales now. ! ... density physFlux(1) = (1.0_rk + ((1.0_rk/porosity)-1.0_rk)*penalty_char) * state(2) ! ... x-velocity physFlux(2) = pressure_eff + state(2)*velocity(1) ! ... y-velocity physFlux(3) = state(2)*velocity(2) ! ... total energy physFlux(4) = velocity(1) * ( state(4) + pressure_eff ) ! ... turbulent KE physFlux(5) = velocity(1)*state(5) ! ... spec dissipation rate physFlux(6) = velocity(1)*state(6) end function atl_physFluxRans_2d !> Physical flux calculation along x direction for Euler equation. function atl_viscPhysFluxRans(state, state_gradient, isenCoeff, mu, & & lambda, thermCond, heatCap ) result(physFlux) ! ------------------------------------------------------------------------------------ !> The state in nodal space. Dimension is the number of vars, i.e. 5 for Navier-Stokes. real(kind=rk), intent(in) :: state(:) !> The state in nodal space. First dimension is the number of vars, i.e. 5 for Navier-Stokes. !! Second dimension is the dimension, e.g. 3 in two dimensions. real(kind=rk), intent(in) :: state_gradient(:,:) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The thermal cond real(kind=rk), intent(in) :: thermCond !> The specific heat capacity (per mass unit mass, at constant volume) real(kind=rk), intent(in) :: heatCap !> The physical flux along the x axis for all variables real(kind=rk) :: physFlux(7) ! ------------------------------------------------------------------------------- real(kind=rk) :: velocity(1:3) ! The turbulent viscosity (dynamic) real(kind=rk) :: mu_turb ! The turbulent viscosity real(kind=rk) :: lam_turb ! The effective viscosity (dynamic) real(kind=rk) :: mu_eff ! The effective turbulent viscosity real(kind=rk) :: lam_eff real(kind=rk) :: energy_coeff real(kind=rk) :: sig_k real(kind=rk) :: sig_omg real(kind=rk) :: turbulent_prandtl_number ! ------------------------------------------------------------------------------- velocity(1:3) = state(2:4)/state(1) !mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) ! The code above was deactivated without adding a proper initialization ! for the variables. I'm letting the code abort when it is executed to ! inform the user that it is not yet usable. call tem_abort( "This routine doesn't use properly initialized variables" ) lam_turb = 2.0*mu_turb/3.0 mu_eff = mu + mu_turb lam_eff = lambda + lam_turb turbulent_prandtl_number = 0.9_rk sig_k = 0.5_rk sig_omg = 0.5_rk energy_coeff = thermCond/(heatCap*state(1)) & & + mu_turb*isenCoeff/(turbulent_prandtl_number*state(1)) ! Viscous flux for density physFlux(1) = 0.0_rk ! Viscous flux for momentum in x physFlux(2) = & ! (nu_{1,1})_{2,1} (\nabla u)_{1,1} : k = 1, i = 1 & ((-2.0_rk * mu_eff + lam_eff) / state(1))*velocity(1)*state_gradient(1,1) & ! (nu_{1,2})_{2,1} (\nabla u)_{1,2} : k = 2, i = 1 & + (lam_eff / state(1))*velocity(2)*state_gradient(1,2) & ! (nu_{1,3})_{2,1} (\nabla u)_{1,3} : k = 3, i = 1 & + (lam_eff / state(1))*velocity(3)*state_gradient(1,3) & ! (nu_{1,1})_{2,2} (\nabla u)_{2,1} : k = 1, i = 2 & + ((2.0_rk * mu_eff - lam_eff) / state(1))*state_gradient(2,1) & ! (nu_{1,2})_{2,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & !(nu_{1,3})_{2,2} (\nabla u)_{2,3} : k = 3, i = 2 & + 0.0_rk & ! (nu_{1,1})_{2,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{2,3} (\nabla u)_{3,2} : k = 2, i = 3 & + (-lam_eff/state(1))*state_gradient(3,2) & ! (nu_{1,3})_{2,3} (\nabla u)_{3,3} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,1})_{2,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{2,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{2,4} (\nabla u)_{4,3} : k = 3, i = 4 & + (-lam_eff/state(1))*state_gradient(4,3) & ! (nu_{1,1})_{2,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{2,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{2,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{2,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{2,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{2,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{2,7} (\nabla u)_{7,1} : k = 1, i = 7 & + 0.0_rk & ! (nu_{1,2})_{2,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{2,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk ! Viscous flux for momentum in y physFlux(3) = & ! (nu_{1,1})_{3,1} (\nabla u)_{1,1} : k = 1, i = 1 & (-mu_eff / state(1))*velocity(2)*state_gradient(1,1) & ! (nu_{1,2})_{3,1} (\nabla u)_{1,2} : k = 2, i = 1 & + (-mu_eff / state(1))*velocity(1)*state_gradient(1,2) & ! (nu_{1,3})_{3,1} (\nabla u)_{1,3} : k = 3, i = 1 & + 0.0_rk & ! (nu_{1,1})_{3,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{3,2} (\nabla u)_{2,2} : k = 2, i = 2 & + (mu_eff/state(1))*state_gradient(2,2) & ! (nu_{1,3})_{3,2} (\nabla u)_{2,3} : k = 3, i = 2 & + 0.0_rk & ! (nu_{1,1})_{3,3} (\nabla u)_{3,1} : k = 1, i = 3 & + (mu_eff/state(1))*state_gradient(3,1) & ! (nu_{1,2})_{3,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,3})_{3,3} (\nabla u)_{3,3} : k = 3, i = 3 & + 0.0_rk & ! (nu_{1,1})_{3,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{3,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{3,4} (\nabla u)_{4,3} : k = 3, i = 4 & + 0.0_rk & ! (nu_{1,1})_{3,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{3,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{3,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{3,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{3,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{3,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{3,7} (\nabla u)_{7,1} : k = 1, i = 7 & + 0.0_rk & ! (nu_{1,2})_{3,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{3,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk ! Viscous flux for momentum in z physFlux(4) = & ! (nu_{1,1})_{4,1} (\nabla u)_{1,1} : k = 1, i = 1 & (-mu_eff / state(1))*velocity(3)*state_gradient(1,1) & ! (nu_{1,2})_{4,1} (\nabla u)_{1,2} : k = 2, i = 1 & + 0.0_rk & ! (nu_{1,3})_{4,1} (\nabla u)_{1,3} : k = 3, i = 1 & + (-mu_eff / state(1))*velocity(1)*state_gradient(1,3) & ! (nu_{1,1})_{4,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{4,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,3})_{4,2} (\nabla u)_{2,3} : k = 3, i = 2 & + (mu_eff/state(1))*state_gradient(2,3) & ! (nu_{1,1})_{4,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{4,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,3})_{4,3} (\nabla u)_{3,3} : k = 3, i = 3 & + 0.0_rk & ! (nu_{1,1})_{4,4} (\nabla u)_{4,1} : k = 1, i = 4 & + (mu_eff/state(1))*state_gradient(4,1) & ! (nu_{1,2})_{4,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{4,4} (\nabla u)_{4,3} : k = 3, i = 4 & + 0.0_rk & ! (nu_{1,1})_{4,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{4,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{4,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{4,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{4,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{4,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{4,7} (\nabla u)_{7,1} : k = 1, i = 7 & + 0.0_rk & ! (nu_{1,2})_{4,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{4,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk ! Viscous flux for Energy physFlux(5) = & ! (nu_{1,1})_{5,1} (\nabla u)_{1,1} : k = 1, i = 1 & ( ((-2.0_rk * mu_eff + lam_eff) / state(1))*(velocity(1)**2.0_rk) & & +(-mu_eff/state(1))*(velocity(2)**2.0_rk) & & +(-mu_eff/state(1))*(velocity(3)**2.0_rk) & & -energy_coeff*(state(5)/state(1)-sum(velocity(:)**2.0_rk) - state(6)/state(1))) & & * state_gradient(1,1) & ! (nu_{1,2})_{5,1} (\nabla u)_{1,2} : k = 2, i = 1 & + ((-mu_eff+lam_eff)/state(1))*velocity(1)*velocity(2)*state_gradient(1,2) & ! (nu_{1,3})_{5,1} (\nabla u)_{1,3} : k = 3, i = 1 & + ((-mu_eff+lam_eff)/state(1))*velocity(1)*velocity(3)*state_gradient(1,3) & ! (nu_{1,1})_{5,2} (\nabla u)_{2,1} : k = 1, i = 2 & + ((2.0_rk*mu_eff-lam_eff)/state(1) - energy_coeff)*velocity(1) & & * state_gradient(2,1) & ! (nu_{1,2})_{5,2} (\nabla u)_{2,2} : k = 2, i = 2 & + (mu_eff/state(1))*velocity(2)*state_gradient(2,2) & ! (nu_{1,3})_{5,2} (\nabla u)_{2,3} : k = 3, i = 2 & + (mu_eff/state(1))*velocity(3)*state_gradient(2,3) & ! (nu_{1,1})_{5,3} (\nabla u)_{3,1} : k = 1, i = 3 & + ((mu_eff/state(1))- energy_coeff)*velocity(2)*state_gradient(3,1) & ! (nu_{1,2})_{5,3} (\nabla u)_{3,2} : k = 2, i = 3 & + (-lam_eff/state(1))*velocity(1)*state_gradient(3,2) & ! (nu_{1,3})_{5,3} (\nabla u)_{3,3} : k = 3, i = 3 & + 0.0_rk & ! (nu_{1,1})_{5,4} (\nabla u)_{4,1} : k = 1, i = 4 & + ((mu_eff/state(1))- energy_coeff)*velocity(3)*state_gradient(4,1) & ! (nu_{1,2})_{5,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{5,4} (\nabla u)_{4,3} : k = 3, i = 4 & + (-lam_eff/state(1))*velocity(1)*state_gradient(4,3) & ! (nu_{1,1})_{5,5} (\nabla u)_{5,1} : k = 1, i = 5 & + energy_coeff*state_gradient(5,1) & ! (nu_{1,2})_{5,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{5,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{5,6} (\nabla u)_{6,1} : k = 1, i = 6 & + ((mu + sig_k*mu_turb)/state(1) - energy_coeff)*state_gradient(6,1) & ! (nu_{1,2})_{5,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{5,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{5,7} (\nabla u)_{7,1} : k = 1, i = 7 & + 0.0_rk & ! (nu_{1,2})_{5,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{5,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk ! Viscous flux for turbulent KE physFlux(6) = & ! (nu_{1,1})_{6,1} (\nabla u)_{1,1} : k = 1, i = 1 & ( -(mu + sig_k*mu_turb)/state(1))*(state(6)/state(1)) & & *state_gradient(1,1) & ! (nu_{1,2})_{6,1} (\nabla u)_{1,2} : k = 2, i = 1 & + 0.0_rk & ! (nu_{1,3})_{6,1} (\nabla u)_{1,3} : k = 3, i = 1 & + 0.0_rk & ! (nu_{1,1})_{6,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{6,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,3})_{6,2} (\nabla u)_{2,3} : k = 3, i = 2 & + (mu_eff/state(1))*state_gradient(2,3) & ! (nu_{1,1})_{6,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{6,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,3})_{6,3} (\nabla u)_{3,3} : k = 3, i = 3 & + 0.0_rk & ! (nu_{1,1})_{6,4} (\nabla u)_{4,1} : k = 1, i = 4 & + (mu_eff/state(1))*state_gradient(4,1) & ! (nu_{1,2})_{6,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{6,4} (\nabla u)_{4,3} : k = 3, i = 4 & + 0.0_rk & ! (nu_{1,1})_{6,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{6,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{6,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{6,6} (\nabla u)_{6,1} : k = 1, i = 6 & + (mu + sig_k*mu_turb)/state(1)*state_gradient(6,1) & ! (nu_{1,2})_{6,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{6,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{6,7} (\nabla u)_{7,1} : k = 1, i = 7 & + 0.0_rk & ! (nu_{1,2})_{6,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{6,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk ! Viscous flux for specific Dissipation rate (\Omega) physFlux(7) = & ! (nu_{1,1})_{7,1} (\nabla u)_{1,1} : k = 1, i = 1 & ( -(mu + sig_k*mu_turb)/state(1))*(state(7)/state(1)) & & *state_gradient(1,1) & ! (nu_{1,2})_{7,1} (\nabla u)_{1,2} : k = 2, i = 1 & + 0.0_rk & ! (nu_{1,3})_{7,1} (\nabla u)_{1,3} : k = 3, i = 1 & + 0.0_rk & ! (nu_{1,1})_{7,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{7,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,3})_{7,2} (\nabla u)_{2,3} : k = 3, i = 2 & + (mu_eff/state(1))*state_gradient(2,3) & ! (nu_{1,1})_{7,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{7,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,3})_{7,3} (\nabla u)_{3,3} : k = 3, i = 3 & + 0.0_rk & ! (nu_{1,1})_{7,4} (\nabla u)_{4,1} : k = 1, i = 4 & + (mu_eff/state(1))*state_gradient(4,1) & ! (nu_{1,2})_{7,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,3})_{7,4} (\nabla u)_{4,3} : k = 3, i = 4 & + 0.0_rk & ! (nu_{1,1})_{7,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{7,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,3})_{7,5} (\nabla u)_{5,3} : k = 3, i = 5 & + 0.0_rk & ! (nu_{1,1})_{7,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{7,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk & ! (nu_{1,3})_{7,6} (\nabla u)_{6,3} : k = 3, i = 6 & + 0.0_rk & ! (nu_{1,1})_{7,7} (\nabla u)_{7,1} : k = 1, i = 7 & + ((mu + sig_omg*mu_turb)/state(1))*state_gradient(7,1) & ! (nu_{1,2})_{7,7} (\nabla u)_{7,2} : k = 2, i = 7 & + 0.0_rk & ! (nu_{1,3})_{7,7} (\nabla u)_{7,3} : k = 3, i = 7 & + 0.0_rk end function atl_viscPhysFluxRans function atl_viscPhysFluxRans_2d(state, state_gradient, isenCoeff, mu, & & lambda, thermCond, rans_params, heatCap ) result(physFlux) ! ------------------------------------------------------------------------------------ !> The state in nodal space. Dimension is the number of vars, i.e. 4 for Navier-Stokes. real(kind=rk), intent(in) :: state(:) !> The state in nodal space. First dimension is the number of vars, i.e. 4 for Navier-Stokes. !! Second dimension is the dimension, e.g. 2 in two dimensions. real(kind=rk), intent(in) :: state_gradient(:,:) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The thermal cond real(kind=rk), intent(in) :: thermCond !> The specific heat capacity (per mass unit mass, at constant volume) real(kind=rk), intent(in) :: heatCap !> The physical flux along the x axis for all variables real(kind=rk) :: physFlux(6) !> The constants for the Rans eqn type(atl_Navier_stokes_rans_type), intent(in) :: rans_params ! ----------------------------------------------------------------------------- real(kind=rk) :: velocity(1:2) ! The turbulent viscosity (dynamic) real(kind=rk) :: mu_turb ! The turbulent viscosity real(kind=rk) :: lam_turb ! The effective viscosity (dynamic) real(kind=rk) :: mu_eff ! The effective turbulent viscosity real(kind=rk) :: lam_eff real(kind=rk) :: energy_coeff real(kind=rk) :: k_eff real(kind=rk) :: turbPrNum, limited_eddy_visc, turb_coeff1, turb_coeff2 real(kind=rk) :: velGrad(2,2), ViscStressTensor(2,2), omega_r ! ----------------------------------------------------------------------------- mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) lam_turb = 2.0*mu_turb/3.0 mu_eff = mu + mu_turb lam_eff = lambda + lam_turb turbPrNum = rans_params%turb_prandtl_num k_eff = max(state(6),0.0_rk) energy_coeff = thermCond/(heatCap*state(1)) & & + mu_turb*isenCoeff/(turbPrNum*state(1) ) velocity(1:2) = state(2:3)/state(1) ! Now to calculate the coefficient \omega_r: We need to do the following ! Step-1: Get the velocity gradient from the state gradient present call atl_get_pointwise_velocity_gradient_2D ( state_gradient, & & state, velGrad ) ! Step-2: Calculate the viscous stress tensor call atl_get_pointwise_visc_stress_tensor_2D( & & velGrad = velGrad, & & S = ViscStressTensor ) ! Step-3: Get the value of \omega_r call atl_get_lower_bound_turb_disscipation( & & S = ViscStressTensor, & & c_mu = rans_params%c_mu, & & omega = state(6)/ state(1), & & omega_r = omega_r ) limited_eddy_visc = rans_params%alpha*k_eff*exp(-omega_r) turb_coeff1 = (mu + rans_params%sig_k*limited_eddy_visc)/ state(1) turb_coeff2 = (mu + rans_params%sig_omg*limited_eddy_visc)/ state(1) ! Viscous flux for density physFlux(1) = 0.0_rk ! Viscous flux for momentum in x physFlux(2) = & ! (nu_{1,1})_{2,1} (\nabla u)_{1,1} : k = 1, i = 1 & ((-2.0_rk * mu_eff + lam_eff) / state(1))*velocity(1)*state_gradient(1,1) & ! (nu_{1,2})_{2,1} (\nabla u)_{1,2} : k = 2, i = 1 & + (lam_eff / state(1))*velocity(2)*state_gradient(1,2) & ! (nu_{1,1})_{2,2} (\nabla u)_{2,1} : k = 1, i = 2 & + ((2.0_rk * mu_eff - lam_eff) / state(1))*state_gradient(2,1) & ! (nu_{1,2})_{2,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,1})_{2,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{2,3} (\nabla u)_{3,2} : k = 2, i = 3 & + (-lam_eff/state(1))*state_gradient(3,2) & ! (nu_{1,1})_{2,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{2,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk ! Viscous flux for momentum in y physFlux(3) = & ! (nu_{1,1})_{3,1} (\nabla u)_{1,1} : k = 1, i = 1 & (-mu_eff / state(1))*velocity(2)*state_gradient(1,1) & ! (nu_{1,2})_{3,1} (\nabla u)_{1,2} : k = 2, i = 1 & + (-mu_eff / state(1))*velocity(1)*state_gradient(1,2) & ! (nu_{1,1})_{3,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{3,2} (\nabla u)_{2,2} : k = 2, i = 2 & + (mu_eff/state(1))*state_gradient(2,2) & ! (nu_{1,1})_{3,3} (\nabla u)_{3,1} : k = 1, i = 3 & + (mu_eff/state(1))*state_gradient(3,1) & ! (nu_{1,2})_{3,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,1})_{3,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{3,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk ! Viscous flux for Energy physFlux(4) = & ! (nu_{1,1})_{4,1} (\nabla u)_{1,1} : k = 1, i = 1 & ( ((-2.0_rk * mu_eff + lam_eff) / state(1))*(velocity(1)**2.0_rk) & & + (-mu_eff/state(1))*(velocity(2)**2.0_rk) & & -energy_coeff*(state(4)/state(1)-sum(velocity(:)**2.0_rk) - state(5)/state(1)) & & - turb_coeff1*(state(5)/state(1)) ) & & * state_gradient(1,1) & ! (nu_{1,2})_{4,1} (\nabla u)_{1,2} : k = 2, i = 1 & + ((-mu_eff+lam_eff)/state(1))*velocity(1)*velocity(2)*state_gradient(1,2) & ! (nu_{1,1})_{4,2} (\nabla u)_{2,1} : k = 1, i = 2 & + ((2.0_rk*mu_eff-lam_eff)/state(1) - energy_coeff)*velocity(1) & & * state_gradient(2,1) & ! (nu_{1,2})_{4,2} (\nabla u)_{2,2} : k = 2, i = 2 & + (mu_eff/state(1))*velocity(2)*state_gradient(2,2) & ! (nu_{1,1})_{4,3} (\nabla u)_{3,1} : k = 1, i = 3 & + ((mu_eff/state(1)) - energy_coeff)*velocity(2)*state_gradient(3,1) & ! (nu_{1,2})_{4,3} (\nabla u)_{3,2} : k = 2, i = 3 & + (-lam_eff/state(1))*velocity(1)*state_gradient(3,2) & ! (nu_{1,1})_{4,4} (\nabla u)_{4,1} : k = 1, i = 4 & + energy_coeff*state_gradient(4,1) & ! (nu_{1,2})_{4,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,1})_{4,5} (\nabla u)_{5,1} : k = 1, i = 5 & + (-energy_coeff + turb_coeff1)*state_gradient(5,1) & ! (nu_{1,2})_{4,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,1})_{4,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{4,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk physFlux(5) = & ! (nu_{1,1})_{5,1} (\nabla u)_{1,1} : k = 1, i = 1 & -turb_coeff1*(state(5)/state(1)) *state_gradient(1,1) & ! (nu_{1,2})_{5,1} (\nabla u)_{1,2} : k = 2, i = 1 & + 0.0_rk & ! (nu_{1,1})_{5,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{5,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,1})_{5,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{5,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,1})_{5,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{5,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,1})_{5,5} (\nabla u)_{5,1} : k = 1, i = 5 & + turb_coeff1*state_gradient(5,1) & ! (nu_{1,2})_{5,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,1})_{5,6} (\nabla u)_{6,1} : k = 1, i = 6 & + 0.0_rk & ! (nu_{1,2})_{5,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk physFlux(6) = & ! (nu_{1,1})_{6,1} (\nabla u)_{1,1} : k = 1, i = 1 & ( -turb_coeff2*state(6)/state(1) )*state_gradient(1,1) & ! (nu_{1,2})_{6,1} (\nabla u)_{1,2} : k = 2, i = 1 & + 0.0_rk & ! (nu_{1,1})_{6,2} (\nabla u)_{2,1} : k = 1, i = 2 & + 0.0_rk & ! (nu_{1,2})_{6,2} (\nabla u)_{2,2} : k = 2, i = 2 & + 0.0_rk & ! (nu_{1,1})_{6,3} (\nabla u)_{3,1} : k = 1, i = 3 & + 0.0_rk & ! (nu_{1,2})_{6,3} (\nabla u)_{3,2} : k = 2, i = 3 & + 0.0_rk & ! (nu_{1,1})_{6,4} (\nabla u)_{4,1} : k = 1, i = 4 & + 0.0_rk & ! (nu_{1,2})_{6,4} (\nabla u)_{4,2} : k = 2, i = 4 & + 0.0_rk & ! (nu_{1,1})_{6,5} (\nabla u)_{5,1} : k = 1, i = 5 & + 0.0_rk & ! (nu_{1,2})_{6,5} (\nabla u)_{5,2} : k = 2, i = 5 & + 0.0_rk & ! (nu_{1,1})_{6,6} (\nabla u)_{6,1} : k = 1, i = 6 & + turb_coeff2*state_gradient(6,1) & ! (nu_{1,2})_{6,6} (\nabla u)_{6,2} : k = 2, i = 6 & + 0.0_rk end function atl_viscPhysFluxRans_2d ! Multiplies the viscous flux matrux nu_11 with a given vector function atl_mult_nu11_Rans_2d( state, velocity, inVec, & & isenCoeff, mu, lambda, thermCond, rans_params, heatCap) & & result( outVec ) ! -------------------------------------------------------------------------! !> The velocity real(kind=rk), intent(in) :: velocity(2) !> The state array real(kind=rk), intent(in) :: state(6) !> Vector to be multiplied with nu11 real(kind=rk), intent(in) :: inVec(6) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The thermal cond real(kind=rk), intent(in) :: thermCond !> The specific heat capacity (per mass unit mass, at constant volume) real(kind=rk), intent(in) :: heatCap !> The constants for the Rans eqn type(atl_Navier_stokes_rans_type), intent(in) :: rans_params !> The result of the matrix vector product real(kind=rk) :: outVec(6) ! -------------------------------------------------------------------------! !> mu_turb real(kind=rk) :: mu_turb, mu_eff, lam_eff, limited_eddy_visc, energy_coeff real(kind=rk) :: turb_coeff1, turb_coeff2 ! -------------------------------------------------------------------------! mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) mu_eff = mu + mu_turb lam_eff = lambda + 2.0*mu_turb/3.0 ! Stuff neeeded energy_coeff = thermCond/(heatCap*state(1)) & & + mu_turb*isenCoeff/(rans_params%turb_prandtl_num*state(1)) !NA! ! Now to calculate the coefficient \omega_r: We need to do the following !NA! ! Step-1: Get the velocity gradient from the state gradient present !NA! call atl_get_pointwise_velocity_gradient_2D ( inVec, & !NA! & state, velGrad ) !NA! !NA! ! Step-2: Calculate the viscous stress tensor !NA! call atl_get_pointwise_visc_stress_tensor_2D( & !NA! & velGrad = velGrad, & !NA! & S = ViscStressTensor ) !NA! !NA! ! Step-3: Get the value of \omega_r !NA! call atl_get_lower_bound_turb_disscipation( & !NA! & S = ViscStressTensor, & !NA! & c_mu = rans_params%c_mu, & !NA! & omega = state(6)/ state(1), & !NA! & omega_r = omega_r ) ! @todo : NA : Calculate limited_eddy_visc Appropriately !NA! limited_eddy_visc = rans_params%alpha*max(state(5),0.0)*exp(-omega_r) limited_eddy_visc = rans_params%alpha*max(state(5),0.0_rk) & & *exp(state(6)/state(1)) turb_coeff1 = (mu + rans_params%sig_k*limited_eddy_visc)/ state(1) turb_coeff2 = (mu + rans_params%sig_omg*limited_eddy_visc)/ state(1) ! First row has zeros only outVec(1) = 0.0_rk ! Second row outVec(2) = ((-2.0_rk*mu_eff + lam_eff)/state(1))*velocity(1) * inVec(1) & & + ((2.0_rk*mu_eff - lam_eff)/state(1)) * inVec(2) ! Third row outVec(3) = (-mu_eff/state(1)) * velocity(2) * inVec(1) & & + (mu_eff/state(1)) * inVec(3) ! Fourth row outVec(4) = ( & & ((-2.0_rk*mu_eff + lam_eff)/state(1))*velocity(1)*velocity(1) & & + (-mu_eff/state(1)) * velocity(2)*velocity(2) & & - energy_coeff*(state(4)/state(1) - sum(velocity(:)**2) & & - state(5)/state(1) ) & & - turb_coeff1*(state(5)/state(1)) )* inVec(1) & & + ( & & ((2.0_rk*mu_eff-lam_eff)/state(1) - energy_coeff)*velocity(1) & & ) * inVec(2) & & + ( (mu_eff/state(1) - energy_coeff)*velocity(2))* inVec(3) & & + ( energy_coeff ) * inVec(4) & & + ( -energy_coeff + turb_coeff1 )* inVec(5) ! Fifth Row outVec(5) = ( & & -turb_coeff1*(state(5)/state(1)) )* inVec(1) & & + turb_coeff1*inVec(5) ! Sixth Row outVec(6) = ( -turb_coeff2*state(6)/state(1) )* inVec(1) & & + ( turb_coeff2 )* inVec(6) end function atl_mult_nu11_Rans_2d ! Multiplies the viscous flux matrux nu_21 with a given vector function atl_mult_nu21_Rans_2d( state, velocity, inVec, mu, lambda, & & rans_params) & & result( outVec ) ! -------------------------------------------------------------------------! !> The velocity real(kind=rk), intent(in) :: velocity(2) !> The state array real(kind=rk), intent(in) :: state(6) !> Vector to be multiplied with nu11 real(kind=rk), intent(in) :: inVec(6) !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The constants for the Rans eqn type(atl_Navier_stokes_rans_type), intent(in) :: rans_params !> The result of the matrix vector product real(kind=rk) :: outVec(6) ! -------------------------------------------------------------------------! !> mu_turb real(kind=rk) :: mu_turb, mu_eff, lam_eff ! -------------------------------------------------------------------------! mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) mu_eff = mu + mu_turb lam_eff = lambda + 2.0*mu_turb/3.0 ! First row has zeros only outVec(1) = 0.0_rk ! Second row outVec(2) = (-mu_eff/state(1)) * velocity(2) * inVec(1) & & + (mu_eff/state(1)) * inVec(3) ! Third row outVec(3) = (lam_eff/state(1)) * velocity(1) * inVec(1) & & + (-lam_eff/state(1)) * inVec(2) ! Fourth row outVec(4) = ( & & ((-mu_eff+lam_eff)/state(1))*velocity(1)*velocity(2) & & ) * inVec(1) & & + ( & & (-lam_eff/state(1))*velocity(2) & & ) * inVec(2) & & + ( & & (mu_eff/state(1))*velocity(1) & & ) * inVec(3) outVec(5) = 0.0_rk outVec(6) = 0.0_rk end function atl_mult_nu21_Rans_2d ! Multiplies the viscous flux matrux nu_12 with a given vector function atl_mult_nu12_Rans_2d( state, velocity, inVec, mu, lambda, & & rans_params ) & & result( outVec ) ! -------------------------------------------------------------------------! !> The velocity real(kind=rk), intent(in) :: velocity(2) !> The state array real(kind=rk), intent(in) :: state(6) !> Vector to be multiplied with nu11 real(kind=rk), intent(in) :: inVec(6) !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The constants for the Rans eqn type(atl_Navier_stokes_rans_type), intent(in) :: rans_params !> The result of the matrix vector product real(kind=rk) :: outVec(6) ! -------------------------------------------------------------------------! !> mu_turb real(kind=rk) :: mu_turb, mu_eff, lam_eff ! -------------------------------------------------------------------------! mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) mu_eff = mu + mu_turb lam_eff = lambda + 2.0*mu_turb/3.0 ! First row has zeros only outVec(1) = 0.0_rk ! Second row outVec(2) = (lam_eff/state(1)) * velocity(2) * inVec(1) & & + (-lam_eff/state(1)) * inVec(3) ! Third row outVec(3) = (-mu_eff/state(1)) * velocity(1) * inVec(1) & & + (mu_eff/state(1)) * inVec(2) ! Fourth row outVec(4) = ( & & ((-mu_eff+lam_eff)/state(1))*velocity(1)*velocity(2) & & ) * inVec(1) & & + ( & & (mu_eff/state(1))*velocity(2) & & ) * inVec(2) & & + ( & & (-lam_eff/state(1))*velocity(1) & & ) * inVec(3) outVec(5) = 0.0_rk outVec(6) = 0.0_rk end function atl_mult_nu12_Rans_2d ! Multiplies the viscous flux matrux nu_22 with a given vector function atl_mult_nu22_Rans_2d( state, velocity, inVec, & & isenCoeff, mu, lambda, thermCond, rans_params, heatCap) & & result( outVec ) ! -------------------------------------------------------------------------! !> The velocity real(kind=rk), intent(in) :: velocity(2) !> The state array real(kind=rk), intent(in) :: state(6) !> Vector to be multiplied with nu11 real(kind=rk), intent(in) :: inVec(6) !> Adiabatice index, also known as isentropic expansion factor. real(kind=rk), intent(in) :: isenCoeff !> Dynamic Viscosity real(kind=rk), intent(in) :: mu !> Viscosity real(kind=rk), intent(in) :: lambda !> The thermal cond real(kind=rk), intent(in) :: thermCond !> The specific heat capacity (per mass unit mass, at constant volume) real(kind=rk), intent(in) :: heatCap !> The constants for the Rans eqn type(atl_Navier_stokes_rans_type), intent(in) :: rans_params !> The result of the matrix vector product real(kind=rk) :: outVec(6) ! -------------------------------------------------------------------------! !> mu_turb real(kind=rk) :: mu_turb, mu_eff, lam_eff, limited_eddy_visc, energy_coeff real(kind=rk) :: turb_coeff1, turb_coeff2 ! -------------------------------------------------------------------------! mu_turb = rans_params%c_mu*state(5)/exp(state(6)/state(1)) mu_eff = mu + mu_turb lam_eff = lambda + 2.0*mu_turb/3.0 ! Stuff neeeded energy_coeff = thermCond/(heatCap*state(1)) & & + mu_turb*isenCoeff/(rans_params%turb_prandtl_num*state(1) ) ! @todo : NA : Calculate limited_eddy_visc Appropriately limited_eddy_visc = rans_params%alpha*max(state(5),0.0_rk) & & *exp(state(6)/state(1)) turb_coeff1 = (mu + rans_params%sig_k*limited_eddy_visc)/ state(1) turb_coeff2 = (mu + rans_params%sig_omg*limited_eddy_visc)/ state(1) ! First row has zeros only outVec(1) = 0.0_rk ! Second row outVec(2) = (-mu_eff/state(1)) * velocity(1) * inVec(1) & & + (mu_eff/state(1)) * inVec(2) ! Third row outVec(3) = ((-2.0_rk*mu_eff + lam_eff)/state(1))*velocity(2) * inVec(1) & & + ((2.0_rk*mu_eff - lam_eff)/state(1)) * inVec(3) ! Fourth row outVec(4) = ( & & (-mu_eff/state(1)) * velocity(1)*velocity(1) & & + ((-2.0_rk*mu_eff + lam_eff)/state(1))*velocity(2)*velocity(2) & & - energy_coeff*(state(4)/state(1) - sum(velocity(:)**2) & & -state(5)/state(1) ) & & - turb_coeff1*state(5)/state(1) ) * inVec(1) & & + ( & & (mu_eff/state(1) - energy_coeff)*velocity(1) & & ) * inVec(2) & & + ( & & ((2.0_rk*mu_eff-lam_eff)/state(1) - energy_coeff )*velocity(2) & & ) * inVec(3) & & + ( & & energy_coeff & & ) * inVec(4) & & + (-energy_coeff + turb_coeff1 )* invec(5) ! Fifth row outVec(5) = ( -turb_coeff1*(state(5)/state(1)) )* inVec(1) & & + ( turb_coeff1 )* inVec(5) ! Sixt Row outVec(6) = ( -turb_coeff2*state(6)/state(1) ) * inVec(1) & & + ( turb_coeff2 )* inVec(6) end function atl_mult_nu22_Rans_2d end module atl_physFluxFilNvrStk_module