! Copyright (c) 2013-2014 Jiaxing Qi <jiaxing.qi@uni-siegen.de> ! Copyright (c) 2013 Simon Zimny <s.zimny@grs-sim.de> ! Copyright (c) 2013, 2016, 2020 Kannan Masilamani <kannan.masilamani@uni-siegen.de> ! Copyright (c) 2014 Kartik Jain <kartik.jain@uni-siegen.de> ! Copyright (c) 2016 Tobias Schneider <tobias1.schneider@student.uni-siegen.de> ! Copyright (c) 2020 Peter Vitt <peter.vitt2@uni-siegen.de> ! Copyright (c) 2020 Harald Klimach <harald.klimach@uni-siegen.de> ! ! Redistribution and use in source and binary forms, with or without ! modification, are permitted provided that the following conditions are met: ! ! 1. Redistributions of source code must retain the above copyright notice, ! this list of conditions and the following disclaimer. ! ! 2. Redistributions in binary form must reproduce the above copyright notice, ! this list of conditions and the following disclaimer in the documentation ! and/or other materials provided with the distribution. ! ! THIS SOFTWARE IS PROVIDED BY THE UNIVERSITY OF SIEGEN “AS IS” AND ANY EXPRESS ! OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES ! OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. ! IN NO EVENT SHALL UNIVERSITY OF SIEGEN OR CONTRIBUTORS BE LIABLE FOR ANY ! DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES ! (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; ! LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ! ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT ! (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS ! SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. ! **************************************************************************** ! !> author: Jiaxing Qi, Kannan Masilamani !! This module keeps all information about the nonNewtonian models. !! Contains routines which calculates non-Newtonian kinematic !! viscosity according to non-Newtonian model. !! !! It supports three non-Newtonian models: !! Power law, Carrear Yasuda and Casson. !! All these models are described in !! Ashrafizaadeh, M., & Bakhshaei, H. (2009). A comparison of non-Newtonian !! models for lattice Boltzmann blood flow simulations. !! Computers and Mathematics with Applications, 58(5), 1045–1054. !! !! For further information about the theory visit the !! [non-newtonian theory page](../page/mus_nonNewtonianTheory.html). !! ! Copyright (c) 2011-2013 Manuel Hasert <m.hasert@grs-sim.de> ! Copyright (c) 2011 Harald Klimach <harald.klimach@uni-siegen.de> ! Copyright (c) 2011 Konstantin Kleinheinz <k.kleinheinz@grs-sim.de> ! Copyright (c) 2011-2012 Simon Zimny <s.zimny@grs-sim.de> ! Copyright (c) 2012, 2014-2016 Jiaxing Qi <jiaxing.qi@uni-siegen.de> ! Copyright (c) 2012 Kartik Jain <kartik.jain@uni-siegen.de> ! Copyright (c) 2013-2015, 2019 Kannan Masilamani <kannan.masilamani@uni-siegen.de> ! Copyright (c) 2016 Tobias Schneider <tobias1.schneider@student.uni-siegen.de> ! ! Redistribution and use in source and binary forms, with or without ! modification, are permitted provided that the following conditions are met: ! ! 1. Redistributions of source code must retain the above copyright notice, ! this list of conditions and the following disclaimer. ! ! 2. Redistributions in binary form must reproduce the above copyright notice, ! this list of conditions and the following disclaimer in the documentation ! and/or other materials provided with the distribution. ! ! THIS SOFTWARE IS PROVIDED BY THE UNIVERSITY OF SIEGEN “AS IS” AND ANY EXPRESS ! OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES ! OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. ! IN NO EVENT SHALL UNIVERSITY OF SIEGEN OR CONTRIBUTORS BE LIABLE FOR ANY ! DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES ! (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; ! LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ! ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT ! (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS ! SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. ! Copyright (c) 2014-2015, 2019-2020 Kannan Masilamani <kannan.masilamani@uni-siegen.de> ! Copyright (c) 2015-2016 Jiaxing Qi <jiaxing.qi@uni-siegen.de> ! Copyright (c) 2016 Tobias Schneider <tobias1.schneider@student.uni-siegen.de> ! Copyright (c) 2020 Peter Vitt <peter.vitt2@uni-siegen.de> ! ! Redistribution and use in source and binary forms, with or without ! modification, are permitted provided that the following conditions are met: ! ! 1. Redistributions of source code must retain the above copyright notice, ! this list of conditions and the following disclaimer. ! ! 2. Redistributions in binary form must reproduce the above copyright notice, ! this list of conditions and the following disclaimer in the documentation ! and/or other materials provided with the distribution. ! ! THIS SOFTWARE IS PROVIDED BY THE UNIVERSITY OF SIEGEN “AS IS” AND ANY EXPRESS ! OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES ! OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. ! IN NO EVENT SHALL UNIVERSITY OF SIEGEN OR CONTRIBUTORS BE LIABLE FOR ANY ! DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES ! (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; ! LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ! ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT ! (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS ! SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. module mus_nonNewtonian_module ! include treelm modules use env_module, only: rk, labellen use tem_tools_module, only: tem_horizontalSpacer, upper_to_lower use tem_logging_module, only: logUnit use tem_aux_module, only: tem_abort use tem_param_module, only: rho0, rho0Inv, cs2, cs2inv, div1_2 ! include aotus modules use aotus_module, only: flu_State, aot_get_val use aot_table_module, only: aot_table_open, aot_table_close use aot_out_module, only: aot_out_type, aot_out_val, aot_out_open_table, & & aot_out_close_table ! include musubi modules use mus_physics_module, only: mus_convertFac_type use mus_scheme_layout_module, only: mus_scheme_layout_type use mus_scheme_header_module, only: mus_scheme_header_type implicit none private public :: mus_nNwtn_type public :: mus_nNwtn_load public :: mus_nNwtn_save2lua public :: mus_nNwtn_dump2outUnit public :: mus_assign_nNwtnVisc_ptr public :: calcVisc_CY !> Identifier for Power-Law model integer, parameter, public :: powerLaw = 1 !> Identifier for Casson model integer, parameter, public :: casson = 2 !> Identifier for Carreau-Yasuda model integer, parameter, public :: carreauYasuda = 3 ! --------------------------------------------------------------------------- !> The nonNewtonian power law model parameter !! !! This date type gathers parameters of a power law (PL) model. !! It is encapsulated in mus_nNwtn_type. type mus_nNwtn_PL_type !> exponentiation parameter real(kind=rk) :: n = 0.5_rk !> Unit consistency index. !! Dynamic viscosity parameter when shear rate equals to 1. !! i.e. backgroud viscosity for power-law model real(kind=rk) :: visc0 = 0.0035_rk !> parameter for computation real(kind=rk) :: nMinus1 end type mus_nNwtn_PL_type ! ---------------------------------------------------------------------------- ! ---------------------------------------------------------------------------- !> The nonNewtonian power law model parameter !! !! This date type gathers parameters of the Carreau-Yasuda (CY) model !! It is encapsulated in mus_nNwtn_type. type mus_nNwtn_CY_type !> model parameter real(kind=rk) :: n = 0.2128_rk !> model parameter real(kind=rk) :: a = 0.64_rk !> model parameter real(kind=rk) :: lambda = 8.2_rk !> model parameter, dynamic viscosity at zero shear-rate real(kind=rk) :: visc0 = 0.16_rk !> model parameter, dynamic viscosity in infinity shear-rate real(kind=rk) :: viscInf = 0.0035_rk !> calculated parameter for later usage, nMinus1Div_a = (n-1)/a real(kind=rk) :: nMinus1Div_a = (0.2128_rk - 1._rk) / 0.64_rk end type mus_nNwtn_CY_type ! ---------------------------------------------------------------------------- ! ---------------------------------------------------------------------------- !> The nonNewtonian power law model parameter !! !! This date type gathers parameters of the Casson model !! It is encapsulated in mus_nNwtn_type. type mus_nNwtn_CS_type !> model parameter real(kind=rk) :: k0 = 0.1937_rk !> model parameter real(kind=rk) :: k1 = 0.055_rk end type mus_nNwtn_CS_type ! ---------------------------------------------------------------------------- ! ---------------------------------------------------------------------------- !> The nonNewtonian fluid feature description type !! !! This date type gathers related parameters of a nonNewtonian fluid. type mus_nNwtn_type !> Indicator whether nonNewtonian feature is active !! maybe not useful. schemeHeader%kind can used to check if nNwtn is active logical :: active = .false. !> nonNewtonian fluid model label character(len=labellen) :: label !> nonNewtonian fluid model identifier integer :: model !> Power Law (PL) model type type( mus_nNwtn_PL_type ) :: PL !> Carreau-Yasuda (CY) model type type( mus_nNwtn_CY_type ) :: CY !> Casson model type type( mus_nNwtn_CS_type ) :: CS !> this procedure compute kinematic viscosity in lattice unit on current !! level from preCollision PDF based on non-Newtonian model. !! It uses shear-rate to compute viscosity. !! Non-newtonian model is given in dynamic viscosity in physical unit !! so it is dimensionalized using viscDyna in physics%fac and !! lattice kinematic viscosity = lattice dynamic viscosity !! / rho (local density) for compressible model and !! lattice kinematic viscosity = lattice dynamic viscosity / rho0 !! for incompressible model. procedure(proc_calc_nNwtn_visc_fromPreColPDF), pointer :: calcVisc => null() end type mus_nNwtn_type ! ---------------------------------------------------------------------------- !> Interface to calculate kinematic viscosity for non-Newtonian model. !! Viscosity is computed from shear rate which is computed from strain rate !! which is computed from nonEquilibrium PDF which in turn is computed from !! pre-collision PDF abstract interface subroutine proc_calc_nNwtn_visc_fromPreColPDF(nNwtn, viscKine, omega, & & state, neigh, auxField, densPos, velPos, nSize, nSolve, nScalars, & & nAuxScalars, layout, convFac) import :: rk, mus_nNwtn_type, mus_scheme_layout_type, mus_convertFac_type !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: kinematic viscosity from non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac end subroutine proc_calc_nNwtn_visc_fromPreColPDF end interface contains ! ************************************************************************** ! !> Read in the nonNewtonian table from Lua file and dump parameters to logUnit !! Specificly, this routine calls each model parameter loader. !! subroutine mus_nNwtn_load( me, conf, parent ) ! -------------------------------------------------------------------------- !> nonNewtonian type type( mus_nNwtn_type ), intent(out) :: me !> lua state type( flu_state ), intent(inout) :: conf !> parent handle integer, intent(in), optional :: parent ! -------------------------------------------------------------------------- integer :: nonNwt_table integer :: iError CHARACTER(LEN=12) :: nonNwt_table_str ! -------------------------------------------------------------------------- nonNwt_table_str = "nonNewtonian" ! if nonNewtonian informations in scheme table parentHandle /= 0 call aot_table_open( L = conf, & & parent = parent, & & thandle = nonNwt_table, & & key = nonNwt_table_str ) if ( nonNwt_table == 0 ) then write(logUnit(1),*)'No nonNewtonian table defined' me%active = .false. return endif ! when table exist, read in parameters from table write(logUnit(1),*) 'Loading nonNewtonian informations' ! Set nonNewtonian feature in on me%active = .true. ! load model label name call aot_get_val(L = conf, & & tHandle = nonNwt_table,& & key = 'model', & & val = me%label, & & default = 'power_law', & & ErrCode = iError ) ! load model parameters by calling model loader ! set model identifier select case( trim(upper_to_lower(me%label)) ) case ( 'power_law' ) me%model = powerLaw call mus_nNwtn_PL_load( me%PL, conf, nonNwt_table ) case ( 'carreau_yasuda') me%model = carreauYasuda call mus_nNwtn_CY_load( me%CY, conf, nonNwt_table ) case ( 'casson' ) me%model = casson call mus_nNwtn_CS_load( me%CS, conf, nonNwt_table ) case default call tem_abort('Error: Unknown non-Newtonian model') end select call aot_table_close( L=conf, thandle = nonNwt_table ) end subroutine mus_nNwtn_load ! ************************************************************************** ! ! ************************************************************************** ! !> Read in the nonNewtonian Power Law (PL) model parameters from Lua file subroutine mus_nNwtn_PL_load( me, conf, tHandle ) ! -------------------------------------------------------------------------- !> nonNewtonian type type( mus_nNwtn_PL_type ), intent(out) :: me !> lua state type( flu_state ), intent(inout) :: conf !> nonNewtonian table handle integer, intent(inout) :: tHandle ! -------------------------------------------------------------------------- integer :: iError ! -------------------------------------------------------------------------- ! load n call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'n', & & val = me%n, & & default = 0.5_rk, & & ErrCode = iError ) ! load k call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'dynamic_viscosity_0', & & val = me%visc0, & & default = 0.0000035_rk, & & ErrCode = iError ) me%nMinus1 = me%n - 1._rk end subroutine mus_nNwtn_PL_load ! ************************************************************************** ! ! ************************************************************************** ! !> Read in the nonNewtonian Carreau-Yasuda (CY) model parameters from Lua file subroutine mus_nNwtn_CY_load( me, conf, tHandle ) ! -------------------------------------------------------------------------- !> nonNewtonian type type( mus_nNwtn_CY_type ), intent(out) :: me !> lua state type( flu_state ), intent(inout) :: conf !> nonNewtonian table handle integer, intent(inout) :: tHandle ! -------------------------------------------------------------------------- integer :: iError ! -------------------------------------------------------------------------- ! load visc0 call aot_get_val(L = conf, & & thandle = tHandle, & & key = 'dynamic_viscosity_0', & & val = me%visc0, & & default = 0.16_rk, & & ErrCode = iError ) ! load viscInf call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'dynamic_viscosity_infty', & & val = me%viscInf, & & default = 0.0035_rk, & & ErrCode = iError ) ! load lambda call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'lambda', & & val = me%lambda, & & default = 8.2_rk, & & ErrCode = iError ) ! load a call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'a', & & val = me%a, & & default = 0.64_rk, & & ErrCode = iError ) ! load n call aot_get_val( L = conf, & & thandle = tHandle, & & key = 'n', & & val = me%n, & & default = 0.2128_rk, & & ErrCode = iError ) ! calculate intermediate parameter me%nMinus1Div_a = ( me%n - 1._rk ) / me%a end subroutine mus_nNwtn_CY_load ! ************************************************************************** ! ! ************************************************************************** ! !> Read in the nonNewtonian Casson model parameters from Lua file subroutine mus_nNwtn_CS_load( me, conf, tHandle ) ! -------------------------------------------------------------------------- !> nonNewtonian type type( mus_nNwtn_CS_type ), intent(out) :: me !> lua state type( flu_state ), intent(inout) :: conf !> nonNewtonian table handle integer, intent(inout) :: tHandle ! -------------------------------------------------------------------------- integer :: iError ! -------------------------------------------------------------------------- ! load k0 call aot_get_val(L = conf, & & tHandle = tHandle, & & key = 'k0', & & val = me%k0, & & default = 0.1937_rk, & & ErrCode = iError ) ! load k1 call aot_get_val( L = conf, & & tHandle = tHandle, & & key = 'k1', & & val = me%k1, & & default = 0.055_rk, & & ErrCode = iError ) end subroutine mus_nNwtn_CS_load ! ************************************************************************** ! ! ************************************************************************** ! !> write nonNewtonian fluid parameters into a lua file !! subroutine mus_nNwtn_save2lua( me, conf ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_type ), intent(in) :: me type( aot_out_type ) :: conf ! -------------------------------------------------------------------------- call aot_out_open_table( put_conf = conf, tname = 'nonNewtonian' ) call aot_out_val( put_conf = conf, & & vname = 'model', & & val = trim(me%label) ) select case( me%model ) case ( powerLaw ) call mus_nNwtn_PL_save( me%PL, conf ) case ( carreauYasuda ) call mus_nNwtn_CY_save( me%CY, conf ) case ( casson ) call mus_nNwtn_CS_save( me%CS, conf ) end select call aot_out_close_table( put_conf = conf ) end subroutine mus_nNwtn_save2lua ! ************************************************************************** ! ! ************************************************************************** ! !> write nonNewtonian Power Law (PL) parameters into a lua file !! subroutine mus_nNwtn_PL_save( me, conf ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_PL_type ), intent(in) :: me type( aot_out_type ) :: conf ! -------------------------------------------------------------------------- call aot_out_val( put_conf = conf, & & vname = 'n', & & val = me%n ) call aot_out_val( put_conf = conf, & & vname = 'dynamic_viscosity_0', & & val = me%visc0 ) end subroutine mus_nNwtn_PL_save ! ************************************************************************** ! ! ************************************************************************** ! !> write nonNewtonian (CY) parameters into a lua file !! subroutine mus_nNwtn_CY_save( me, conf ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_CY_type ), intent(in) :: me type( aot_out_type ) :: conf ! -------------------------------------------------------------------------- call aot_out_val( put_conf = conf, & & vname = 'n', & & val = me%n ) call aot_out_val( put_conf = conf, & & vname = 'a', & & val = me%a ) call aot_out_val( put_conf = conf, & & vname = 'lambda', & & val = me%lambda ) call aot_out_val( put_conf = conf, & & vname = 'dynamic_viscosity_0', & & val = me%visc0 ) call aot_out_val( put_conf = conf, & & vname = 'dynamic_viscosity_infty', & & val = me%viscInf ) end subroutine mus_nNwtn_CY_save ! ************************************************************************** ! ! ************************************************************************** ! !> write nonNewtonian Casson parameters into a lua file !! subroutine mus_nNwtn_CS_save( me, conf ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_CS_type ), intent(in) :: me type( aot_out_type ) :: conf ! -------------------------------------------------------------------------- call aot_out_val( put_conf = conf, & & vname = 'k0', & & val = me%k0 ) call aot_out_val( put_conf = conf, & & vname = 'k1', & & val = me%k1 ) end subroutine mus_nNwtn_CS_save ! ************************************************************************** ! ! ************************************************************************** ! !> Dump nonNewtonian fluid parameters to outUnit !! subroutine mus_nNwtn_dump2outUnit( me, outUnit ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_type ), intent(in) :: me integer, intent(in) :: outUnit ! -------------------------------------------------------------------------- if ( me%active ) then write(outUnit,'(A)') 'nonNewtonian fluid parameters:' write(outUnit,'(A)') ' model label: ', trim(me%label) ! dump model parameters by calling model dumper select case( me%model ) case ( powerLaw ) call mus_nNwtn_PL_dump( me%PL, outUnit ) case ( carreauYasuda ) call mus_nNwtn_CY_dump( me%CY, outUnit ) case ( casson ) call mus_nNwtn_CS_dump( me%CS, outUnit ) end select else write(outUnit,'(A)') 'No nonNewtonian table defined.' end if call tem_horizontalSpacer( fUnit = outUnit ) end subroutine mus_nNwtn_dump2outUnit ! ************************************************************************** ! ! ************************************************************************** ! !> Dump nonNewtonian Power Law (PL) parameters to outUnit !! subroutine mus_nNwtn_PL_dump( me, outUnit ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_PL_type ), intent(in) :: me integer, intent(in) :: outUnit ! -------------------------------------------------------------------------- write(outUnit,"( ' n = ', F8.4)") me%n write(outUnit,"( ' dynamic_viscosity_0 = ', F8.4)") me%visc0 end subroutine mus_nNwtn_PL_dump ! ************************************************************************** ! ! ************************************************************************** ! !> Dump nonNewtonian (CY) parameters to outUnit !! subroutine mus_nNwtn_CY_dump( me, outUnit ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_CY_type ), intent(in) :: me integer, intent(in) :: outUnit ! -------------------------------------------------------------------------- write(outUnit, "(' n = ', F8.4)") me%n write(outUnit, "(' a = ', F8.4)") me%a write(outUnit, "(' lambda = ', F8.4)") me%lambda write(outUnit, "(' dynamic_viscosity_0 = ', F8.4)") me%visc0 write(outUnit, "(' dynamic_viscosity_infty = ', F8.4)") me%viscInf end subroutine mus_nNwtn_CY_dump ! ************************************************************************** ! ! ************************************************************************** ! !> Dump nonNewtonian (CY) parameters to outUnit !! subroutine mus_nNwtn_CS_dump( me, outUnit ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_CS_type ), intent(in) :: me integer, intent(in) :: outUnit ! -------------------------------------------------------------------------- write(outUnit,"(' k0 = ', F8.4)") me%k0 write(outUnit,"(' k1 = ', F8.4)") me%k1 end subroutine mus_nNwtn_CS_dump ! ************************************************************************** ! ! ************************************************************************** ! !> nonNewtonian power-law model !! real(kind=rk) function viscPhy_PL( me, shearRate ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_type ), intent(in) :: me real(kind=rk), intent(in) :: shearRate ! -------------------------------------------------------------------------- viscPhy_PL = ( shearRate ** me%PL%nMinus1 ) * me%PL%visc0 end function viscPhy_PL ! ************************************************************************** ! ! ************************************************************************** ! !> nonNewtonian Casson model !! real(kind=rk) function viscPhy_CS( me, shearRate ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_type ), intent(in) :: me real(kind=rk), intent(in) :: shearRate ! -------------------------------------------------------------------------- real(kind=rk) :: t t = ( me%CS%k0 + me%CS%k1 * sqrt(shearRate) ) viscPhy_CS = t * t / shearRate end function viscPhy_CS ! ************************************************************************** ! ! ************************************************************************** ! !> nonNewtonian Carreau-Yasuda model !! real(kind=rk) function viscPhy_CY( me, shearRate ) ! -------------------------------------------------------------------------- !> nonNewtonian parameters type( mus_nNwtn_type ), intent(in) :: me real(kind=rk), intent(in) :: shearRate ! -------------------------------------------------------------------------- real(kind=rk) :: t t = ( 1._rk + (me%CY%lambda*shearRate) ** me%CY%a ) ** me%CY%nMinus1Div_a viscPhy_CY = me%CY%viscInf + ( me%CY%visc0 - me%CY%viscInf ) * t end function viscPhy_CY ! ************************************************************************** ! ! ************************************************************************** ! !> This routine assigns function pointer to compute non-Newtonian viscosity subroutine mus_assign_nNwtnVisc_ptr(nNwtn, schemeHeader) ! -------------------------------------------------------------------------- !> non-Newtonian type type(mus_nNwtn_type), intent(inout) :: nNwtn !> scheme header type(mus_scheme_header_type), intent(in) :: schemeHeader ! -------------------------------------------------------------------------- select case(trim(schemeHeader%kind)) case('fluid') select case(nNwtn%model) case (powerLaw) nNwtn%calcVisc => calcVisc_PL case (carreauYasuda) nNwtn%calcVisc => calcVisc_CY case (casson) nNwtn%calcVisc => calcVisc_CS end select case('fluid_incompressible') select case(nNwtn%model) case (powerLaw) nNwtn%calcVisc => calcVisc_incomp_PL case (carreauYasuda) nNwtn%calcVisc => calcVisc_incomp_CY case (casson) nNwtn%calcVisc => calcVisc_incomp_CS end select case default call tem_abort('Unknown scheme kind for non-Newtonian model') end select end subroutine mus_assign_nNwtnVisc_ptr ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian power-law model. !! $\mu = K shearRate^(n-1)$. !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_PL(nNwtn, viscKine, omega, state, neigh, auxField, & & densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, inv_rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, viscDynaPhy, coeffSR ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) inv_rho = 1.0_rk/rho ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, QQ ! calculate equilibrium density feq(idir) = layout%weight( idir ) & & * rho & & * ( 1._rk & & + ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & + (sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:))) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:)*vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz !nEqTens = nEqTens * (-1.5_rk) * omega(iElem)*convFac%strainRate*inv_rho ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it. ! physical unit conversion factor is pre-multiplied in coeffSR ! KM: Actual formula to compute strainrate has negative but since we ! calculating a magnitude, it is not used strainRate = coeffSR * omega(iElem) * inv_rho * nEqTensMag !strainRate = nEqTensMag ! compute shearRate shearRate = 2.0_rk * strainRate ! compute physical dynamic viscosity from non-Newtonian powerlaw model viscDynaPhy = (shearRate ** nNwtn%PL%nMinus1) * nNwtn%PL%visc0 ! viscKine_L = viscDyna_L / rho viscKine(iElem) = (viscDynaPhy / convFac%viscDyna) * inv_rho end do end subroutine calcVisc_PL ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian Casson model. !! $\mu = (k0 + k1 * sqrt(shearRate))^2/shearRate$ !! !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_CS(nNwtn, viscKine, omega, state, neigh, auxField, & & densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, inv_rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, viscTerm, coeffSR, viscDynaPhy ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state ( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) inv_rho = 1.0_rk/rho ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, QQ ! calculate equilibrium density feq(idir) = layout%weight( idir ) & & * rho & & * ( 1._rk & & + ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & + (sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:))) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:)*vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it ! physical unit conversion factor is pre-multiplied in coeffSR strainRate = coeffSR * omega(iElem) * inv_rho * nEqTensMag ! compute shearRate shearRate = 2.0_rk * strainRate ! compute dynamic viscosity from non-Newtonian Casson model ! mu = (k0 + k1 * sqrt(shearRate))**2/shearRate viscTerm = ( nNwtn%CS%k0 + nNwtn%CS%k1 * sqrt(shearRate) ) viscDynaPhy = viscTerm * viscTerm / shearRate ! convert to lattice kinematic viscosity viscKine(iElem) = ( viscDynaPhy / convFac%viscDyna) * inv_rho end do end subroutine calcVisc_CS ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian Carreau-Yasuda model. !! $\mu = \mu_\inf + (\mu_0-\mu_\inf)(1+(\lambda*shearRate)*a)^((n-1)/a)$ !! !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_CY(nNwtn, viscKine, omega, state, neigh, auxField, & & densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, inv_rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, v0_vInf, coeffSR real(kind=rk) :: viscDynaPhy, viscTerm ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ v0_vInf = nNwtn%CY%visc0 - nNwtn%CY%viscInf ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state ( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) inv_rho = 1.0_rk/rho ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, QQ ! calculate equilibrium density feq(idir) = layout%weight( idir ) & & * rho & & * ( 1._rk & & + ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & + (sum(layout%fstencil%cxdirrk(:,idir) * vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir) * vel(:))) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:)*vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it. ! physical unit conversion factor is pre-multiplied in coeffSR strainRate = coeffSR * omega(iElem) * inv_rho * nEqTensMag ! compute shearRate = 2*strainRate shearRate = 2.0_rk * strainRate ! compute dynamic viscosity from non-Newtonian Casson model ! mu = (k0 + k1 * sqrt(shearRate))**2/shearRate viscTerm = 1.0_rk + (nNwtn%CY%lambda*shearRate)**nNwtn%CY%a viscDynaPhy = nNwtn%CY%viscInf + v0_vInf & & * (viscTerm**nNwtn%CY%nMinus1Div_a) ! viscKine_L = viscDyna_L / rho viscKine(iElem) = (viscDynaPhy / convFac%viscDyna) * inv_rho end do end subroutine calcVisc_CY ! ************************************************************************** ! ! ************************************************************************** ! ! Incompressible model ! ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian power-law model for !! incompressible model !! $\mu = K shearRate^(n-1)$ !! !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_incomp_PL(nNwtn, viscKine, omega, state, neigh, & & auxField, densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, & & convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, viscDynaPhy, coeffSR ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state ( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, layout%fStencil%QQ feq(idir) = layout%weight( idir ) & & * ( rho + rho0 & & * ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & + ( sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) ) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:) * vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it. ! physical unit conversion factor is pre-multiplied in coeffSR strainRate = coeffSR * omega(iElem) * rho0Inv * nEqTensMag ! compute shearRate shearRate = 2.0_rk * strainRate ! compute physical dynamic viscosity from non-Newtonian powerlaw model viscDynaPhy = (shearRate ** nNwtn%PL%nMinus1) * nNwtn%PL%visc0 ! viscKine_L = viscDyna_L / rho viscKine(iElem) = (viscDynaPhy / convFac%viscDyna) * rho0Inv end do end subroutine calcVisc_incomp_PL ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian Casson model for !! incompressible model. !! $\mu = (k0 + k1 * sqrt(shearRate))^2/shearRate$ !! !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_incomp_CS(nNwtn, viscKine, omega, state, neigh, & & auxField, densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, & & convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, viscTerm, coeffSR, viscDynaPhy ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state ( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, layout%fStencil%QQ feq(idir) = layout%weight( idir ) & & * ( rho + rho0 & & * ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & + ( sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) ) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:) * vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it ! physical unit conversion factor is pre-multiplied in coeffSR strainRate = coeffSR * omega(iElem) * rho0Inv * nEqTensMag ! compute shearRate shearRate = 2.0_rk * strainRate ! compute dynamic viscosity from non-Newtonian Casson model ! mu = (k0 + k1 * sqrt(shearRate))**2/shearRate viscTerm = ( nNwtn%CS%k0 + nNwtn%CS%k1 * sqrt(shearRate) ) viscDynaPhy = viscTerm * viscTerm / shearRate ! convert to lattice kinematic viscosity viscKine(iElem) = ( viscDynaPhy / convFac%viscDyna) * rho0Inv end do end subroutine calcVisc_incomp_CS ! ************************************************************************** ! ! ************************************************************************** ! !> Calculate kinematic viscosity from nonNewtonian Carreau-Yasuda model for !! incompressible model. !! $\mu = \mu_\inf + (\mu_0-\mu_\inf)(1+(\lambda*shearRate)*a)^((n-1)/a)$ !! !! Shear rate is computed from strain rate which is computed from !! nonEquilibrium PDF which in turn computed from pre-collision PDF subroutine calcVisc_incomp_CY(nNwtn, viscKine, omega, state, neigh, & & auxField, densPos, velPos, nSize, nSolve, nScalars, nAuxScalars, layout, & & convFac) ! -------------------------------------------------------------------------- !> contains non-Newtonian model parameters loaded from config file class(mus_nNwtn_type), intent(in) :: nNwtn !> output: physical kinematic viscosity will be overwritten by !! non-Netonian model real(kind=rk), intent(inout) :: viscKine(:) !> Kinematic viscosity omega from last timestep real(kind=rk), intent(in) :: omega(:) !> state array real(kind=rk), intent(in) :: state(:) !> neigh array to obtain precollision pdf integer, intent(in) :: neigh(:) !> Auxiliary field variable array real(kind=rk), intent(in) :: auxField(:) !> position of density in auxField integer, intent(in) :: densPos !> position of velocity components in auxField integer, intent(in) :: velPos(3) !> number of elements in state array integer, intent(in) :: nSize !> Number of element to solve in this level integer, intent(in) :: nSolve !> number of scalars in state array integer, intent(in) :: nScalars !> number of scalars in auxField array integer, intent(in) :: nAuxScalars !> scheme layout type(mus_scheme_layout_type), intent(in) :: layout !> conversion factor to convert lattice to physical units type(mus_convertFac_type), intent(in) :: convFac ! -------------------------------------------------------------------------- integer :: iElem, iDir, QQ, elemOff real(kind=rk) :: rho, vel(3) !> precollision PDF real(kind=rk) :: f_preCol(layout%fStencil%QQ) real(kind=rk) :: fEq(layout%fStencil%QQ), nEq(layout%fStencil%QQ) real(kind=rk) :: nEqTens(6), nEqTensMag real(kind=rk) :: shearRate, strainRate, v0_vInf, coeffSR real(kind=rk) :: viscDynaPhy, viscTerm ! -------------------------------------------------------------------------- QQ = layout%fStencil%QQ v0_vInf = nNwtn%CY%visc0 - nNwtn%CY%viscInf ! constant coefficients in strainRate computation coeffSR = div1_2 * cs2inv * convFac%strainRate do iElem = 1, nSolve ! Get pre-collisiton PDF do iDir = 1, QQ f_preCol(iDir) = state ( & & neigh((idir-1)* nsize+ ielem)+( 1-1)* qq+ nscalars*0) end do ! Access density and velocity from auxField elemOff = (iElem-1)*nAuxScalars ! density rho = auxField( elemOff + densPos) ! velocity vel(1) = auxField( elemOff + velPos(1) ) vel(2) = auxField( elemOff + velPos(2) ) vel(3) = auxField( elemOff + velPos(3) ) ! Calculate the equilibrium distribution function do iDir = 1, layout%fStencil%QQ feq(idir) = layout%weight( idir ) & & * ( rho + rho0 & & * ( cs2inv & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & + ( sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) & & * sum(layout%fstencil%cxdirrk(:,idir)*vel(:)) ) & & * cs2inv * cs2inv * 0.5_rk & & - sum(vel(:) * vel(:)) * 0.5_rk * cs2inv ) ) end do ! Calculate the non-equilibrium part nEq(:) = f_preCol(:) - fEq(:) ! Now calculate the symmetric deviatoric second-order tensor of ! nonEquilibrium part ! the static part cs2 I is usually neglected for weakly compressible flows ! however, in current implementation it is considered ! now calculate the symmetric deviatoric second-order tensor of ! nonequilibrium part ! the static part cs2 i is usually neglected. ! however, in current implementation it is considered neqtens(1) = sum( (layout%fstencil%cxcx(1,:) - cs2) * neq) !xx neqtens(2) = sum( (layout%fstencil%cxcx(2,:) - cs2) * neq) !yy neqtens(3) = sum( (layout%fstencil%cxcx(3,:) - cs2) * neq) !zz neqtens(4) = sum( (layout%fstencil%cxcx(4,:) ) * neq) !xy neqtens(5) = sum( (layout%fstencil%cxcx(5,:) ) * neq) !yz neqtens(6) = sum( (layout%fstencil%cxcx(6,:) ) * neq) !xz ! compute strain ! magnitude of second-order tensor nEqTensMag = sqrt(nEqTens(1)**2 + nEqTens(2)**2 + nEqTens(3)**2 & & + 2.0_rk*(nEqTens(4)**2 + nEqTens(5)**2 + nEqTens(6)**2) ) ! omega from last time step ! convert shear-rate into physical unit because only ! non-Newtonian model requies it. ! physical unit conversion factor is pre-multiplied in coeffSR strainRate = coeffSR * omega(iElem) * rho0Inv * nEqTensMag ! compute shearRate = 2*strainRate shearRate = 2.0_rk * strainRate ! compute dynamic viscosity from non-Newtonian Casson model ! mu = (k0 + k1 * sqrt(shearRate))**2/shearRate viscTerm = 1.0_rk + (nNwtn%CY%lambda*shearRate)**nNwtn%CY%a viscDynaPhy = nNwtn%CY%viscInf + v0_vInf & & * (viscTerm**nNwtn%CY%nMinus1Div_a) ! viscKine_L = viscDyna_L / rho viscKine(iElem) = (viscDynaPhy / convFac%viscDyna) * rho0Inv end do end subroutine calcVisc_incomp_CY ! ************************************************************************** ! end module mus_nonNewtonian_module ! **************************************************************************** !