#include "Includes.h"
Module Physics_NSSAKeywordsModule
IMPLICIT NONE
INTEGER, PARAMETER :: KEYWORD_LENGTH = 132
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: REFERENCE_TEMPERATURE_KEY = "reference temperature (k)"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: REFERENCE_PRESSURE_KEY = "reference pressure (pa)"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: MACH_NUMBER_KEY = "mach number"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: REYNOLDS_NUMBER_KEY = "reynolds number"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: PRANDTL_NUMBER_KEY = "prandtl number"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: TURBULENT_PRANDTL_NUMBER_KEY = "turbulent prandtl number"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: FROUDE_NUMBER_KEY = "froude number"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: GRAVITY_DIRECTION_KEY = "gravity direction"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: AOA_THETA_KEY = "aoa theta"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: AOA_PHI_KEY = "aoa phi"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: FLOW_EQUATIONS_KEY = "flow equations"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: LESMODEL_KEY = "les model"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: COMPUTE_GRADIENTS_KEY = "compute gradients"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: SUTHERLAND_TEMPERATURE_KEY = "sutherland temperature"
CHARACTER(LEN = KEYWORD_LENGTH), PARAMETER :: SUTHERLAND_REF_TEMPERATURE_KEY = "sutherland reference temperature"
CHARACTER(LEN=KEYWORD_LENGTH), DIMENSION(2) :: physics_NSSAKeywords = [MACH_NUMBER_KEY, FLOW_EQUATIONS_KEY]
!PARTICLES
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: particlesKey = "lagrangian particles"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: numberOfParticlesKey = "number of particles"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: particlesPerParcelKey = "particles per parcel"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: sourceTermKey = "high order particles source term"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: STOKES_NUMBER_PART_KEY = "stokes number"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: GAMMA_PART_KEY = "gamma"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PHI_M_PART_KEY = "phi_m"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: I0_PART_KEY = "radiation source"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: MIN_BOX_KEY = "minimum box"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: MAX_BOX_KEY = "maximum box"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: BC_BOX_KEY = "bc box"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_FILE_KEY = "particles file"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_LOG_FILE_KEY = "vel and temp from file"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_LOG_INJ_KEY = "injection"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_INJ_KEY = "particles injection"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_NUMB_PER_STEP_KEY = "particles per step"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: PART_PERIOD_KEY = "particles iter period"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: INJ_VEL_KEY = "particles injection velocity"
CHARACTER(LEN=KEYWORD_LENGTH), PARAMETER :: INJ_TEMP_KEY = "particles injection temperature"
END MODULE Physics_NSSAKeywordsModule
!
!////////////////////////////////////////////////////////////////////////
!
! ******
MODULE PhysicsStorage_NSSA
! ******
!
USE SMConstants
use FluidData_NSSA
use FileReadingUtilities, only: getRealArrayFromString
IMPLICIT NONE
private
public flowIsNavierStokes, NCONS, NGRAD
public IRHO, IRHOU, IRHOV, IRHOW, IRHOE, IRHOTHETA
public NPRIM, IPIRHO, IPU, IPV, IPW, IPP, IPT, IPA2
public TemperatureReNormalization_Sutherland, S_div_TRef_Sutherland
public computeGradients
public ConstructPhysicsStorage_NSSA, DestructPhysicsStorage_NSSA, DescribePhysicsStorage_NSSA
public CheckPhysicsNSInputIntegrity
public GRADVARS_STATE, GRADVARS_ENTROPY, GRADVARS_ENERGY
public grad_vars, SetGradientVariables
! ----------------------------
! Either NavierStokes or Euler
! ----------------------------
!
logical, protected :: flowIsNavierStokes = .true.
logical, protected :: computeGradients = .true.
!
! --------------------------
!! The sizes of the NS system
! --------------------------
! -------------------------------------------
!! The positions of the conservative variables
! -------------------------------------------
!
INTEGER, PARAMETER :: NCONS = 6, NGRAD = 6
INTEGER, PARAMETER :: IRHO = 1 , IRHOU = 2 , IRHOV = 3 , IRHOW = 4 , IRHOE = 5, IRHOTHETA = 6
!
! ----------------------------------------
!! The positions of the primitive variables
! ----------------------------------------
!
INTEGER, PARAMETER :: NPRIM = 7
INTEGER, PARAMETER :: IPIRHO = 1, IPU = 2, IPV = 3, IPW = 4, IPP = 5, IPT = 6, IPA2 = 7
!
real(kind=RP), protected :: TRef_Sutherland ! Sutherland's reference temperature
real(kind=RP), protected :: S_Sutherland ! Sutherland's temperature
real(kind=RP), protected :: TemperatureReNormalization_Sutherland ! TRef/SutherlandsTRef
real(kind=RP), protected :: S_div_Tref_Sutherland
!
! --------------------------------
! Choice of the gradient variables
! --------------------------------
!
enum, bind(C)
enumerator :: GRADVARS_STATE, GRADVARS_ENTROPY, GRADVARS_ENERGY
end enum
integer, protected :: grad_vars = GRADVARS_STATE
!
! ------------------------------
! Thermodynamic specs of the Air
! ------------------------------
!
type(Thermodynamics_t), target, private :: ThermodynamicsAir = Thermodynamics_t( &
"Air", & ! Name
287.058_RP, & ! R ! J / (kg * °K)
1.4_RP, & ! gamma
sqrt(1.4_RP), & ! sqrtGamma
1.4_RP - 1.0_RP, & ! gammaMinus1
(1.4_RP - 1.0_RP) / 2.0_RP, & ! gammaMinus1Div2
(1.4_RP + 1.0_RP) / 2.0_RP, & ! gammaPlus1Div2
(1.4_RP - 1.0_RP) / (2.0_RP * sqrt(1.4_RP)), & ! gammaMinus1Div2sg
(1.4_RP - 1.0_RP) / (2.0_RP * 1.4_RP), & ! gammaMinus1Div2g
2.0_RP / (1.4_RP + 1.0_RP), & ! InvGammaPlus1Div2
1.0_RP / (1.4_RP - 1.0_RP), & ! InvGammaMinus1
1.0_RP / 1.4_RP, & ! InvGamma
1.4_RP / ( 1.4_RP - 1.0_RP ), & ! gammaDivGammaMinus1
287.058_RP * 1.4_RP / ( 1.4_RP - 1.0_RP ), & ! cp
287.058_RP / ( 1.4_RP - 1.0_RP ), & ! cv
0.0_RP & ! Bulk viscosity ratio
)
!
! ========
CONTAINS
! ========
!
! ///////////////////////////////////////////////////////
!
! --------------------------------------------------
!! Constructor: Define default values for the physics
!! variables.
! --------------------------------------------------
!
SUBROUTINE ConstructPhysicsStorage_NSSA( controlVariables, Lref, timeref, success )
USE FTValueDictionaryClass
USE Physics_NSSAKeywordsModule
use Utilities, only: toLower, almostEqual
!
! ---------
! Arguments
! ---------
!
TYPE(FTValueDictionary) :: controlVariables
real(kind=RP), intent(in) :: Lref
real(kind=RP), intent(out) :: timeref
LOGICAL :: success
!
! ---------------
! Local variables
! ---------------
!
CHARACTER(LEN=KEYWORD_LENGTH) :: keyword
type(Thermodynamics_t), pointer :: thermodynamics_
type(RefValues_t) :: refValues_
type(Dimensionless_t) :: dimensionless_
real(kind=RP), allocatable :: array(:)
!
! --------------------
! Collect input values
! --------------------
!
success = .TRUE.
CALL CheckPhysicsNSInputIntegrity(controlVariables,success)
IF(.NOT. success) RETURN
!
!
! ---------------------
! Set the gas to be air
! ---------------------
!
thermodynamics_ => thermodynamicsAir
!
! ------------------------
! Dimensionless quantities
! ------------------------
!
dimensionless_ % cp = thermodynamics_ % gamma * thermodynamics_ % InvGammaMinus1
dimensionless_ % cv = thermodynamics_ % InvGammaMinus1
dimensionless_ % Mach = controlVariables % doublePrecisionValueForKey(MACH_NUMBER_KEY)
if ( controlVariables % ContainsKey(PRANDTL_NUMBER_KEY) ) then
dimensionless_ % Pr = controlVariables % doublePrecisionValueForKey(PRANDTL_NUMBER_KEY)
else
dimensionless_ % Pr = 0.72_RP
end if
if ( controlVariables % ContainsKey(TURBULENT_PRANDTL_NUMBER_KEY) ) then
dimensionless_ % Prt = controlVariables % doublePrecisionValueForKey(TURBULENT_PRANDTL_NUMBER_KEY)
else
dimensionless_ % Prt = 0.9_RP
end if
!
! *********************
! Select flow equations
! *********************
!
keyword = controlVariables % stringValueForKey(FLOW_EQUATIONS_KEY,KEYWORD_LENGTH)
CALL toLower(keyword)
IF ( keyword == "euler" ) THEN
flowIsNavierStokes = .FALSE.
dimensionless_ % Re = 0.0_RP
dimensionless_ % mu = 0.0_RP
dimensionless_ % kappa = 0.0_RP
ELSE
flowIsNavierStokes = .TRUE.
!
! ----------------------------
! Look for the Reynolds number
! ----------------------------
!
IF ( controlVariables % containsKey(REYNOLDS_NUMBER_KEY) ) THEN
dimensionless_ % Re = controlVariables % doublePrecisionValueForKey(REYNOLDS_NUMBER_KEY)
ELSE
PRINT *, "Input file is missing entry for keyword: ", REYNOLDS_NUMBER_KEY
success = .FALSE.
RETURN
END IF
!
! ------------------------------------------------
! Set molecular viscosity and thermal conductivity
! ------------------------------------------------
!
if ( .not. almostEqual(dimensionless_ % Re, 0.0_RP) ) then
dimensionless_ % mu = 1.0_RP / dimensionless_ % Re
dimensionless_ % kappa = 1.0_RP / ( thermodynamics_ % gammaMinus1 * &
POW2( dimensionless_ % Mach) * &
dimensionless_ % Re * dimensionless_ % Pr )
else
dimensionless_ % mu = 0.0_RP
dimensionless_ % kappa = 0.0_RP
end if
dimensionless_ % mu_to_kappa = 1.0_RP / (thermodynamics_ % gammaMinus1*POW2(dimensionless_ % Mach)* dimensionless_ % Pr)
dimensionless_ % mut_to_kappa_SA = 1.0_RP / (thermodynamics_ % gammaMinus1*POW2(dimensionless_ % Mach)* dimensionless_ % Prt)
END IF
!
! **************************************
! Check if state gradients are requested
! **************************************
!
if ( controlVariables % containsKey(COMPUTE_GRADIENTS_KEY) ) then
!
! Do not compute gradients if Euler equations are used and it is specified in the control file
! --------------------------------------------------------------------------------------------
if ( .not. flowIsNavierStokes ) then
if ( .not. controlVariables % logicalValueForKey(COMPUTE_GRADIENTS_KEY) ) then
computeGradients = .false.
end if
end if
else
!
! Do not compute gradients if Euler equations and the default option is selected
! ------------------------------------------------------------------------------
if ( .not. flowIsNavierStokes ) then
computeGradients = .false.
end if
end if
dimensionless_ % gammaM2 = thermodynamics_ % gamma * POW2( dimensionless_ % Mach )
!
! ********************
! Set reference values
! ********************
!
if ( controlVariables % ContainsKey(REFERENCE_TEMPERATURE_KEY) ) then
refValues_ % T = controlVariables % DoublePrecisionValueForKey(REFERENCE_TEMPERATURE_KEY)
else
refValues_ % T = 520.0_RP*5.0_RP/9.0_RP ! ≃ 288.88 K
end if
if ( controlVariables % ContainsKey(REFERENCE_PRESSURE_KEY) ) then
refValues_ % rho = controlVariables % DoublePrecisionValueForKey(REFERENCE_PRESSURE_KEY) / (thermodynamics_ % R * refValues_ % T)
else
refValues_ % rho = 101325.0_RP / (thermodynamics_ % R * refValues_ % T)
end if
refValues_ % V = dimensionless_ % Mach &
* sqrt( thermodynamics_ % gamma * thermodynamics_ % R * refValues_ % T )
refValues_ % p = refValues_ % rho * POW2( refValues_ % V )
if ( flowIsNavierStokes ) then
dimensionless_ % niu = dimensionless_ % mu * refValues_ % rho
refValues_ % mu = refValues_ % rho * refValues_ % V * Lref * dimensionless_ % mu
refValues_ % niu = refValues_ % mu / refValues_ % rho
refValues_ % kappa = refValues_ % mu * thermodynamics_ % cp / dimensionless_ % Pr
else
refValues_ % mu = 0.0_RP
refValues_ % kappa = 0.0_RP
end if
timeref = Lref / refValues_ % V
!
! *******************************************
! Set the Froude number and gravity direction
! *******************************************
!
if ( controlVariables % ContainsKey(FROUDE_NUMBER_KEY) ) then
dimensionless_ % Fr = controlVariables % DoublePrecisionValueForKey(FROUDE_NUMBER_KEY)
else
!
! Default Froude number: earth's gravity
! --------------------------------------
dimensionless_ % Fr = refValues_ % V / sqrt(9.81_RP * Lref)
end if
if ( controlVariables % ContainsKey(GRAVITY_DIRECTION_KEY) ) then
allocate(array(1:3))
array = getRealArrayFromString( controlVariables % StringValueForKey(GRAVITY_DIRECTION_KEY,&
KEYWORD_LENGTH))
dimensionless_ % gravity_dir = array(1:3)
if ( norm2(dimensionless_ % gravity_dir) < epsilon(1.0_RP)*10.0_RP ) then
!
! Disable gravity
! ---------------
dimensionless_ % gravity_dir = 0.0_RP
dimensionless_ % invFr2 = 0.0_RP
dimensionless_ % Fr = huge(1.0_RP)
else
dimensionless_ % gravity_dir = dimensionless_ % gravity_dir / norm2(dimensionless_ % gravity_dir)
dimensionless_ % invFr2 = 1.0_RP / POW2(dimensionless_ % Fr)
end if
else
if ( controlVariables % ContainsKey(FROUDE_NUMBER_KEY) ) then
print*, "When specifying a Froude number, the gravity direction must be specified"
print*, "Gravity direction = [x,y,z]"
errorMessage(STD_OUT)
error stop
else
!
! Gravity is disabled
! -------------------
dimensionless_ % gravity_dir = 0.0_RP
dimensionless_ % Fr = huge(1.0_RP)
dimensionless_ % invFr2 = 0.0_RP
end if
end if
!
! **********
! LES Models
! **********
!
if ( controlVariables % containsKey(LESMODEL_KEY)) then
if ( controlVariables % stringValueForKey(LESMODEL_KEY,4) .ne. "none") then
!
! Enable NS fluxes
! ----------------
flowIsNavierStokes = .true.
computeGradients = .true.
end if
end if
!
! ***************
! Angle of attack
! ***************
!
IF ( controlVariables % containsKey(AOA_PHI_KEY) ) THEN
refValues_ % AOAPhi = controlVariables % doublePrecisionValueForKey(AOA_PHI_KEY)
ELSE
!
! Phi angle of attack is zero by default
! --------------------------------------
refValues_ % AOAPhi = 0.0_RP
END IF
IF ( controlVariables % containsKey(AOA_THETA_KEY) ) THEN
refValues_ % AOATheta = controlVariables % doublePrecisionValueForKey(AOA_THETA_KEY)
ELSE
!
! Theta angle of attack is zero by default
! ----------------------------------------
refValues_ % AOATheta = 0.0_RP
END IF
!
! **************************
! Sutherland's law constants
! **************************
!
if ( controlVariables % ContainsKey(SUTHERLAND_TEMPERATURE_KEY) ) then
S_Sutherland = controlVariables % DoublePrecisionValueForKey(SUTHERLAND_TEMPERATURE_KEY)
else
S_Sutherland = 198.6_RP*5.0_RP/9.0_RP ! ≃ 110.4
end if
if ( controlVariables % ContainsKey(SUTHERLAND_REF_TEMPERATURE_KEY) ) then
TRef_Sutherland = controlVariables % DoublePrecisionValueForKey(SUTHERLAND_REF_TEMPERATURE_KEY)
else
TRef_Sutherland = refValues_ % T
end if
S_div_TRef_Sutherland = S_Sutherland / TRef_Sutherland
TemperatureReNormalization_Sutherland = refValues_ % T / TRef_Sutherland
!
! **********************************************************************
! Set the global (proteted) thermodynamics, dimensionless, and refValues
! **********************************************************************
!
call setThermodynamics( thermodynamics_ )
call setDimensionless( dimensionless_ )
call setRefValues( refValues_ )
END SUBROUTINE ConstructPhysicsStorage_NSSA
!
! ///////////////////////////////////////////////////////
!
! -------------------------------------------------
!! Destructor: Does nothing for this storage
! -------------------------------------------------
!
SUBROUTINE DestructPhysicsStorage_NSSA
END SUBROUTINE DestructPhysicsStorage_NSSA
!
! //////////////////////////////////////////////////////
!
! -----------------------------------------
!! Descriptor: Shows the gathered data
! -----------------------------------------
!
SUBROUTINE DescribePhysicsStorage_NSSA()
USE Headers
use MPI_Process_Info
IMPLICIT NONE
real(kind=RP) :: pRef
if ( .not. MPI_Process % isRoot ) return
pRef = thermodynamics % R * refValues % rho * refValues % T
write(STD_OUT,'(/,/)')
if (flowIsNavierStokes) then
call Section_Header("Loading Navier-Stokes physics")
else
call Section_Header("Loading Euler physics")
end if
write(STD_OUT,'(/)')
call SubSection_Header("Fluid data")
write(STD_OUT,'(30X,A,A22,A10)') "->" , "Gas: " , "Air"
write(STD_OUT,'(30X,A,A22,F10.3,A)') "->" , "State constant: " , thermodynamics % R, " I.S."
write(STD_OUT,'(30X,A,A22,F10.3)') "->" , "Specific heat ratio: " , thermodynamics % gamma
write(STD_OUT,'(/)')
call SubSection_Header("Reference quantities")
write(STD_OUT,'(30X,A,A30,F10.3,A)') "->" , "Reference Temperature: " , refValues % T, " K."
write(STD_OUT,'(30X,A,A30,F10.3,A)') "->" , "Reference pressure: " , pRef, " Pa."
write(STD_OUT,'(30X,A,A30,F10.3,A)') "->" , "Reference density: " , refValues % rho , " kg/m^3."
write(STD_OUT,'(30X,A,A30,F10.3,A)') "->" , "Reference velocity: " , refValues % V , " m/s."
if ( flowIsNavierStokes ) then
write(STD_OUT,'(30X,A,A30,1pG10.3,A)') "->" , "Reference viscosity: ",refValues % mu , " Pa·s."
write(STD_OUT,'(30X,A,A30,1pG10.3,A)') "->" , "Reference conductivity: ", refValues % kappa, " W/(m·K)."
end if
write(STD_OUT,'(/)')
call SubSection_Header("Dimensionless quantities")
write(STD_OUT,'(30X,A,A27,F10.3)') "->" , "Mach number: " , dimensionless % Mach
if ( flowIsNavierStokes ) then
write(STD_OUT,'(30X,A,A27,ES10.3)') "->" , "Reynolds number: " , dimensionless % Re
write(STD_OUT,'(30X,A,A27,F10.3)') "->" , "Prandtl number: " , dimensionless % Pr
write(STD_OUT,'(30X,A,A27,F10.3)') "->" , "Turbulent Prandtl number: " , dimensionless % Prt
end if
write(STD_OUT,'(30X,A,A27,F10.3)') "->" , "Froude number: " , dimensionless % Fr
write(STD_OUT,'(30X,A,A27,A,F4.1,A,F4.1,A,F4.1,A)') "->" , "Gravity direction: ","[", &
dimensionless % gravity_dir(1), ", ", &
dimensionless % gravity_dir(2), ", ", &
dimensionless % gravity_dir(3), "]"
END SUBROUTINE DescribePhysicsStorage_NSSA
!
!////////////////////////////////////////////////////////////////////////
!
SUBROUTINE CheckPhysicsNSInputIntegrity( controlVariables, success )
USE FTValueDictionaryClass
USE Physics_NSSAKeywordsModule
IMPLICIT NONE
!
! ---------
! Arguments
! ---------
!
TYPE(FTValueDictionary) :: controlVariables
LOGICAL :: success
!
! ---------------
! Local variables
! ---------------
!
CLASS(FTObject), POINTER :: obj
INTEGER :: i
success = .TRUE.
DO i = 1, SIZE(physics_NSSAKeywords)
obj => controlVariables % objectForKey(physics_NSSAKeywords(i))
IF ( .NOT. ASSOCIATED(obj) ) THEN
PRINT *, "Input file is missing entry for keyword: ",physics_NSSAKeywords(i)
success = .FALSE.
END IF
END DO
END SUBROUTINE CheckPhysicsNSInputIntegrity
subroutine SetGradientVariables(grad_vars_)
implicit none
integer, intent(in) :: grad_vars_
select case(grad_vars_)
case(GRADVARS_STATE, GRADVARS_ENTROPY, GRADVARS_ENERGY)
grad_vars = grad_vars_
case default
print*, "Unrecognized option"
errorMessage(STD_OUT)
error stop
end select
end subroutine SetGradientVariables
!
! **********
END MODULE PhysicsStorage_NSSA
! **********
