Subroutine to calculate state at the face, generalized for all direction : I,J, and K.
Type | Intent | Optional | Attributes | Name | ||
---|---|---|---|---|---|---|
real(kind=wp), | intent(in), | dimension(-2:dims%imx+2, -2:dims%jmx+2, -2:dims%kmx+2, 1:dims%n_var) | :: | qp | Store primitive variable at cell center |
|
real(kind=wp), | intent(inout), | dimension(1-flags(1):dims%imx-1+2*flags(1), 1-flags(2):dims%jmx-1+2*flags(2), 1-flags(3):dims%kmx-1+2*flags(3), 1:dims%n_var) | :: | f_qp_left | primitive state variable at faces |
|
real(kind=wp), | intent(inout), | dimension(1-flags(1):dims%imx-1+2*flags(1), 1-flags(2):dims%jmx-1+2*flags(2), 1-flags(3):dims%kmx-1+2*flags(3), 1:dims%n_var) | :: | f_qp_right | primitive state variable at faces |
|
integer, | intent(in), | dimension(3) | :: | flags | flags for direction switch |
|
type(extent), | intent(in) | :: | dims | Extent of the domain:imx,jmx,kmx |
subroutine compute_face_states(qp, f_qp_left, f_qp_right, flags, dims)
!< Subroutine to calculate state at the face, generalized for
!< all direction : I,J, and K.
implicit none
type(extent), intent(in) :: dims
!< Extent of the domain:imx,jmx,kmx
integer, dimension(3), intent(in) :: flags
!< flags for direction switch
real(wp), dimension(-2:dims%imx+2, -2:dims%jmx+2, -2:dims%kmx+2, 1:dims%n_var), intent(in) :: qp
!< Store primitive variable at cell center
real(wp), dimension(1-flags(1):dims%imx-1+2*flags(1), 1-flags(2):dims%jmx-1+2*flags(2), 1-flags(3):dims%kmx-1+2*flags(3), 1:dims%n_var), intent(inout) :: f_qp_left, f_qp_right
!< primitive state variable at faces
integer :: i, j, k, l
integer :: i_f=0, j_f=0, k_f=0
real(wp), dimension(3) :: P !< polynomial approximation
real(wp), dimension(3) :: B !< smoothness factor
real(wp), dimension(3) :: w !< wieght
real(wp), dimension(3) :: g !< linear wieght
real(wp), dimension(-2:2) :: u !< state_variable
real(wp) :: eps=1e-6
g(1) = 1.0/10.0
g(2) = 6.0/10.0
g(3) = 3.0/10.0
i_f = flags(1)
j_f = flags(2)
k_f = flags(3)
do l = 1, dims%n_var
do k = 1-k_f, dims%kmx-1+k_f
do j = 1-j_f, dims%jmx-1+j_f
do i = 1-i_f, dims%imx-1+i_f
U(-2) = qp(i-2*i_f,j-2*j_f,k-2*k_f,l) !u_{i-2}
U(-1) = qp(i-1*i_f,j-1*j_f,k-1*k_f,l) !u_{i-1}
u( 0) = qp(i ,j ,k ,l) !u_{i}
U( 1) = qp(i+1*i_f,j+1*j_f,k+1*k_f,l) !u_{i+1}
U( 2) = qp(i+2*i_f,j+2*j_f,k+2*k_f,l) !u_{i+2}
P(1) = ( 2.0*U(-2) - 7.0*U(-1) + 11.0*U(0))/6.0
P(2) = (-1.0*U(-1) + 5.0*U( 0) + 2.0*U(1))/6.0
P(3) = ( 2.0*U( 0) + 5.0*U( 1) - 1.0*U(2))/6.0
B(1) = (13.0/12.0)*(U(-2)-2.0*U(-1)+U(0))**2 + (1.0/4.0)*( U(-2)-4.0*U(-1)+3.0*U(0))**2
B(2) = (13.0/12.0)*(U(-1)-2.0*U( 0)+U(1))**2 + (1.0/4.0)*( U(-1)- U(1))**2
B(3) = (13.0/12.0)*(U( 0)-2.0*U( 1)+U(2))**2 + (1.0/4.0)*(3.0*U( 0)-4.0*U( 1)+ U(2))**2
w(:) = g(:)/(eps + B(:))**2
f_qp_left(i+i_f,j+j_f,k+k_f,l) = SUM(w*P)/SUM(w)
P(1) = ( 2.0*U(2) - 7.0*U( 1) + 11.0*U( 0))/6.0
P(2) = (-1.0*U(1) + 5.0*U( 0) + 2.0*U(-1))/6.0
P(3) = ( 2.0*U(0) + 5.0*U(-1) - 1.0*U(-2))/6.0
!B(1) = (13.0/12.0)*(U( 2)-2.0*U( 1)+U( 0))**2 + (1.0/4.0)*( U(2)-4.0*U( 1)+3.0*U( 0))**2
!B(2) = (13.0/12.0)*(U( 1)-2.0*U( 0)+U(-1))**2 + (1.0/4.0)*( U(1)- U(-1))**2
!B(3) = (13.0/12.0)*(U( 0)-2.0*U(-1)+U(-2))**2 + (1.0/4.0)*(3.0*U(0)-4.0*U(-1)+ U(-2))**2
w(1) = g(1)/(eps + B(3))**2
w(2) = g(2)/(eps + B(2))**2
w(3) = g(3)/(eps + B(1))**2
f_qp_right(i,j,k,l) = SUM(w*P)/SUM(w)
end do
end do
end do
end do
end subroutine compute_face_states