diff --git a/srcF/module_z0t_lake.f90 b/srcF/module_z0t_lake.f90
deleted file mode 100644
index 628d4db5ff409a75622575cd929dc08a44372d4e..0000000000000000000000000000000000000000
--- a/srcF/module_z0t_lake.f90
+++ /dev/null
@@ -1,150 +0,0 @@
-module module_z0t_lake
-    !< @brief surface thermal roughness parameterizations for ocean
-
-    implicit none
-    
-   
-    public :: get_thermal_roughness_kl
-    public :: get_thermal_roughness_ca
-    public :: get_thermal_roughness_zm
-    public :: get_thermal_roughness_br
-    public :: get_thermal_roughness_re
-    
-
-
-
-    ! --------------------------------------------------------------------------------
-    real, parameter, private :: kappa = 0.40         !< von Karman constant [n/d]
-    real, parameter, private :: Pr_m = 0.71              !< molecular Prandtl number (air) [n/d]
-    !< Re fully roughness minimum value [n/d]
-    real, parameter ::  Re_rough_min = 16.3
-    !< roughness model coeff. [n/d]
-    !< --- transitional mode
-    !<     B = log(z0_m / z0_t) = B1 * log(B3 * Re) + B2
-    real, parameter :: B1_rough = 5.0 / 6.0
-    real, parameter :: B2_rough = 0.45
-    real, parameter :: B3_rough = kappa * Pr_m
-    !< --- fully rough mode (Re > Re_rough_min)
-    !<     B = B4 * Re^(B2)
-    real, parameter :: B4_rough =(0.14 * (30.0**B2_rough)) * (Pr_m**0.8)
-
-    real, parameter :: B_max_lake = 8.0
-    
-
-    contains
-
-    
-     ! thermal roughness definition by Kazakov, Lykosov
-     ! --------------------------------------------------------------------------------
-       subroutine get_thermal_roughness_kl(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        ! ----------------------------------------------------------------------------
-
-         !--- define B = log(z0_m / z0_t)
-        if (Re <= Re_rough_min) then
-            B = B1_rough * alog(B3_rough * Re) + B2_rough
-        else
-            ! *: B4 takes into account Re value at z' ~ O(10) z0
-            B = B4_rough * (Re**B2_rough)
-        end if
-         
-            B = min(B, B_max_lake)
-       
-       z0_t = z0_m / exp(B)
-
-     end subroutine
-    
-        
-
-    ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Cahill, A.T., Parlange, M.B., Albertson, J.D., 1997.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_ca(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-3.8         !4-Cahill et al. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition z0_t = C*z0_m  
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_zm(z0_t, B, &
-            z0_m, Czm)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Czm                 !< proportionality coefficient
-        
-       
-
-        z0_t =Czm*z0_m
-        B=log(z0_m / z0_t)
-    end subroutine
-     ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Brutsaert W., 2003.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_br(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-2.0       !Brutsaert
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-
-! thermal roughness definition by Repina, 2023.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_re(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-      
-       
-        
-        B=alog(-0.56*(4.0*(Re)**(0.5)-3.4))     !Repina, 2023
-
-
-       ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)   
-       
-    end subroutine
-
-end module module_z0t_lake
diff --git a/srcF/module_z0t_land.f90 b/srcF/module_z0t_land.f90
deleted file mode 100644
index ae78742dacbb3b2831189ccaea44320915e122b7..0000000000000000000000000000000000000000
--- a/srcF/module_z0t_land.f90
+++ /dev/null
@@ -1,219 +0,0 @@
-module module_z0t
-    !< @brief surface thermal roughness parameterizations for land
-
-    implicit none
-    
-   
-    public :: get_thermal_roughness_kl
-    public :: get_thermal_roughness_cz
-    public :: get_thermal_roughness_zi
-    public :: get_thermal_roughness_ca
-    public :: get_thermal_roughness_zm
-    public :: get_thermal_roughness_ot
-    public :: get_thermal_roughness_du
-    public :: get_thermal_roughness_mix
-
-
-
-    ! --------------------------------------------------------------------------------
-    real, parameter, private :: kappa = 0.40         !< von Karman constant [n/d]
-    real, parameter, private :: Pr_m = 0.71              !< molecular Prandtl number (air) [n/d]
-    !< Re fully roughness minimum value [n/d]
-    real, parameter ::  Re_rough_min = 16.3
-    !< roughness model coeff. [n/d]
-    !< --- transitional mode
-    !<     B = log(z0_m / z0_t) = B1 * log(B3 * Re) + B2
-    real, parameter :: B1_rough = 5.0 / 6.0
-    real, parameter :: B2_rough = 0.45
-    real, parameter :: B3_rough = kappa * Pr_m
-    !< --- fully rough mode (Re > Re_rough_min)
-    !<     B = B4 * Re^(B2)
-    real, parameter :: B4_rough =(0.14 * (30.0**B2_rough)) * (Pr_m**0.8)
-
-    real, parameter :: B_max_land = 2.0
-    
-
-    contains
-
-    
-     ! thermal roughness definition by Kazakov, Lykosov
-     ! --------------------------------------------------------------------------------
-       subroutine get_thermal_roughness_kl(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        ! ----------------------------------------------------------------------------
-
-         !--- define B = log(z0_m / z0_t)
-        if (Re <= Re_rough_min) then
-            B = B1_rough * alog(B3_rough * Re) + B2_rough
-        else
-            ! *: B4 takes into account Re value at z' ~ O(10) z0
-            B = B4_rough * (Re**B2_rough)
-        end if
-         
-            B = min(B, B_max_land)
-       
-       z0_t = z0_m / exp(B)
-
-     end subroutine
-    ! --------------------------------------------------------------------------------  
-        
-    ! thermal roughness definition by Chen, F., Zhang, Y., 2009. 
-    ! --------------------------------------------------------------------------------  
-    subroutine get_thermal_roughness_cz(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-        
-       
-        B=(kappa*10.0**(-0.4*z0_m/0.07))*(Re**0.45)        !Chen and Zhang
-        
-         ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-      ! --------------------------------------------------------------------------------
-        ! thermal roughness definition by Zilitinkevich, S., 1995.
-        ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_zi(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-       
-        B=0.1*kappa*(Re**0.5)         !6-Zilitinkevich
-       
-       
-
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Cahill, A.T., Parlange, M.B., Albertson, J.D., 1997.
-     ! It is better to use for dynamic surfaces such as sand
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_ca(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-3.8         !4-Cahill et al. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Owen P. R., Thomson W. R., 1963. 
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_ot(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-    
-        
-        
-        B=kappa*(Re**0.45)         !Owen P. R., Thomson W. R. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition by Duynkerke P. G., 1992. 
-    !It is better to use for surfaces wiht forest
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_du(z0_t, B, &
-            z0_m, u_dyn, LAI)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: u_dyn              !< dynamic velocity [m/s]
-        real, intent(in) :: LAI                 !< leaf-area index
-       
-       
-        
-        
-        B=(13*u_dyn**0.4)/LAI+0.85         !Duynkerke P. G., 1992. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition z0_t = C*z0_m  
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_zm(z0_t, B, &
-            z0_m, Czm)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Czm                 !< proportionality coefficient
-        
-       
-
-        z0_t =Czm*z0_m
-        B=log(z0_m / z0_t)
-    end subroutine
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition by  Chen and Zhang  and Zilitinkevich
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_mix(z0_t, B, &
-            z0_m, u_dyn, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: u_dyn              !< dynamic velocity [m/s]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-    
-       
-        real, parameter :: u_dyn_th=0.17         !< dynamic velocity treshhold [m/s]
-        
-        if (u_dyn <= u_dyn_th) then
-          B=0.1*kappa*(Re**0.5)  !Zilitinkevich
-        else
-            B=(kappa*10.0**(-0.4*z0_m/0.07))*(Re**0.45) !Chen and Zhang
-        end if
-       
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-
-
-end module module_z0t
diff --git a/srcF/module_z0t_ocean.f90 b/srcF/module_z0t_ocean.f90
deleted file mode 100644
index bd0d6e5243ccd012250dbe6a003b0ac63cc09ceb..0000000000000000000000000000000000000000
--- a/srcF/module_z0t_ocean.f90
+++ /dev/null
@@ -1,125 +0,0 @@
-module module_z0t_ocean
-    !< @brief surface thermal roughness parameterizations for ocean
-
-    implicit none
-    
-   
-    public :: get_thermal_roughness_kl
-    public :: get_thermal_roughness_ca
-    public :: get_thermal_roughness_zm
-    public :: get_thermal_roughness_br
-    
-
-
-
-    ! --------------------------------------------------------------------------------
-    real, parameter, private :: kappa = 0.40         !< von Karman constant [n/d]
-    real, parameter, private :: Pr_m = 0.71              !< molecular Prandtl number (air) [n/d]
-    !< Re fully roughness minimum value [n/d]
-    real, parameter ::  Re_rough_min = 16.3
-    !< roughness model coeff. [n/d]
-    !< --- transitional mode
-    !<     B = log(z0_m / z0_t) = B1 * log(B3 * Re) + B2
-    real, parameter :: B1_rough = 5.0 / 6.0
-    real, parameter :: B2_rough = 0.45
-    real, parameter :: B3_rough = kappa * Pr_m
-    !< --- fully rough mode (Re > Re_rough_min)
-    !<     B = B4 * Re^(B2)
-    real, parameter :: B4_rough =(0.14 * (30.0**B2_rough)) * (Pr_m**0.8)
-
-    real, parameter :: B_max_ocean = 8.0
-    
-
-    contains
-
-    
-     ! thermal roughness definition by Kazakov, Lykosov
-     ! --------------------------------------------------------------------------------
-       subroutine get_thermal_roughness_kl(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        ! ----------------------------------------------------------------------------
-
-         !--- define B = log(z0_m / z0_t)
-        if (Re <= Re_rough_min) then
-            B = B1_rough * alog(B3_rough * Re) + B2_rough
-        else
-            ! *: B4 takes into account Re value at z' ~ O(10) z0
-            B = B4_rough * (Re**B2_rough)
-        end if
-         
-            B = min(B, B_max_ocean)
-       
-       z0_t = z0_m / exp(B)
-
-     end subroutine
-    
-        
-
-    ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Cahill, A.T., Parlange, M.B., Albertson, J.D., 1997.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_ca(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-3.8         !4-Cahill et al. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition z0_t = C*z0_m  
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_zm(z0_t, B, &
-            z0_m, Czm)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Czm                 !< proportionality coefficient
-        
-       
-
-        z0_t =Czm*z0_m
-        B=log(z0_m / z0_t)
-    end subroutine
-     ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Brutsaert W., 2003.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_br(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-2.0       !Brutsaert
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-end module module_z0t_ocean
diff --git a/srcF/module_z0t_snow.f90 b/srcF/module_z0t_snow.f90
deleted file mode 100644
index a8545a9409a2217920b5f7bd0d7e9163e0566256..0000000000000000000000000000000000000000
--- a/srcF/module_z0t_snow.f90
+++ /dev/null
@@ -1,125 +0,0 @@
-module module_z0t_snow
-    !< @brief surface thermal roughness parameterizations for snow
-
-    implicit none
-    
-   
-    public :: get_thermal_roughness_kl
-    public :: get_thermal_roughness_ca
-    public :: get_thermal_roughness_zm
-    public :: get_thermal_roughness_br
-    
-
-
-
-    ! --------------------------------------------------------------------------------
-    real, parameter, private :: kappa = 0.40         !< von Karman constant [n/d]
-    real, parameter, private :: Pr_m = 0.71              !< molecular Prandtl number (air) [n/d]
-    !< Re fully roughness minimum value [n/d]
-    real, parameter ::  Re_rough_min = 16.3
-    !< roughness model coeff. [n/d]
-    !< --- transitional mode
-    !<     B = log(z0_m / z0_t) = B1 * log(B3 * Re) + B2
-    real, parameter :: B1_rough = 5.0 / 6.0
-    real, parameter :: B2_rough = 0.45
-    real, parameter :: B3_rough = kappa * Pr_m
-    !< --- fully rough mode (Re > Re_rough_min)
-    !<     B = B4 * Re^(B2)
-    real, parameter :: B4_rough =(0.14 * (30.0**B2_rough)) * (Pr_m**0.8)
-
-    real, parameter :: B_max_snow = 8.0
-    
-
-    contains
-
-    
-     ! thermal roughness definition by Kazakov, Lykosov
-     ! --------------------------------------------------------------------------------
-       subroutine get_thermal_roughness_kl(z0_t, B, &
-            z0_m, Re)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        ! ----------------------------------------------------------------------------
-
-         !--- define B = log(z0_m / z0_t)
-        if (Re <= Re_rough_min) then
-            B = B1_rough * alog(B3_rough * Re) + B2_rough
-        else
-            ! *: B4 takes into account Re value at z' ~ O(10) z0
-            B = B4_rough * (Re**B2_rough)
-        end if
-         
-            B = min(B, B_max_snow)
-       
-       z0_t = z0_m / exp(B)
-
-     end subroutine
-    
-        
-
-    ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Cahill, A.T., Parlange, M.B., Albertson, J.D., 1997.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_ca(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-3.8         !4-Cahill et al. 
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-    ! --------------------------------------------------------------------------------
-    ! thermal roughness definition z0_t = C*z0_m  
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_zm(z0_t, B, &
-            z0_m, Czm)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Czm                 !< proportionality coefficient
-        
-       
-
-        z0_t =Czm*z0_m
-        B=log(z0_m / z0_t)
-    end subroutine
-     ! --------------------------------------------------------------------------------
-     ! thermal roughness definition by Brutsaert W., 2003.
-    ! --------------------------------------------------------------------------------
-        subroutine get_thermal_roughness_br(z0_t, B, &
-            z0_m, Re)
-    ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-       
-       
-        
-        
-        B=2.46*(Re**0.25)-2.0       !Brutsaert
-       
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-   
-end module module_z0t_snow
diff --git a/srcF/sfx_thermal_roughness.f90 b/srcF/sfx_thermal_roughness.f90
deleted file mode 100644
index 04755f763e1c847fcaff4ec8b5d049086c3fee3e..0000000000000000000000000000000000000000
--- a/srcF/sfx_thermal_roughness.f90
+++ /dev/null
@@ -1,141 +0,0 @@
-module sfx_thermal_roughness
-    !< @brief surface thermal roughness parameterizations
-
-    ! modules used
-    ! --------------------------------------------------------------------------------
-    use sfx_phys_const
-    use sfx_surface
-    ! --------------------------------------------------------------------------------
-
-    ! directives list
-    ! --------------------------------------------------------------------------------
-    implicit none
-    ! --------------------------------------------------------------------------------
-
-    ! public interface
-    ! --------------------------------------------------------------------------------
-    public :: get_thermal_roughness_kl
-    public :: get_thermal_roughness_cz
-    public :: get_thermal_roughness_zi
-    public :: get_thermal_roughness_ca
-    ! --------------------------------------------------------------------------------
-
-    ! --------------------------------------------------------------------------------
-    real, parameter, private :: kappa = 0.40         !< von Karman constant [n/d]
-    ! --------------------------------------------------------------------------------
-
-contains
-
-
-    ! thermal roughness definition by (Kazakov, Lykosov)
-    ! --------------------------------------------------------------------------------
-    subroutine get_thermal_roughness_kl(z0_t, B, &
-            z0_m, Re, surface_type)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        integer, intent(in) :: surface_type     !< = [ocean] || [land] || [lake]
-        ! ----------------------------------------------------------------------------
-
-        ! --- local variables
-        ! ----------------------------------------------------------------------------
-
-        !--- define B = log(z0_m / z0_t)
-        if (Re <= Re_rough_min) then
-            B = B1_rough * alog(B3_rough * Re) + B2_rough
-        else
-            ! *: B4 takes into account Re value at z' ~ O(10) z0
-            B = B4_rough * (Re**B2_rough)
-        end if
-
-        ! --- apply max restriction based on surface type
-        if (surface_type == surface_ocean) then
-            B = min(B, B_max_ocean)
-        else if (surface_type == surface_lake) then
-            B = min(B, B_max_lake)
-        else if (surface_type == surface_land) then
-            B = min(B, B_max_land)
-        end if
-
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-
-    ! thermal roughness definition by (Chen, F., Zhang, Y., 2009)
-    ! --------------------------------------------------------------------------------
-    subroutine get_thermal_roughness_cz(z0_t, B, &
-            z0_m, Re, surface_type)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        integer, intent(in) :: surface_type     !< = [ocean] || [land] || [lake]
-
-        ! --- local variables
-        ! ----------------------------------------------------------------------------
-
-        !--- define B = log(z0_m / z0_t)
-        B = (kappa * 10.0**(-0.4 * z0_m / 0.07)) * (Re**0.45)
-
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-    
-    ! thermal roughness definition by (Zilitinkevich, S., 1995)
-    ! --------------------------------------------------------------------------------
-    subroutine get_thermal_roughness_zi(z0_t, B, &
-            z0_m, Re, surface_type)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        integer, intent(in) :: surface_type     !< = [ocean] || [land] || [lake]
-
-        ! --- local variables
-        ! ----------------------------------------------------------------------------
-
-        !--- define B = log(z0_m / z0_t)
-        B = 0.1 * kappa * (Re**0.5)
-
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-    
-    ! thermal roughness definition by (Cahill, A.T., Parlange, M.B., Albertson, J.D., 1997)
-    ! --------------------------------------------------------------------------------
-    subroutine get_thermal_roughness_ca(z0_t, B, &
-            z0_m, Re, surface_type)
-        ! ----------------------------------------------------------------------------
-        real, intent(out) :: z0_t               !< thermal roughness [m]
-        real, intent(out) :: B                  !< = log(z0_m / z0_t) [n/d]
-
-        real, intent(in) :: z0_m                !< aerodynamic roughness [m]
-        real, intent(in) :: Re                  !< roughness Reynolds number [n/d]
-        integer, intent(in) :: surface_type     !< = [ocean] || [land] || [lake]
-
-        ! --- local variables
-        ! ----------------------------------------------------------------------------
-
-        !--- define B = log(z0_m / z0_t)
-        B = 2.46 * (Re**0.25) - 3.8
-
-        ! --- define roughness [thermal]
-        z0_t = z0_m / exp(B)
-
-    end subroutine
-    ! --------------------------------------------------------------------------------
-
-end module sfx_thermal_roughness