Skip to content
Snippets Groups Projects
Commit a1b737d5 authored by 数学の武士's avatar 数学の武士
Browse files

Remove unnecessary files

parent 57f905b5
No related branches found
No related tags found
No related merge requests found
Hide whitespace changes
Inline Side-by-side
includeCXX/sfx_compute_sheba.h deleted 100644 → 0
+ 0
− 17
View file @ 57f905b5
#pragma once
template<typename T>
void compute_flux_sheba_cpu(T *zeta_, T *Rib_, T *Re_, T *B_, T *z0_m_, T *z0_t_, T *Rib_conv_lim_, T *Cm_, T *Ct_, T *Km_, T *Pr_t_inv_,
const T *U_, const T *dT_, const T *Tsemi_, const T *dQ_, const T *h_, const T *in_z0_m_,
const T kappa, const T Pr_t_0_inv,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h,
const T Re_rough_min,
const T B1_rough, const T B2_rough,
const T B_max_land, const T B_max_ocean, const T B_max_lake,
const T gamma_c, const T Re_visc_min,
const T Pr_m, const T nu_air, const T g,
const int maxiters_charnock,
const int grid_size);
\ No newline at end of file
srcCXX/sfx_compute_sheba.cpp deleted 100644 → 0
+ 0
− 325
View file @ 57f905b5
#include <cmath>
#include <iostream>
#include "../includeCXX/sfx_compute_sheba.h"
// #include "../includeCXX/sfx_surface.h"
template<typename T>
void get_psi_mh(T &psi_m, T &psi_h,
const T zeta_m, const T zeta_h,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h)
{
T x_m, x_h;
T q_m, q_h;
if (zeta_m >= 0.0)
{
q_m = pow((1.0 - b_m) / b_m, 1.0 / 3.0);
x_m = pow(1.0 + zeta_m, 1.0 / 3.0);
psi_m = -3.0 * (a_m / b_m) * (x_m - 1.0) + 0.5 * (a_m / b_m) * q_m * (2.0 * log((x_m + q_m) / (1.0 + q_m)) - log((x_m * x_m - x_m * q_m + q_m * q_m) / (1.0 - q_m + q_m * q_m)) + 2.0 * sqrt(3.0) * (atan((2.0 * x_m - q_m) / (sqrt(3.0) * q_m)) - atan((2.0 - q_m) / (sqrt(3.0) * q_m))));
}
else
{ x_m = pow(1.0 - alpha_m * zeta_m, 0.25);
psi_m = (4.0 * atan(1.0) / 2.0) + 2.0 * log(0.5 * (1.0 + x_m)) + log(0.5 * (1.0 + x_m * x_m)) - 2.0 * atan(x_m);
}
if (zeta_h >= 0.0)
{
q_h = sqrt(c_h * c_h - 4.0);
x_h = zeta_h;
psi_h = -0.5 * b_h * log(1.0 + c_h * x_h + x_h * x_h) + ((-a_h / q_h) + ((b_h * c_h) / (2.0 * q_h))) * (log((2.0 * x_h + c_h - q_h) / (2.0 * x_h + c_h + q_h)) - log((c_h - q_h) / (c_h + q_h)));
}
else
{
x_h = pow(1.0 - alpha_h * zeta_h, 0.25);
psi_h = 2.0 * log(0.5 * (1.0 + x_h * x_h));
}
}
template void get_psi_mh(float &psi_m, float &psi_h,
const float zeta_m, const float zeta_h,
const float alpha_m, const float alpha_h,
const float a_m, const float a_h,
const float b_m, const float b_h,
const float c_h);
template void get_psi_mh(double &psi_m, double &psi_h,
const double zeta_m, const double zeta_h,
const double alpha_m, const double alpha_h,
const double a_m, const double a_h,
const double b_m, const double b_h,
const double c_h);
template<typename T>
void get_psi(T &psi_m, T &psi_h,
const T zeta,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h)
{
T x_m, x_h;
T q_m, q_h;
if (zeta >= 0.0)
{
q_m = pow((1.0 - b_m) / b_m, 1.0 / 3.0);
q_h = sqrt(c_h * c_h - 4.0);
x_m = pow(1.0 + zeta, 1.0 / 3.0);
x_h = zeta;
psi_m = -3.0 * (a_m / b_m) * (x_m - 1.0) + 0.5 * (a_m / b_m) * q_m * (2.0 * log((x_m + q_m) / (1.0 + q_m)) - log((x_m * x_m - x_m * q_m + q_m * q_m) / (1.0 - q_m + q_m * q_m)) + 2.0 * sqrt(3.0) * (atan((2.0 * x_m - q_m) / (sqrt(3.0) * q_m)) - atan((2.0 - q_m) / (sqrt(3.0) * q_m))));
psi_h = -0.5 * b_h * log(1.0 + c_h * x_h + x_h * x_h) + ((-a_h / q_h) + ((b_h * c_h) / (2.0 * q_h))) * (log((2.0 * x_h + c_h - q_h) / (2.0 * x_h + c_h + q_h)) - log((c_h - q_h) / (c_h + q_h)));
}
else
{
x_m = pow(1.0 - alpha_m * zeta, 0.25);
x_h = pow(1.0 - alpha_h * zeta, 0.25);
psi_m = (4.0 * atan(1.0) / 2.0) + 2.0 * log(0.5 * (1.0 + x_m)) + log(0.5 * (1.0 + x_m * x_m)) - 2.0 * atan(x_m);
psi_h = 2.0 * log(0.5 * (1.0 + x_h * x_h));
}
}
template void get_psi(float &psi_m, float &psi_h,
const float zeta,
const float alpha_m, const float alpha_h,
const float a_m, const float a_h,
const float b_m, const float b_h,
const float c_h);
template void get_psi(double &psi_m, double &psi_h,
const double zeta,
const double alpha_m, const double alpha_h,
const double a_m, const double a_h,
const double b_m, const double b_h,
const double c_h);
template<typename T>
void get_dynamic_scales(T &Udyn, T &Tdyn, T &Qdyn, T &zeta,
const T U, const T Tsemi, const T dT, const T dQ, const T z, const T z0_m, const T z0_t, const T beta,
const T kappa, const T Pr_t_0_inv,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h,
const int maxiters)
{
T psi_m, psi_h, psi0_m, psi0_h, Linv;
const T gamma = 0.61;
Udyn = kappa * U / log(z / z0_m);
Tdyn = kappa * dT * Pr_t_0_inv / log(z / z0_t);
Qdyn = kappa * dQ * Pr_t_0_inv / log(z / z0_t);
zeta = 0.0;
// --- no wind
if (Udyn < 1e-5)
return;
Linv = kappa * beta * (Tdyn + gamma * Qdyn * Tsemi) / (Udyn * Udyn);
zeta = z * Linv;
// --- near neutral case
if (Linv < 1e-5)
return;
for (int i = 0; i < maxiters; i++)
{
get_psi(psi_m, psi_h, zeta, alpha_m, alpha_h,
a_m, a_h,
b_m, b_h,
c_h);
get_psi_mh(psi0_m, psi0_h, z0_m * Linv, z0_t * Linv,
alpha_m, alpha_h,
a_m, a_h,
b_m, b_h,
c_h);
Udyn = kappa * U / (log(z / z0_m) - (psi_m - psi0_m));
Tdyn = kappa * dT * Pr_t_0_inv / (log(z / z0_t) - (psi_h - psi0_h));
Qdyn = kappa * dQ * Pr_t_0_inv / (log(z / z0_t) - (psi_h - psi0_h));
if (Udyn < 1e-5)
break;
Linv = kappa * beta * (Tdyn + gamma * Qdyn * Tsemi) / (Udyn * Udyn);
zeta = z * Linv;
}
}
template void get_dynamic_scales(float &Udyn, float &Tdyn, float &Qdyn, float & zeta,
const float U, const float Tsemi, const float dT, const float dQ, const float z, const float z0_m, const float z0_t, const float beta,
const float kappa, const float Pr_t_0_inv,
const float alpha_m, const float alpha_h,
const float a_m, const float a_h,
const float b_m, const float b_h,
const float c_h,
const int maxiters);
template void get_dynamic_scales(double &Udyn, double &Tdyn, double &Qdyn, double & zeta,
const double U, const double Tsemi, const double dT, const double dQ, const double z, const double z0_m, const double z0_t, const double beta,
const double kappa, const double Pr_t_0_inv,
const double alpha_m, const double alpha_h,
const double a_m, const double a_h,
const double b_m, const double b_h,
const double c_h,
const int maxiters);
template<typename T>
void get_phi(T &phi_m, T &phi_h,
const T zeta,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h)
{
if (zeta >= 0.0)
{
phi_m = 1.0 + (a_m * zeta * pow(1.0 + zeta, 1.0 / 3.0) ) / (1.0 + b_m * zeta);
phi_h = 1.0 + (a_h * zeta + b_h * zeta * zeta) / (1.0 + c_h * zeta + zeta * zeta);
}
else
{
phi_m = pow(1.0 - alpha_m * zeta, -0.25);
phi_h = pow(1.0 - alpha_h * zeta, -0.5);
}
}
template void get_phi(float &phi_m, float &phi_h,
const float zeta,
const float alpha_m, const float alpha_h,
const float a_m, const float a_h,
const float b_m, const float b_h,
const float c_h);
template void get_phi(double &phi_m, double &phi_h,
const double zeta,
const double alpha_m, const double alpha_h,
const double a_m, const double a_h,
const double b_m, const double b_h,
const double c_h);
template<typename T>
void compute_flux_sheba_cpu(T *zeta_, T *Rib_, T *Re_, T *B_, T *z0_m_, T *z0_t_, T *Rib_conv_lim_, T *Cm_, T *Ct_, T *Km_, T *Pr_t_inv_,
const T *U_, const T *dT_, const T *Tsemi_, const T *dQ_, const T *h_, const T *in_z0_m_,
const T kappa, const T Pr_t_0_inv,
const T alpha_m, const T alpha_h,
const T a_m, const T a_h,
const T b_m, const T b_h,
const T c_h,
const T Re_rough_min,
const T B1_rough, const T B2_rough,
const T B_max_land, const T B_max_ocean, const T B_max_lake,
const T gamma_c, const T Re_visc_min,
const T Pr_m, const T nu_air, const T g,
const int maxiters_charnock,
const int grid_size)
{
// T h, U, dT, Tsemi, dQ, z0_m;
// T z0_t, B, h0_m, h0_t, u_dyn0, Re,
// zeta, Rib, Udyn, Tdyn, Qdyn, phi_m, phi_h,
// Km, Pr_t_inv, Cm, Ct;
// const T B3_rough = kappa * Pr_m, B4_rough =(0.14 * (pow(30.0, B2_rough))) * (pow(Pr_m, 0.8));
// const T h_charnock = 10.0, c1_charnock = log(h_charnock * (g / gamma_c)), c2_charnock = Re_visc_min * nu_air * c1_charnock;
// int surface_type;
// for (int step = 0; step < grid_size; step++)
// {
// U = U_[step];
// Tsemi = Tsemi_[step];
// dT = dT_[step];
// dQ = dQ_[step];
// h = h_[step];
// z0_m = in_z0_m_[step];
// if (z0_m < 0.0) surface_type = 0;
// else surface_type = 1;
// if (surface_type == 0)
// {
// get_charnock_roughness(z0_m, u_dyn0, h, U, kappa, h_charnock, c1_charnock, c2_charnock, maxiters_charnock);
// h0_m = h / z0_m;
// }
// if (surface_type == 1)
// {
// h0_m = h / z0_m;
// u_dyn0 = U * kappa / log(h0_m);
// }
// Re = u_dyn0 * z0_m / nu_air;
// get_thermal_roughness(z0_t, B, z0_m, Re, Re_rough_min, B1_rough, B2_rough, B3_rough, B4_rough, B_max_ocean, B_max_lake, B_max_land, surface_type);
// // --- define relative height [thermal]
// h0_t = h / z0_t;
// // --- define Ri-bulk
// Rib = (g / Tsemi) * h * (dT + 0.61e0 * Tsemi * dQ) / (U*U);
// // --- get the fluxes
// // ----------------------------------------------------------------------------
// get_dynamic_scales(Udyn, Tdyn, Qdyn, zeta, U, Tsemi, dT, dQ, h, z0_m, z0_t, (g / Tsemi), kappa, Pr_t_0_inv, alpha_m, alpha_h, a_m, a_h, b_m, b_h, c_h, 10);
// // ----------------------------------------------------------------------------
// get_phi(phi_m, phi_h, zeta, alpha_m, alpha_h, a_m, a_h, b_m, b_h, c_h);
// // ----------------------------------------------------------------------------
// // --- define transfer coeff. (momentum) & (heat)
// Cm = 0.0;
// if (U > 0.0)
// Cm = Udyn / U;
// Ct = 0.0;
// if (fabs(dT) > 0.0)
// Ct = Tdyn / dT;
// // --- define eddy viscosity & inverse Prandtl number
// Km = kappa * Cm * U * h / phi_m;
// Pr_t_inv = phi_m / phi_h;
// zeta_[step] = zeta;
// Rib_[step] = Rib;
// Re_[step] = Re;
// B_[step] = B;
// z0_m_[step] = z0_m;
// z0_t_[step] = z0_t;
// Rib_conv_lim_[step] = 0.0;
// Cm_[step] = Cm;
// Ct_[step] = Ct;
// Km_[step] = Km;
// Pr_t_inv_[step] = Pr_t_inv;
// }
}
template void compute_flux_sheba_cpu(float *zeta_, float *Rib_, float *Re_, float *B_, float *z0_m_, float *z0_t_, float *Rib_conv_lim_, float *Cm_, float *Ct_, float *Km_, float *Pr_t_inv_,
const float *U, const float *dt, const float *T_semi, const float *dq, const float *H, const float *in_z0_m,
const float kappa, const float Pr_t_0_inv,
const float alpha_m, const float alpha_h,
const float a_m, const float a_h,
const float b_m, const float b_h,
const float c_h,
const float Re_rough_min,
const float B1_rough, const float B2_rough,
const float B_max_land, const float B_max_ocean, const float B_max_lake,
const float gamma_c, const float Re_visc_min,
const float Pr_m, const float nu_air, const float g,
const int maxiters_charnock,
const int grid_size);
template void compute_flux_sheba_cpu(double *zeta_, double *Rib_, double *Re_, double *B_, double *z0_m_, double *z0_t_, double *Rib_conv_lim_, double *Cm_, double *Ct_, double *Km_, double *Pr_t_inv_,
const double *U, const double *dt, const double *T_semi, const double *dq, const double *H, const double *in_z0_m,
const double kappa, const double Pr_t_0_inv,
const double alpha_m, const double alpha_h,
const double a_m, const double a_h,
const double b_m, const double b_h,
const double c_h,
const double Re_rough_min,
const double B1_rough, const double B2_rough,
const double B_max_land, const double B_max_ocean, const double B_max_lake,
const double gamma_c, const double Re_visc_min,
const double Pr_m, const double nu_air, const double g,
const int maxiters_charnock,
const int grid_size);
\ No newline at end of file
0% or .
You are about to add 0 people to the discussion. Proceed with caution.
Finish editing this message first!
Please register or to comment