Exemplo n.º 1
0
Arquivo: proc.c Projeto: ds2dev/gcc
unsigned
gomp_dynamic_max_threads (void)
{
  unsigned n_onln, loadavg, nthreads_var = gomp_icv (false)->nthreads_var;

  n_onln = get_num_procs ();
  if (n_onln > nthreads_var)
    n_onln = nthreads_var;

  loadavg = 0;
#ifdef HAVE_GETLOADAVG
  {
    double dloadavg[3];
    if (getloadavg (dloadavg, 3) == 3)
      {
	/* Add 0.1 to get a kind of biased rounding.  */
	loadavg = dloadavg[2] + 0.1;
      }
  }
#endif

  if (loadavg >= n_onln)
    return 1;
  else
    return n_onln - loadavg;
}
Exemplo n.º 2
0
int openblas_get_num_procs(void) {
#ifndef SMP
  return 1;
#else
  return get_num_procs();
#endif
}
Exemplo n.º 3
0
int blas_get_cpu_number(void){
  char *p;
#if defined(OS_LINUX) || defined(OS_WINDOWS) || defined(OS_FREEBSD) || defined(OS_DARWIN)
  int max_num;
#endif
  int blas_goto_num   = 0;
  int blas_omp_num    = 0;

  if (blas_num_threads) return blas_num_threads;

#if defined(OS_LINUX) || defined(OS_WINDOWS) || defined(OS_FREEBSD) || defined(OS_DARWIN)
  max_num = get_num_procs();
#endif

  blas_goto_num = 0;
#ifndef USE_OPENMP
  p = getenv("OPENBLAS_NUM_THREADS");
  if (p) blas_goto_num = atoi(p);
  if (blas_goto_num < 0) blas_goto_num = 0;

  if (blas_goto_num == 0) {
	    p = getenv("GOTO_NUM_THREADS");
		if (p) blas_goto_num = atoi(p);
		if (blas_goto_num < 0) blas_goto_num = 0;
  }
  
#endif

  blas_omp_num = 0;
  p = getenv("OMP_NUM_THREADS");
  if (p) blas_omp_num = atoi(p);
  if (blas_omp_num < 0) blas_omp_num = 0;

  if (blas_goto_num > 0) blas_num_threads = blas_goto_num;
  else if (blas_omp_num > 0) blas_num_threads = blas_omp_num;
  else blas_num_threads = MAX_CPU_NUMBER;

#if defined(OS_LINUX) || defined(OS_WINDOWS) || defined(OS_FREEBSD) || defined(OS_DARWIN)
  if (blas_num_threads > max_num) blas_num_threads = max_num;
#endif

  if (blas_num_threads > MAX_CPU_NUMBER) blas_num_threads = MAX_CPU_NUMBER;

#ifdef DEBUG
  printf( "Adjusted number of threads : %3d\n", blas_num_threads);
#endif
  
  blas_cpu_number = blas_num_threads;  

  return blas_num_threads;
}
Exemplo n.º 4
0
//                                   B C S
//##############################################################################
//
// Apply boundary conditions.
//
void bcs( lattice_ptr lattice)
{
  int    i, j, k, n, n1, a, id;
  int    ni, nj, nk;
  int    subs;
  double *ftemp, *f, *f1, *feq, *feq1, *rhoo, temp[Q];
  double  v, rho_in, rho_out, rho1;
  double  c0;
  double  D;
  double  c2;

#if RHO0_TEST
//------------------------------------------------------------------[ TEST ]----
  double *rho0;
//------------------------------------------------------------------[ TEST ]----
#endif /* RHO0_TEST */
  double u_x,  u_y, u_z, usq,udotx;
  double u_in[2][2],
         u_out[2][2],
         u,
         rho,
         hua;
  double c;

  ni = lattice->param.LX;
  nj = lattice->param.LY;
  nk = lattice->param.LZ;

  id = get_proc_id(lattice);

  // for( subs=0; subs<(NUM_FLUID_COMPONENTS)-(INAMURO_SIGMA_COMPONENT); subs++)
  for( subs=0; subs<NUM_FLUID_COMPONENTS; subs++)
  {
    // P R E S S U R E   T O P   I N F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // pressure top inflow
    //  -- Pressure boundary on top side using inflow pressure condition.
    if(   (id ==(get_num_procs(lattice)-1))
        && !lattice->param.GZL
        && lattice->param.pressure_t_in[subs] )
    {
      k = nk-1;
      switch(NUM_FLUID_COMPONENTS)
      {
        case 1:
        { rho_in = lattice->param.rho_in; break;}
        case 2:
        {
          if(subs==0) { rho_in = lattice->param.rho_in;}
          if(subs==1) { rho_in = lattice->param.rho_A[subs];}
          break;
        }
      }

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          ftemp = lattice->pdf[subs][n].ftemp;

          // Top, Inflow
          if( lattice->param.incompressible)
          {
            u_z = -rho_in
                + ( ftemp[ C]
                  + ftemp[ N] + ftemp[ S] + ftemp[ E] + ftemp[ W]
                  + 2.*( ftemp[T ]
                       + ftemp[TW] + ftemp[TE] + ftemp[TS] + ftemp[TN]));
            c = u_z;
          }
          else // compressible
          {
            u_z = -1.
                + ( ftemp[C]
                  + ftemp[N ] + ftemp[S ] + ftemp[ E] + ftemp[ W]
                  + ftemp[NE] + ftemp[NW] + ftemp[SE] + ftemp[SW]
                  + 2.*( ftemp[T ]
                       + ftemp[TW] + ftemp[TE] + ftemp[TS] + ftemp[TN]))
                / rho_in;
            c = u_z*rho_in;
          }
          //rev_Huang
          ftemp[B ] = ftemp[T ] - (1./3.)*c;
          ftemp[BW] = ftemp[TE] - (1./6.)*c
                    + 0.5*(-ftemp[ W] - ftemp[NW] - ftemp[SW]
                          + ftemp[ E] + ftemp[NE] + ftemp[SE]);
          ftemp[BE] = ftemp[TW] - (1./6.)*c
                    - 0.5*(-ftemp[ W] - ftemp[NW] - ftemp[SW]
                          + ftemp[ E] + ftemp[NE] + ftemp[SE]);
          ftemp[BS] = ftemp[TN] - (1./6.)*c
                    + 0.5*( ftemp[N ] + ftemp[NW] + ftemp[NE]
                          - ftemp[S ] - ftemp[SW] - ftemp[SE]);
          ftemp[BN] = ftemp[TS] - (1./6.)*c
                    - 0.5*( ftemp[N ] + ftemp[NW] + ftemp[NE]
                          - ftemp[S ] - ftemp[SW] - ftemp[SE]);
#if 1 // Confirm density
  rho = ftemp[ C]
      + ftemp[ E] + ftemp[ W]
      + ftemp[ N] + ftemp[ S]
      + ftemp[ T] + ftemp[ B]
      + ftemp[NE] + ftemp[NW] + ftemp[SE] + ftemp[SW]
      + ftemp[TN] + ftemp[TS] + ftemp[BN] + ftemp[BS]
      + ftemp[TE] + ftemp[TW] + ftemp[BE] + ftemp[BW];
  if( rho_in - rho > 1e-6)
  {
    printf("%s %d >> ERROR: pressure_top_in FAIL! "
           "rho_in = %f, rho = %f\n",__FILE__,__LINE__, rho_in, rho);
  }
#endif

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.pressure_t_in[subs] ) */


    //********************************************************************************


    // P R E S S U R E   B O T T O M   O U T F L O W   B C  (peter's attempt?)
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // pressure bottom outflow
    //  -- Pressure boundary on bottom side using outflow pressure condition.

    if((id ==0) && !lattice->param.GZL && lattice->param.pressure_b_out[subs] )
    {
      k = 0;

      switch(NUM_FLUID_COMPONENTS)
      {
        case 1:
        {  rho_out = lattice->param.rho_out; break; }
        case 2:
        {
          if(subs==0) { rho_out = lattice->param.rho_out;}
          if(subs==1) { rho_out = lattice->param.rho_A[subs];}
          break;
        }
      }

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          ftemp = lattice->pdf[subs][n].ftemp;

          // Bottom, rho_out
          if( lattice->param.incompressible)
          {
            u_z = rho_out
              - ( ftemp[C]
                + ftemp[N] + ftemp[S] + ftemp[E] + ftemp[W]
                + 2.*( ftemp[B]
                     + ftemp[BW] + ftemp[BE] + ftemp[BS] + ftemp[BN]));
            c = u_z;
          }
          else // compressible
          {
            u_z =  1.
              - ( ftemp[C]
                + ftemp[N ] + ftemp[S ] + ftemp[ E] + ftemp[ W]
                + ftemp[NW] + ftemp[NE] + ftemp[SW] + ftemp[SE]
                + 2.*( ftemp[B ]
                     + ftemp[BW] + ftemp[BE] + ftemp[BS] + ftemp[BN]))
              / rho_out;
            c = u_z*rho_out;
          }

          ftemp[T ] = ftemp[B ] + (1./3.)*c;
          ftemp[TW] = ftemp[BE] + (1./6.)*c
                    + 0.5*(-ftemp[ W] - ftemp[NW] - ftemp[SW]
                          + ftemp[ E] + ftemp[NE] + ftemp[SE]);
          ftemp[TE] = ftemp[BW] + (1./6.)*c
                    - 0.5*(-ftemp[ W] - ftemp[NW] - ftemp[SW]
                          + ftemp[ E] + ftemp[NE] + ftemp[SE]);
          ftemp[TS] = ftemp[BN] + (1./6.)*c
                    + 0.5*( ftemp[N ] + ftemp[NW] + ftemp[NE]
                          - ftemp[S ] - ftemp[SW] - ftemp[SE]);
          ftemp[TN] = ftemp[BS] + (1./6.)*c
                    - 0.5*( ftemp[N ] + ftemp[NW] + ftemp[NE]
                          - ftemp[S ] - ftemp[SW] - ftemp[SE]);

#if 1 // Confirm density
  rho = ftemp[ C]
      + ftemp[ E] + ftemp[ W]
      + ftemp[ N] + ftemp[ S]
      + ftemp[ T] + ftemp[ B]
      + ftemp[NE] + ftemp[NW] + ftemp[SE] + ftemp[SW]
      + ftemp[TN] + ftemp[TS] + ftemp[BN] + ftemp[BS]
      + ftemp[TE] + ftemp[TW] + ftemp[BE] + ftemp[BW];
  if( rho_out - rho > 1e-6)
  {
    printf("%s %d >> ERROR: pressure_bottom_out FAIL! "
           "rho_out = %f, rho = %f\n",__FILE__,__LINE__, rho_out, rho);
  }
#endif

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.pressure_b_out[subs] ) */


    //********************************************************************************
    // V E L O C I T Y   T O P   I N F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // velocity top inflow
    //  -- Velocity boundary on top side using inflow velocity condition.
    if( id == get_num_procs( lattice) - 1 && !lattice->param.GZL && 
												lattice->param.velocity_t_in[subs])
    {

		//printf("%s %d >> BOOM!",__FILE__,__LINE__);
      if(subs==0) u = lattice->param.uz_in;    //lattice->param.uz_in; Non-wetting
      if(subs==1) u = lattice->param.uz_in;    //lattice->param.uz_in;

      k = nk-1;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          ftemp = lattice->pdf[subs][n].ftemp;

          if( !lattice->solids[subs][n].is_solid)
          {
            rho = ( ftemp[C ]
                + ftemp[W ] + ftemp[E ] + ftemp[N ] + ftemp[S ]
                + ftemp[NW] + ftemp[NE] + ftemp[SW] + ftemp[SE]
                + 2.*( ftemp[T ]
                  + ftemp[TW] + ftemp[TE] + ftemp[TS] + ftemp[TN])
                )
              / ( 1. + u);
            c = rho*u;

            ftemp[B ] = ftemp[T ] - (1./3.)*c;
            ftemp[BW] = ftemp[TE] - (1./6.)*c + 0.5* (-ftemp[W ]- ftemp[NW]- ftemp[SW]
                + ftemp[E] +ftemp[NE] + ftemp[SE]);
            ftemp[BE] = ftemp[TW] - (1./6.)*c - 0.5* (-ftemp[W ]- ftemp[NW]- ftemp[SW]
                + ftemp[E] +ftemp[NE] + ftemp[SE]);
            ftemp[BS] = ftemp[TN] - (1./6.)*c + 0.5* (ftemp[N ] + ftemp[NW] + ftemp[NE]
                -ftemp[S ] -ftemp[SW] - ftemp[SE]);
            ftemp[BN] = ftemp[TS] - (1./6.)*c - 0.5* (ftemp[N ] + ftemp[NW] + ftemp[NE]
                -ftemp[S ] -ftemp[SW] - ftemp[SE]);

          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_t_in[subs]) */

    // V E L O C I T Y   B O T T O M   O U T F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // velocity bottom inflow
    //  -- Velocity boundary on bottom side using outflow velocity condition.
    if( id == 0 && !lattice->param.GZL && lattice->param.velocity_b_out[subs])
    {
//printf("%s %d >> BOOM!",__FILE__,__LINE__);
      if(subs==0) u = lattice->param.uz_out;    //lattice->param.uz_out;  Non-wetting
      if(subs==1) u = lattice->param.uz_out;    //lattice->param.uz_out;

      k = 0;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          ftemp = lattice->pdf[subs][n].ftemp;

          if( !lattice->solids[subs][n].is_solid)
          {
            rho = ( ftemp[C ]
                + ftemp[W ] + ftemp[E ] + ftemp[N ] + ftemp[S ]
                + ftemp[NW] + ftemp[NE] + ftemp[SW] + ftemp[SE]
                + 2.*( ftemp[B ]
                  + ftemp[BW] + ftemp[BE] + ftemp[BS] + ftemp[BN])
                )
              / ( 1. - u);
            c = rho*u;


            ftemp[T ] = ftemp[B ] + (1./3.)*c;
            ftemp[TW] = ftemp[BE] + (1./6.)*c + 0.5* (-ftemp[W ]- ftemp[NW]- ftemp[SW]
                + ftemp[E] +ftemp[NE] + ftemp[SE]);
            ftemp[TE] = ftemp[BW] + (1./6.)*c - 0.5* (-ftemp[W ]- ftemp[NW]- ftemp[SW]
                + ftemp[E] +ftemp[NE] + ftemp[SE]);
            ftemp[TS] = ftemp[BN] + (1./6.)*c  + 0.5* (ftemp[N ] + ftemp[NW] + ftemp[NE]
                -ftemp[S ] -ftemp[SW] - ftemp[SE]);
            ftemp[TN] = ftemp[BS] + (1./6.)*c  - 0.5* (ftemp[N ] + ftemp[NW] + ftemp[NE]
                -ftemp[S ] -ftemp[SW] - ftemp[SE]);


          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_b_in[subs]) */

    //********************************************************************************


    // GZL P R E S S U R E // V E L O C I T Y   T O P   I N F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    //  -- Velocity boundary on top side using inflow velocity condition.
#if PARALLEL
    id = get_proc_id(lattice);
#else
    id = get_num_procs(lattice)-1;
#endif

    if( (id ==get_num_procs(lattice)-1) && lattice->param.GZL && lattice->param.PressureBC)//lattice->param.velocity_t_in[subs])
    {
printf("%s %d >> BOOM!",__FILE__,__LINE__);
      k = nk-1;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          f = lattice->pdf[subs][n].f;

#if STORE_UEQ
          //       u_x = &lattice->ueq[n].u[0] = 0.02;
          //       lattice->ueq[n].u[1] = 0.;
          //       lattice->ueq[n].u[2] = 0.;
#else /* !( STORE_UEQ) */
          //       lattice->macro_vars[subs][n].u[0] =  0.02 ;
          //       lattice->macro_vars[subs][n].u[1] =  0. ;
          //       lattice->macro_vars[subs][n].u[2] =  0. ;
#endif /* STORE_UEQ */

          n1 = XYZ2N( i, j, k-1, ni, nj);
          f1 = lattice->pdf[subs][n1].f;
          feq1 = lattice->pdf[subs][n1].feq;

          //  rhoo = &( lattice->macro_vars[subs][n].rho);
          switch(NUM_FLUID_COMPONENTS)
          {case 1:
            {
              rho =  /*lattice->macro_vars[subs][n1].rho;*/lattice->param.rho_in;
              u_x =  0.;//lattice->macro_vars[subs][n1].u[0] ;
              u_y =  0.;//lattice->macro_vars[subs][n1].u[1] ;
              u_z =  lattice->macro_vars[subs][n1].u[2] ;
              lattice->macro_vars[subs][n].u[2] = u_z;
              break;
            }
            case 2:
            {
#if STORE_UEQ
              if(subs==0)
              {
                rho =lattice->param.rho_in;// 8+ 0.001*(double)lattice->time;// ;    subs= 0 Non-wetting
                if( lattice->time >1000)  {rho = lattice->param.rho_in;}
              }
              if(subs==1) rho = 0.000 ;    //lattice->param.uz_in; subs= 1 Wetting

              //          rho =  lattice->param.rho_A[subs];
              u_x =  0.;// lattice->ueq[n1].u[0] ;
              u_y =  0.;// lattice->ueq[n1].u[1] ;
              u_z =  lattice->ueq[n1].u[2] ;
              lattice->macro_vars[subs][n].u[2] = u_z;
              lattice->ueq[n].u[2] = u_z;

#endif
              break;
            }
          }
          lattice->macro_vars[subs][n].rho = rho;
          lattice->macro_vars[subs][n].u[0] = u_x;
          lattice->macro_vars[subs][n].u[1] = u_y;


          if( !lattice->solids[subs][n].is_solid)
          {
            compute_a_feq( feq, rho, u_x, u_y, u_z );

            for (a= 0; a<Q; a++)
            {
              temp[a] =  f1[a] - feq1[a];
              f[a]=feq[a]+ temp[a];
            }


          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_GZL) */

    //GZL P R E S S U R E // V E L O C I T Y   B O T T O M   O U T F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // velocity bottom inflow
    //  -- Velocity boundary on bottom side using inflow velocity condition.
#if PARALLEL
    id = get_proc_id(lattice);
#else
    id = 0;
#endif
    if( (id ==0) && lattice->param.GZL && lattice->param.PressureBC)//lattice->param.velocity_b_in[subs])
    {
printf("%s %d >> BOOM!",__FILE__,__LINE__);
      k = 0;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          f = lattice->pdf[subs][n].f;

          n1 = XYZ2N( i, j, k+1, ni, nj);
          f1   = lattice->pdf[subs][n1].f;
          feq1 = lattice->pdf[subs][n1].feq;

          switch(NUM_FLUID_COMPONENTS)
          {case 1:
            {
              rho =  /*lattice->macro_vars[subs][n1].rho;*/lattice->param.rho_out;
              u_x =  0.;//lattice->macro_vars[subs][n1].u[0] ;
              u_y =  0.;//lattice->macro_vars[subs][n1].u[1] ;
              u_z =  lattice->macro_vars[subs][n1].u[2] ;
              lattice->macro_vars[subs][n].u[2] = u_z;
              break;
            }
            case 2:
            {
#if STORE_UEQ
              if(subs==0) rho = 0.000;
              if(subs==1)
              {
                rho =lattice->param.rho_out; //8.0- 0.001*(double)lattice->time;//
                if( lattice->time >6000)   {rho = lattice->param.rho_out;}
              }
              //          rho =  lattice->param.rho_B[subs];
              u_x =  0.;//lattice->ueq[n1].u[0] ;
              u_y =  0.;//lattice->ueq[n1].u[1] ;
              u_z =  lattice->ueq[n1].u[2] ;
              lattice->macro_vars[subs][n].u[2] = u_z;
              lattice->ueq[n].u[2] = u_z;
#endif
              break;
            }
          }
          lattice->macro_vars[subs][n].rho = rho;
          lattice->macro_vars[subs][n].u[0] = u_x;
          lattice->macro_vars[subs][n].u[1] = u_y;



          if( !lattice->solids[subs][n].is_solid)
          {
            compute_a_feq( feq, rho, u_x, u_y, u_z );

            for (a= 0; a<Q; a++)
            {
              temp[a] =f1[a] - feq1[a];
              f[a] =  feq[a]+ temp[a];
            }

          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_GZL) */



    //PAN   V E L O C I T Y   T O P   I N F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    //  -- Velocity boundary on top side using inflow velocity condition.
    if( lattice->param.GZL && (!lattice->param.PressureBC))//lattice->param.velocity_t_in[subs])
    {
printf("%s %d >> BOOM!",__FILE__,__LINE__);
      k = nk-1;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          f = lattice->pdf[subs][n].f;
          //  feq =  lattice->pdf[subs][n].feq;


          n1 = XYZ2N( i, j, k-1, ni, nj);
          f1 = lattice->pdf[subs][n1].f;
          feq1 = lattice->pdf[subs][n1].feq;

          rhoo = &( lattice->macro_vars[subs][n].rho);
          switch(NUM_FLUID_COMPONENTS)
          {case 1:
            {
              rho =  /*lattice->macro_vars[subs][n1].rho;*/lattice->param.rho_in;
              u_x =  0.;//lattice->macro_vars[subs][n1].u[0] ;
              u_y =  0.;//lattice->macro_vars[subs][n1].u[1] ;
              u_z =  -0.0;//lattice->macro_vars[subs][n1].u[2] ;
              break;
            }
            case 2:
            {
#if STORE_UEQ
              rho    =  lattice->param.rho_A[subs];
              u_x = 0.;// lattice->ueq[n1].u[0] ;
              u_y = 0.;// lattice->ueq[n1].u[1] ;
              u_z = 0.;// lattice->ueq[n1].u[2] ;
#endif
              break;
            }
          }
          lattice->macro_vars[subs][n].rho = rho;
          lattice->macro_vars[subs][n].u[0] = u_x;
          lattice->macro_vars[subs][n].u[1] = u_y;
          lattice->macro_vars[subs][n].u[2] = u_z;


          if( !lattice->solids[subs][n].is_solid)
          {
            compute_a_feq( feq, rho, u_x, u_y, u_z );

            for (a= 0; a<Q; a++)
            {f[a] = feq[a];}//+(f1[a] - feq1[a]);


          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_GZL) */

    //PAN V E L O C I T Y   B O T T O M   I N F L O W   B C
    //- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
    // velocity bottom inflow
    //  -- Velocity boundary on bottom side using inflow velocity condition.
    if(  lattice->param.GZL && (!lattice->param.PressureBC))//lattice->param.velocity_b_in[subs])
    {
printf("%s %d >> BOOM!",__FILE__,__LINE__);
      k = 0;

      for( j=0; j<nj; j++)
      {
        for( i=0; i<ni; i++)
        {
          n = XYZ2N( i, j, k, ni, nj);
          f = lattice->pdf[subs][n].f;
          //  feq =  lattice->pdf[subs][n].feq;

          n1 = XYZ2N( i, j, k+1, ni, nj);
          f1 = lattice->pdf[subs][n1].f;
          feq1 = lattice->pdf[subs][n1].feq;


          switch(NUM_FLUID_COMPONENTS)
          {case 1:
            {
              rho =  /*lattice->macro_vars[subs][n1].rho;*/lattice->param.rho_out;
              u_x =  0.;//lattice->macro_vars[subs][n1].u[0] ;
              u_y =  0.;//lattice->macro_vars[subs][n1].u[1] ;
              u_z =  -0.0;//lattice->macro_vars[subs][n1].u[2] ;
              break;
            }
            case 2:
            {
#if STORE_UEQ
              rho =  lattice->param.rho_B[subs];
              u_x =  0.;//lattice->ueq[n1].u[0] ;
              u_y =  0.;//lattice->ueq[n1].u[1] ;
              u_z =  0.;//lattice->ueq[n1].u[2] ;
#endif
              break;
            }
          }

          lattice->macro_vars[subs][n].rho = rho;
          lattice->macro_vars[subs][n].u[0] = u_x;
          lattice->macro_vars[subs][n].u[1] = u_y;
          lattice->macro_vars[subs][n].u[2] = u_z;

          if( !lattice->solids[subs][n].is_solid)
          {
            compute_a_feq( feq, rho, u_x, u_y, u_z );
            if(subs==1)
              compute_a_feq( feq1, 2.0- 0.0003*(double)lattice->time, u_x, u_y, u_z );

            for (a= 0; a<Q; a++)
            {
              f[a] = feq[a];

            }// +(f1[a] - feq1[a]);

          } /* if( !is_solid) */

        } /* for( i=0; i<ni; i++) */
      } /* for( j=0; j<nj; j++) */

    } /* if( lattice->param.velocity_GZL) */


  } /* for( subs=0; subs<(NUM_FLUID_COMPONENTS)-(INAMURO_SIGMA_COMPONENT); subs++) */

}
Exemplo n.º 5
0
 inline controller::controller() : chains(&stack_m), mirror(&stack_s), clock(1) {
     this->each = new node_each(this);
     this->which = NULL;
     for(int i = 0; i < get_num_procs(); i++) nodes.push_back(i);
     if(!verbose()) this->io_guard.enable();
 }
Exemplo n.º 6
0
Arquivo: proc.c Projeto: ds2dev/gcc
int
omp_get_num_procs (void)
{
  return get_num_procs ();
}