13#include <camp/aero_phase_solver.h>
14#include <camp/aero_reps.h>
15#include <camp/camp_solver.h>
18#define TEMPERATURE_K_ env_data[0]
19#define PRESSURE_PA_ env_data[1]
21#define UPDATE_NUMBER 0
23#define NUM_LAYERS_ int_data[0]
24#define AERO_REP_ID_ int_data[1]
25#define MAX_PARTICLES_ int_data[2]
26#define PARTICLE_STATE_SIZE_ int_data[3]
27#define NUMBER_CONC_(x) aero_rep_env_data[x]
28#define NUM_INT_PROP_ 4
29#define NUM_FLOAT_PROP_ 0
30#define NUM_ENV_PARAM_ MAX_PARTICLES_
31#define LAYER_PHASE_START_(l) (int_data[NUM_INT_PROP_+l]-1)
32#define LAYER_PHASE_END_(l) (int_data[NUM_INT_PROP_+NUM_LAYERS_+l]-1)
33#define TOTAL_NUM_PHASES_ (LAYER_PHASE_END_(NUM_LAYERS_-1)-LAYER_PHASE_START_(0)+1)
34#define NUM_PHASES_(l) (LAYER_PHASE_END_(l)-LAYER_PHASE_START_(l)+1)
35#define PHASE_STATE_ID_(l,p) (int_data[NUM_INT_PROP_+2*NUM_LAYERS_+LAYER_PHASE_START_(l)+p]-1)
36#define PHASE_MODEL_DATA_ID_(l,p) (int_data[NUM_INT_PROP_+2*NUM_LAYERS_+TOTAL_NUM_PHASES_+LAYER_PHASE_START_(l)+p]-1)
37#define PHASE_NUM_JAC_ELEM_(l,p) int_data[NUM_INT_PROP_+2*NUM_LAYERS_+2*TOTAL_NUM_PHASES_+LAYER_PHASE_START_(l)+p]
54 int *aero_rep_int_data,
55 double *aero_rep_float_data,
57 int *int_data = aero_rep_int_data;
58 double *float_data = aero_rep_float_data;
64 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
65 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
87 double *aero_rep_float_data,
89 int *int_data = aero_rep_int_data;
90 double *float_data = aero_rep_float_data;
109 int *aero_rep_int_data,
110 double *aero_rep_float_data,
111 double *aero_rep_env_data) {
112 int *int_data = aero_rep_int_data;
113 double *float_data = aero_rep_float_data;
114 double *env_data = model_data->grid_cell_env;
130 int *aero_rep_int_data,
131 double *aero_rep_float_data,
132 double *aero_rep_env_data) {
133 int *int_data = aero_rep_int_data;
134 double *float_data = aero_rep_float_data;
154 ModelData *model_data,
int aero_phase_idx,
double *layer_radius,
155 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
156 double *aero_rep_env_data) {
158 int *int_data = aero_rep_int_data;
159 double *float_data = aero_rep_float_data;
161 double *curr_partial = NULL;
162 int aero_phase_idx_temp = aero_phase_idx;
165 int i_layer_radius = -1;
166 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
169 i_layer_radius = i_layer;
175 if (partial_deriv) curr_partial = partial_deriv;
176 for (
int i_layer = 0; i_layer <= i_layer_radius; ++i_layer) {
177 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
178 double *state = (
double *)(model_data->grid_cell_state);
182 state, &(volume), curr_partial);
184 *layer_radius += volume;
187 *layer_radius = pow(((*layer_radius) * 3.0 / 4.0 / 3.14159265359), 1.0 / 3.0);
188 if (!partial_deriv)
return;
189 for (
int i_layer = 0; i_layer <= i_layer_radius; ++i_layer) {
190 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
193 1.0 / 4.0 / 3.14159265359 * pow(*layer_radius, -2.0) * (*partial_deriv);
217 ModelData *model_data,
int aero_phase_idx,
double *radius,
218 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
219 double *aero_rep_env_data) {
221 int *int_data = aero_rep_int_data;
222 double *float_data = aero_rep_float_data;
223 double *curr_partial = NULL;
228 aero_phase_idx += offset;
264 ModelData *model_data,
int aero_phase_idx_first,
int aero_phase_idx_second,
265 double *surface_area,
double *partial_deriv,
266 int *aero_rep_int_data,
double *aero_rep_float_data,
double *aero_rep_env_data) {
268 int *int_data = aero_rep_int_data;
269 double *float_data = aero_rep_float_data;
270 double *curr_partial = NULL;
271 int layer_first = -1;
272 int layer_second = -1;
273 int layer_interface = -1;
274 int phase_model_data_id_first = -1;
275 int phase_model_data_id_second = -1;
282 int i_phase_count = 0;
283 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
284 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
287 i_phase_count == aero_phase_idx_first) {
288 layer_first = i_layer;
292 i_phase_count == aero_phase_idx_second) {
293 layer_second = i_layer;
300 layer_interface = layer_first > layer_second ? layer_second : layer_first;
306 double interface_volume = 0.0;
307 double total_volume_layer_first = 0.0;
308 double total_volume_layer_second = 0.0;
309 double volume_phase_first = 0.0;
310 double volume_phase_second = 0.0;
312 if (partial_deriv) curr_partial = partial_deriv;
313 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
314 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
315 double *state = (
double *)(model_data->grid_cell_state);
319 state, &(volume), curr_partial);
320 if (i_layer == layer_first) total_volume_layer_first += volume;
321 if (i_phase_count == aero_phase_idx_first &&
323 phase_model_data_id_first) volume_phase_first = volume;
324 if (i_layer == layer_second) total_volume_layer_second += volume;
325 if (i_phase_count == aero_phase_idx_second &&
327 phase_model_data_id_second) volume_phase_second = volume;
328 if (i_layer <= layer_interface) interface_volume += volume;
338 double f_first = volume_phase_first / total_volume_layer_first;
339 double f_second = volume_phase_second / total_volume_layer_second;
340 radius = pow(((interface_volume) * 3.0 / 4.0 / M_PI), 1.0 / 3.0);
341 *surface_area = f_first * f_second * 4 * M_PI * pow(radius, 2.0);
345 if (!partial_deriv)
return;
347 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
348 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
349 double *state = (
double *)(model_data->grid_cell_state);
353 state, &(volume_phase), NULL);
356 if (i_layer == layer_first && i_phase_count == aero_phase_idx_first) {
358 (((total_volume_layer_first - volume_phase_first) *
359 pow(total_volume_layer_first, -2.0) * f_second * (*surface_area)) +
360 2.0 * f_first * f_second * pow(radius, -1.0)) * (*partial_deriv);
364 else if (i_layer == layer_first && i_phase_count != aero_phase_idx_first) {
366 (((-1 * volume_phase) * pow(total_volume_layer_first, -2.0) *
367 f_second * (*surface_area)) + 2.0 * f_first * f_second *
368 pow(radius, -1.0)) * (*partial_deriv);
372 else if (i_layer == layer_second && i_phase_count == aero_phase_idx_second) {
374 (((total_volume_layer_second - volume_phase_second) *
375 pow(total_volume_layer_second, -2.0) * f_first * (*surface_area)) +
376 2.0 * f_first * f_second * pow(radius, -1.0)) * (*partial_deriv);
380 else if (i_layer == layer_second && i_phase_count != aero_phase_idx_second) {
382 (((-1 * volume_phase) * pow(total_volume_layer_second, -2.0) *
383 f_first * (*surface_area)) + 2.0 * f_first * f_second *
384 pow(radius, -1.0)) * (*partial_deriv);
388 else if (i_layer != layer_first && i_layer != layer_second) {
389 *(partial_deriv++) = ZERO;
392 printf(
"\n\nERROR No conditions met for surface area partial derivative.\n\n");
417 ModelData *model_data,
int aero_phase_idx,
double *layer_thickness,
418 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
419 double *aero_rep_env_data) {
421 int *int_data = aero_rep_int_data;
422 double *float_data = aero_rep_float_data;
424 double radius_inner, radius_outer;
426 int aero_phase_idx_temp = aero_phase_idx;
430 double *jac_inner = NULL;
431 double *jac_outer = NULL;
434 jac_inner = (
double *)calloc(jac_size,
sizeof(
double));
435 jac_outer = (
double *)calloc(jac_size,
sizeof(
double));
438 int i_layer_inner = -1;
439 int i_layer_outer = -1;
440 int i_phase_inner = -1;
441 int i_phase_outer = -1;
442 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
445 i_layer_outer = i_layer;
446 if (i_layer - 1 >= 0 ) {
447 i_layer_inner = i_layer - 1;
448 }
else if (i_layer - 1 < 0 ) {
449 i_layer_inner = i_layer;
454 int aero_phase_idx_inner = -1;
455 if (i_layer_inner == i_layer_outer) {
456 aero_phase_idx_inner = aero_phase_idx;
458 aero_phase_idx_inner = aero_phase_idx - (offset+1);
472 aero_phase_idx_inner,
479 if (i_layer_inner == i_layer_outer) {
480 *layer_thickness = radius_inner;
482 *layer_thickness = radius_outer - radius_inner;
486 for (
int i = 0; i < jac_size; ++i) {
487 partial_deriv[i] = jac_outer[i] - jac_inner[i];
519 ModelData *model_data,
int aero_phase_idx,
double *number_conc,
520 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
521 double *aero_rep_env_data) {
524 int *int_data = aero_rep_int_data;
525 double *float_data = aero_rep_float_data;
531 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
532 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
534 *(partial_deriv++) = ZERO;
558 int *aero_rep_int_data,
559 double *aero_rep_float_data,
560 double *aero_rep_env_data) {
561 int *int_data = aero_rep_int_data;
562 double *float_data = aero_rep_float_data;
589 ModelData *model_data,
int aero_phase_idx,
double *aero_phase_mass,
590 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
591 double *aero_rep_env_data) {
593 int *int_data = aero_rep_int_data;
594 double *float_data = aero_rep_float_data;
598 int i_total_phase = 0;
599 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
600 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
601 if ( i_total_phase == aero_phase_idx ) {
602 double *state = (
double *)(model_data->grid_cell_state);
606 state, aero_phase_mass, &mw, partial_deriv, NULL);
608 }
else if (partial_deriv) {
610 *(partial_deriv++) = ZERO;
638 ModelData *model_data,
int aero_phase_idx,
double *aero_phase_avg_MW,
639 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
640 double *aero_rep_env_data) {
642 int *int_data = aero_rep_int_data;
643 double *float_data = aero_rep_float_data;
647 int i_total_phase = 0;
648 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
649 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
650 if ( i_total_phase == aero_phase_idx ) {
651 double *state = (
double *)(model_data->grid_cell_state);
655 state, &mass, aero_phase_avg_MW, NULL, partial_deriv);
657 }
else if (partial_deriv) {
659 *(partial_deriv++) = ZERO;
690 int *aero_rep_int_data,
691 double *aero_rep_float_data,
692 double *aero_rep_env_data) {
693 int *int_data = aero_rep_int_data;
694 double *float_data = aero_rep_float_data;
696 int *aero_rep_id = (
int *)update_data;
697 int *update_type = (
int *)&(aero_rep_id[1]);
698 int *particle_id = (
int *)&(update_type[1]);
699 double *new_value = (
double *)&(update_type[2]);
721 double *aero_rep_float_data) {
722 int *int_data = aero_rep_int_data;
723 double *float_data = aero_rep_float_data;
725 printf(
"\n\nSingle particle aerosol representation\n");
727 printf(
"\nAerosol representation id: %d",
AERO_REP_ID_);
730 for(
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer){
731 printf(
"\nLayer: %d", i_layer);
733 printf(
"\n Number of phases: %d",
NUM_PHASES_(i_layer));
734 printf(
"\n\n - Phases -");
735 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
736 printf(
"\n state id: %d model data id: %d num Jac elements: %d",
741 printf(
"\n\nEnd single particle aerosol representation\n");
751 int *update_data = (
int *)malloc(3 *
sizeof(
int) +
sizeof(
double));
752 if (update_data == NULL) {
753 printf(
"\n\nERROR allocating space for number update data\n\n");
756 return (
void *)update_data;
769 double number_conc) {
770 int *new_aero_rep_id = (
int *)update_data;
771 int *update_type = (
int *)&(new_aero_rep_id[1]);
772 int *new_particle_id = (
int *)&(update_type[1]);
773 double *new_number_conc = (
double *)&(update_type[2]);
774 *new_aero_rep_id = aero_rep_id;
776 *new_particle_id = particle_id;
777 *new_number_conc = number_conc;
void aero_phase_get_volume__m3_m3(ModelData *model_data, int aero_phase_idx, double *state_var, double *volume, double *jac_elem)
Get the volume of an aerosol phase.
int aero_phase_get_used_jac_elem(ModelData *model_data, int aero_phase_idx, int state_var_id, bool *jac_struct)
Flag Jacobian elements used in calculations of mass and volume.
void aero_phase_get_mass__kg_m3(ModelData *model_data, int aero_phase_idx, double *state_var, double *mass, double *MW, double *jac_elem_mass, double *jac_elem_MW)
Get the mass and average MW in an aerosol phase.
int aero_rep_single_particle_get_used_jac_elem(ModelData *model_data, int aero_phase_idx, int *aero_rep_int_data, double *aero_rep_float_data, bool *jac_struct)
Flag Jacobian elements used in calcualtions of mass and volume.
void aero_rep_single_particle_get_aero_phase_avg_MW__kg_mol(ModelData *model_data, int aero_phase_idx, double *aero_phase_avg_MW, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the average molecular weight in an aerosol phase ( )
void aero_rep_single_particle_get_effective_radius__m(ModelData *model_data, int aero_phase_idx, double *radius, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the effective particle radius (m) Finds the radius of the largest layer in specified particle.
#define PARTICLE_STATE_SIZE_
void aero_rep_single_particle_get_aero_conc_type(int aero_phase_idx, int *aero_conc_type, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the type of aerosol concentration used.
void * aero_rep_single_particle_create_number_update_data()
Create update data for new particle number.
#define PHASE_NUM_JAC_ELEM_(l, p)
void aero_rep_single_particle_get_interface_surface_area__m2(ModelData *model_data, int aero_phase_idx_first, int aero_phase_idx_second, double *surface_area, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the surface area of specified particle layer (m)
void aero_rep_single_particle_print(int *aero_rep_int_data, double *aero_rep_float_data)
Print the Single Particle reaction parameters.
#define LAYER_PHASE_START_(l)
#define PHASE_MODEL_DATA_ID_(l, p)
#define TOTAL_NUM_PHASES_
#define PHASE_STATE_ID_(l, p)
void aero_rep_single_particle_update_env_state(ModelData *model_data, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Update aerosol representation data for new environmental conditions.
void aero_rep_single_particle_get_layer_thickness__m(ModelData *model_data, int aero_phase_idx, double *layer_thickness, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the thickness of a particle layer (m)
bool aero_rep_single_particle_update_data(void *update_data, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Update aerosol representation data.
void aero_rep_single_particle_get_dependencies(int *aero_rep_int_data, double *aero_rep_float_data, bool *state_flags)
Flag elements on the state array used by this aerosol representation.
void aero_rep_single_particle_get_aero_phase_mass__kg_m3(ModelData *model_data, int aero_phase_idx, double *aero_phase_mass, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the total mass in an aerosol phase ( )
#define LAYER_PHASE_END_(l)
void aero_rep_single_particle_get_effective_layer_radius__m(ModelData *model_data, int aero_phase_idx, double *layer_radius, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the effective radius of a specified layer (m)
void aero_rep_single_particle_get_number_conc__n_m3(ModelData *model_data, int aero_phase_idx, double *number_conc, double *partial_deriv, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Get the particle number concentration ( )
void aero_rep_single_particle_set_number_update_data__n_m3(void *update_data, int aero_rep_id, int particle_id, double number_conc)
Set number update data (#/m3)
void aero_rep_single_particle_update_state(ModelData *model_data, int *aero_rep_int_data, double *aero_rep_float_data, double *aero_rep_env_data)
Update aerosol representation data for a new state.