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;
263 ModelData *model_data,
int aero_phase_idx_first,
int aero_phase_idx_second,
264 double *surface_area,
double *partial_deriv,
265 int *aero_rep_int_data,
double *aero_rep_float_data,
double *aero_rep_env_data) {
267 int *int_data = aero_rep_int_data;
268 double *float_data = aero_rep_float_data;
269 double *curr_partial = NULL;
270 int layer_first = -1;
271 int layer_second = -1;
272 int layer_interface = -1;
273 int phase_model_data_id_first = -1;
274 int phase_model_data_id_second = -1;
281 int i_phase_count = 0;
282 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
283 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
286 i_phase_count == aero_phase_idx_first) {
287 layer_first = i_layer;
291 i_phase_count == aero_phase_idx_second) {
292 layer_second = i_layer;
299 layer_interface = layer_first > layer_second ? layer_second : layer_first;
305 double interface_volume = 0.0;
306 double total_volume_layer_first = 0.0;
307 double total_volume_layer_second = 0.0;
308 double volume_phase_first = 0.0;
309 double volume_phase_second = 0.0;
311 if (partial_deriv) curr_partial = partial_deriv;
312 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
313 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
314 double *state = (
double *)(model_data->grid_cell_state);
318 state, &(volume), curr_partial);
319 if (i_layer == layer_first) total_volume_layer_first += volume;
320 if (i_phase_count == aero_phase_idx_first &&
322 phase_model_data_id_first) volume_phase_first = volume;
323 if (i_layer == layer_second) total_volume_layer_second += volume;
324 if (i_phase_count == aero_phase_idx_second &&
326 phase_model_data_id_second) volume_phase_second = volume;
327 if (i_layer <= layer_interface) interface_volume += volume;
337 double f_first = volume_phase_first / total_volume_layer_first;
338 double f_second = volume_phase_second / total_volume_layer_second;
339 radius = pow(((interface_volume) * 3.0 / 4.0 / M_PI), 1.0 / 3.0);
340 *surface_area = f_first * f_second * 4 * M_PI * pow(radius, 2.0);
344 if (!partial_deriv)
return;
346 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
347 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
348 double *state = (
double *)(model_data->grid_cell_state);
352 state, &(volume_phase), NULL);
355 if (i_layer == layer_first && i_phase_count == aero_phase_idx_first) {
357 (((total_volume_layer_first - volume_phase_first) *
358 pow(total_volume_layer_first, -2.0) * f_second * (*surface_area)) +
359 2.0 * f_first * f_second * pow(radius, -1.0)) * (*partial_deriv);
363 else if (i_layer == layer_first && i_phase_count != aero_phase_idx_first) {
365 (((-1 * volume_phase) * pow(total_volume_layer_first, -2.0) *
366 f_second * (*surface_area)) + 2.0 * f_first * f_second *
367 pow(radius, -1.0)) * (*partial_deriv);
371 else if (i_layer == layer_second && i_phase_count == aero_phase_idx_second) {
373 (((total_volume_layer_second - volume_phase_second) *
374 pow(total_volume_layer_second, -2.0) * f_first * (*surface_area)) +
375 2.0 * f_first * f_second * pow(radius, -1.0)) * (*partial_deriv);
379 else if (i_layer == layer_second && i_phase_count != aero_phase_idx_second) {
381 (((-1 * volume_phase) * pow(total_volume_layer_second, -2.0) *
382 f_first * (*surface_area)) + 2.0 * f_first * f_second *
383 pow(radius, -1.0)) * (*partial_deriv);
387 else if (i_layer != layer_first && i_layer != layer_second) {
388 *(partial_deriv++) = ZERO;
391 printf(
"\n\nERROR No conditions met for surface area partial derivative.\n\n");
416 ModelData *model_data,
int aero_phase_idx,
double *layer_thickness,
417 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
418 double *aero_rep_env_data) {
420 int *int_data = aero_rep_int_data;
421 double *float_data = aero_rep_float_data;
423 double radius_inner, radius_outer;
425 int aero_phase_idx_temp = aero_phase_idx;
429 double *jac_inner = NULL;
430 double *jac_outer = NULL;
433 jac_inner = (
double *)calloc(jac_size,
sizeof(
double));
434 jac_outer = (
double *)calloc(jac_size,
sizeof(
double));
437 int i_layer_inner = -1;
438 int i_layer_outer = -1;
439 int i_phase_inner = -1;
440 int i_phase_outer = -1;
441 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
444 i_layer_outer = i_layer;
445 if (i_layer - 1 >= 0 ) {
446 i_layer_inner = i_layer - 1;
447 }
else if (i_layer - 1 < 0 ) {
448 i_layer_inner = i_layer;
453 int aero_phase_idx_inner = -1;
454 if (i_layer_inner == i_layer_outer) {
455 aero_phase_idx_inner = aero_phase_idx;
457 aero_phase_idx_inner = aero_phase_idx - (offset+1);
471 aero_phase_idx_inner,
478 if (i_layer_inner == i_layer_outer) {
479 *layer_thickness = radius_inner;
481 *layer_thickness = radius_outer - radius_inner;
485 for (
int i = 0; i < jac_size; ++i) {
486 partial_deriv[i] = jac_outer[i] - jac_inner[i];
518 ModelData *model_data,
int aero_phase_idx,
double *number_conc,
519 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
520 double *aero_rep_env_data) {
523 int *int_data = aero_rep_int_data;
524 double *float_data = aero_rep_float_data;
530 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
531 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
533 *(partial_deriv++) = ZERO;
557 int *aero_rep_int_data,
558 double *aero_rep_float_data,
559 double *aero_rep_env_data) {
560 int *int_data = aero_rep_int_data;
561 double *float_data = aero_rep_float_data;
588 ModelData *model_data,
int aero_phase_idx,
double *aero_phase_mass,
589 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
590 double *aero_rep_env_data) {
592 int *int_data = aero_rep_int_data;
593 double *float_data = aero_rep_float_data;
597 int i_total_phase = 0;
598 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
599 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
600 if ( i_total_phase == aero_phase_idx ) {
601 double *state = (
double *)(model_data->grid_cell_state);
605 state, aero_phase_mass, &mw, partial_deriv, NULL);
607 }
else if (partial_deriv) {
609 *(partial_deriv++) = ZERO;
637 ModelData *model_data,
int aero_phase_idx,
double *aero_phase_avg_MW,
638 double *partial_deriv,
int *aero_rep_int_data,
double *aero_rep_float_data,
639 double *aero_rep_env_data) {
641 int *int_data = aero_rep_int_data;
642 double *float_data = aero_rep_float_data;
646 int i_total_phase = 0;
647 for (
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer) {
648 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
649 if ( i_total_phase == aero_phase_idx ) {
650 double *state = (
double *)(model_data->grid_cell_state);
654 state, &mass, aero_phase_avg_MW, NULL, partial_deriv);
656 }
else if (partial_deriv) {
658 *(partial_deriv++) = ZERO;
689 int *aero_rep_int_data,
690 double *aero_rep_float_data,
691 double *aero_rep_env_data) {
692 int *int_data = aero_rep_int_data;
693 double *float_data = aero_rep_float_data;
695 int *aero_rep_id = (
int *)update_data;
696 int *update_type = (
int *)&(aero_rep_id[1]);
697 int *particle_id = (
int *)&(update_type[1]);
698 double *new_value = (
double *)&(update_type[2]);
720 double *aero_rep_float_data) {
721 int *int_data = aero_rep_int_data;
722 double *float_data = aero_rep_float_data;
724 printf(
"\n\nSingle particle aerosol representation\n");
726 printf(
"\nAerosol representation id: %d",
AERO_REP_ID_);
729 for(
int i_layer = 0; i_layer <
NUM_LAYERS_; ++i_layer){
730 printf(
"\nLayer: %d", i_layer);
732 printf(
"\n Number of phases: %d",
NUM_PHASES_(i_layer));
733 printf(
"\n\n - Phases -");
734 for (
int i_phase = 0; i_phase <
NUM_PHASES_(i_layer); ++i_phase) {
735 printf(
"\n state id: %d model data id: %d num Jac elements: %d",
740 printf(
"\n\nEnd single particle aerosol representation\n");
750 int *update_data = (
int *)malloc(3 *
sizeof(
int) +
sizeof(double));
751 if (update_data == NULL) {
752 printf(
"\n\nERROR allocating space for number update data\n\n");
755 return (
void *)update_data;
768 double number_conc) {
769 int *new_aero_rep_id = (
int *)update_data;
770 int *update_type = (
int *)&(new_aero_rep_id[1]);
771 int *new_particle_id = (
int *)&(update_type[1]);
772 double *new_number_conc = (
double *)&(update_type[2]);
773 *new_aero_rep_id = aero_rep_id;
775 *new_particle_id = particle_id;
776 *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.