CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT > Fluent UDF and Scheme Programming

Simple UDF for piston movement

Register Blogs Community New Posts Updated Threads Search

Like Tree1Likes
  • 1 Post By nader1977

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 9, 2016, 13:05
Talking Simple UDF for piston movement
  #1
New Member
 
NicolasCheshire's Avatar
 
Nicolas Ramirez
Join Date: May 2016
Posts: 1
Rep Power: 0
NicolasCheshire is on a distinguished road
Dear all,

I'm working on an UDF with DEFINE_GRID_MOTION to move a boundary of a piston. This is the UDF:

Code:
#include "udf.h"
#include "unsteady.h"
#include "dynamesh_tools.h"

FILE *fp;

DEFINE_GRID_MOTION(obliqueWall,domain,dt,time,dtime)
{
    /*Declare Fluent parameters: face threat, nodes*/
    Thread *tf= DT_THREAD(dt);
    face_t f;
    Node *v;
    /*Declare Area vector A and d_displacement vector dx*/
    real NV_VEC(A);
    real NV_VEC(dx);
    /*Declare containers for variables*/
    real amplitude;
    real x;
    real w;
    real waveform;
    /*Declare containers for constants*/
    int n;
    float f1;
    float f2;
    float npx[176]; 
    float npy[176];
    int v1;
    int i;
    /*read node coordinates from the file */
    fp = fopen("meshPointsPP.out", "r");    
        if (!fp) 
            { 
            printf ("Error while opening file %s\n", "meshPointsPP.out"); 
            return 0;
            }
        while (fscanf (fp, "%d %f %f\n",&v1, &f1, &f2) == 3 )
        {
            npx[v1]=f1;
            npy[v1]=f2;
            printf("begin assignation of values of node %d\n",v1);
        }
    fclose(fp);
    printf("finish: assignation of values\n");
    /* calculate displacement vector at the node normal to the surface */
    i=1;
    begin_f_loop(f,tf)
    {
        printf("begin loop in faces\n");
        /* previous_time=PREVIOUS_TIME;*/
        F_AREA(A,f,tf);
        x=time;
        w=2*M_PI;
        amplitude=5e-6;
        waveform = amplitude*sin(w*x);
        printf("time = %f, disp = %f\n", time, waveform);
        dx[0]=A[0]*0;/*/NV_MAG(A)*waveform;*/
        dx[1]=A[1]/NV_MAG(A)*waveform;/*A[1]/NV_MAG(A)*sign;*/
        f_node_loop(f,tf,n)
        {
            printf("begin: loop in nodes\n");
            v = F_NODE(f,tf,n);
            /* update node if the current node has not been previously */
            /* visited when looping through previous faces */
            if ( NODE_POS_NEED_UPDATE (v))
            {
            /* indicate that node position has been update */
            /*so that it's not updated more than once */
            NODE_POS_UPDATED(v);
            NODE_COORD(v)[0]=dx[0]+npx[i];
            NODE_COORD(v)[1]=dx[1]+npy[i];
            i++;
            }
        }
    }
    end_f_loop(f,tf);
}
The UDF loads the initial positions x and Y of the nodes from a text file with the following format,

1, 0.000000000E+00, 0.000000000E+00
2, 2.000000000E-04, 0.000000000E+00
3, 4.000000000E-04, 0.000000000E+00
4, 6.000000000E-04, 0.000000000E+00

(...)

I compile the UDF and assign it to the movingWall zone in dynamic mesh zone. Also enabling "Deform adjacent boundary layer with zone" and using only layering. I set up the transient case with a time step size of 0.001 [s] and 100 steps, [BUT] the mesh deforms oddly and I have negative volume cells in the first time step. My mesh is (initially) a square of 35 by 20 mm.


I welcome any suggestions to my UDF or set up. I think it is a scaling issue, but I don't know where to start.

Cheers!
NicolasCheshire is offline   Reply With Quote

Old   October 7, 2016, 11:36
Default dynamesh/in-cyn/crank-rpm PROBLEME
  #2
New Member
 
Gabes
Join Date: May 2016
Posts: 10
Rep Power: 10
nader1977 is on a distinguished road
# include "udf.h"
# define RPM RP_Get_Real("dynamesh/in-cyn/crank-rpm")

/********************************* User input starts *****************************************/

/* Cell zone ID list for pressure output (cell zone ID for combustion chamber). -1 is a flag
so please keep it. */
static int Zone_ID[]={2, -1};
/* Face zone ID list for work output (face zone ID for the piston) */
static int Piston_ID[]={6, -1};

/********************************** User input ends ******************************************/

static real work=0, start_CA=0, end_CA=0;
static int counter=0;

/* Function to calculate cell volume. It takes care of 2d and 2d axisymmetric case as well. */

static real C_MYVOLUME(cell_t c, Thread *tc)
{
real factor=1.0;

#if RP_2D
if (rp_axi) factor=2*M_PI;
#endif

return C_VOLUME(c,tc)*factor;
}

/* Function to calculate face area. It takes care of 2d and 2d axisymmetric case as well. */

static void F_MYAREA(real * x, face_t f, Thread *tf)
{
real factor=1.0;

F_AREA(x, f, tf);

#if RP_2D
if (rp_axi) factor=2*M_PI;
#endif

NV_S(x, *=, factor);
}

DEFINE_ON_DEMAND(Indicated_work)
{
if(counter==0)
{
Message0("\n\n********************** IC Indicated Work Results *****************************\n");
Message0("\nIndicated work calculation has not started. Please do at least one time step.\n");
Message0("\nStart CA :%5.2f (deg) End CA :%5.2f (deg) Work : %9.3e (J)", start_CA, end_CA, work);
Message0("\n\n************************************ ******************************************\n");
}
else
{
Message0("\n\n********************** IC Indicated Work Results *****************************\n");
Message0("\nIndicated work calculation started at :%7.2f (deg)", start_CA);
Message0("\nIndicated work calculation finished at :%7.2f (deg)", end_CA);
Message0("\nFor the above duration, the indicated work is :%12.4e (J)", work);
Message0("\n\n************************************ ******************************************\n");
}
}

DEFINE_ON_DEMAND(reset)
{
counter=0;
work=0;
start_CA=0;
end_CA=0;

Message0("\n\n******************************** WARNING *************************************\n");
Message0("\nNote that this resets indicated work and the calculation start CA to zero.");
Message0("\nPlease save the data file to save the new values.");
Message0("\n\n************************************ ******************************************\n");
}

DEFINE_EXECUTE_AT_END(output_results)
{
#if !RP_HOST

int i;
real pressure, volume, fmf, mass, work_one_dt, x[ND_ND];

Thread *tc, *tf;
cell_t c;
face_t f;
FILE *fp_results;
Domain* domain;

domain=Get_Domain(1);

#if PARALLEL
if(I_AM_NODE_ZERO_P)
#endif
{
if(!(fp_results=fopen("work.txt","a")))
{
Message0("\nCan not open file-aborting!!");
exit(0);
}
}

if(counter==0)
{
start_CA = (CURRENT_TIME-CURRENT_TIMESTEP)*RPM*6.0+RP_Get_Real("dynamesh/in-cyn/crank-start-angle");

#if PARALLEL
if(I_AM_NODE_ZERO_P)
#endif
{
fprintf(fp_results, " CA Volume Pressure Yfb Work\n");
}

counter ++;
}

end_CA=CURRENT_TIME*RPM*6.0+RP_Get_Real("dynamesh/in-cyn/crank-start-angle");

#endif

node_to_host_int_1(counter);
node_to_host_real_2(start_CA, end_CA);

#if !RP_HOST
/* Calculate volume weighted pressure and burnt fuel mass fraction */

pressure=0;
volume=0;
fmf=0;
mass=0;
i=0;
while(Zone_ID[i]>=0)
{
tc=Lookup_Thread(domain, Zone_ID[i]);

begin_c_loop_int(c, tc)
{
pressure += C_P(c,tc) * C_MYVOLUME(c,tc);
volume += C_MYVOLUME(c,tc);

if(sg_premixed)
{
fmf += C_PREMIXC(c,tc) * C_R(c,tc) * C_MYVOLUME(c,tc);
}
mass += C_R(c,tc) * C_MYVOLUME(c,tc);
}
end_c_loop_int(c, tc)

i++;
}
pressure = PRF_GRSUM1(pressure);
volume = PRF_GRSUM1(volume);
fmf = PRF_GRSUM1(fmf);
mass = PRF_GRSUM1(mass);

pressure /= volume;
fmf /= mass;

/* Calcualte work by piston. Only pressure force is accounted for and viscous force is neglected. */

work_one_dt=0;
i=0;
while(Piston_ID[i]>=0)
{
tf=Lookup_Thread(domain, Piston_ID[i]);

begin_f_loop(f, tf)
{
F_MYAREA(x, f, tf);

work_one_dt += CURRENT_TIMESTEP * F_P(f,tf) * NVD_DOT(x, WALL_F_GRID_VV(f, tf)[0], WALL_F_GRID_VV(f, tf)[1], WALL_F_GRID_VV(f, tf)[2]);
}
end_f_loop(f, tf)

i++;
}

work_one_dt = PRF_GRSUM1(work_one_dt);
work += work_one_dt;

#endif

node_to_host_real_1(work);

#if !RP_HOST

/* Output volume, pressure, burnt fuel mass fraction */

#if PARALLEL
if(I_AM_NODE_ZERO_P)
#endif
{
fprintf(fp_results, "%8.2f %12.4e %12.4e %12.4e %12.4e\n", end_CA, volume, pressure, fmf, work);
fclose(fp_results);
}

#endif
}

DEFINE_RW_FILE(write_data, fp)
{
Message0("\nWriting user defined data to the data file...\n");

#if PARALLEL
#if RP_HOST
fprintf(fp, "\n%d", counter);
fprintf(fp, "\n%e", work);
fprintf(fp, "\n%e", start_CA);
fprintf(fp, "\n%e", end_CA);
#endif
#else
fprintf(fp, "\n%d", counter);
fprintf(fp, "\n%e", work);
fprintf(fp, "\n%e", start_CA);
fprintf(fp, "\n%e", end_CA);
#endif
}

DEFINE_RW_FILE(read_data, fp)
{
Message0("\nReading user defined data from the data file...\n");

#if PARALLEL
#if RP_HOST
fscanf(fp, "%d", &counter);
fscanf(fp, "%e", &work);
fscanf(fp, "%e", &start_CA);
fscanf(fp, "%e", &end_CA);
#endif
#else
fscanf(fp, "%d", &counter);
fscanf(fp, "%e", &work);
fscanf(fp, "%e", &start_CA);
fscanf(fp, "%e", &end_CA);
#endif

host_to_node_int_1(counter);
host_to_node_real_3(work,start_CA,end_CA);
}

ERROR IS
..\..\src\work.c(195) : error C2109: subscript requires array or pointer type
Randal0 likes this.
nader1977 is offline   Reply With Quote

Reply

Tags
dynamic mesh zones, grid motion, udf crash


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Issues with UDF for ball movement inside a valve A.Jalal Fluent UDF and Scheme Programming 1 July 30, 2015 02:11
UDF for 2D translational movement ThinkQuick Fluent UDF and Scheme Programming 0 July 24, 2012 02:59
Simple UDF array question [Fluent] Patrick1 Fluent UDF and Scheme Programming 0 April 19, 2012 02:41
Pb with simple Fluent UDF example for inlet francois FLUENT 0 October 9, 2008 11:34
simple rigid body motion UDF Dan FLUENT 0 January 11, 2006 06:48


All times are GMT -4. The time now is 19:18.