UDF interpret in Fluent
 

Hi all, i have a very strange problem when using UDF.
I can interpret UDF on my own computer using Fluent 12.1 in Win7 64, but i cant do that in the cluster, Fluent 12.1 in Linux, it shows syntax error in line 8, which is where my udf begins. Does anyone have this problem before?

And also, when i use this udf to output result, it always have some 0 value at the beginning and i dont know why, is there anything wrong with my udf or its the compiler's fault?

My UDF


#include "udf.h"
#define ID 16
#define Vel 1
#define Angle 0
#define Alfa 1.0
#define Gama 0.15
#define rho 1.225
DEFINE_ON_DEMAND(VentilationRate)
{
Domain *d;
FILE *fp;
face_t f;
float A[2];
float x[2],z;
Thread *t,*t0,*t1;
double incid;
double v=0,v_door=0,cp=0,cp_sin=0,VentRate=0,deltaP=0;
cell_t c0, c1;
fp = fopen("data.csv","a+");
d = Get_Domain(1);
t = Lookup_Thread (d, ID);
incid = Angle/180.0*3.14159;
begin_f_loop(f, t)
{
F_AREA(A,f,t);
c0 = F_C0(f,t);
t0 = THREAD_T0(t);
c1 = F_C1(f,t); /* Get cell on other side of face */
t1 = THREAD_T1(t);
v_door= 0.5*(C_V(c0,t0)+C_V(c1,t1));/*Average the velocity before and after the door)*/
VentRate=0.5*fabs(A[1]*v_door)+VentRate;
}
end_f_loop(f, thread)


fprintf (fp, "%f\n",VentRate);
begin_f_loop(f, t)
{
F_CENTROID (x,f,t);
v = Vel*Alfa*pow(x[2]/10.0,Gama);
c0 = F_C0(f,t);
t0 = THREAD_T0(t);
c1 = F_C1(f,t); /* Get cell on other side of face */
t1 = THREAD_T1(t);
deltaP= C_P(c0,t0)-C_P(c1,t1);/*Pressure difference before and after the door*/
cp=F_P(f,t)/0.5/v/v/rho;
cp_sin= cos (incid) * F_P(f,t)/0.5/v/v/rho;
fprintf (fp, "%f,%f,%f,%f,%f,%f\n",cp,cp_sin,deltaP,v,x[0],x[2]);
}
end_f_loop(f, thread)
fclose(fp);

}

DEFINE_PROFILE(inlet_u, thread, nv)
{
double x[2];
double z;
face_t f;
float incid = Angle/180.0*3.14159;
begin_f_loop(f, thread)
{
F_CENTROID (x,f,thread);
z=x[2]/10;
F_PROFILE(f, thread, nv) = sin(incid)*Vel*Alfa*pow(z,Gama);
}
end_f_loop(f, thread)
}

DEFINE_PROFILE(inlet_v, thread, nv)
{
double x[2];
double z;
face_t f;
float incid = Angle/180.0*3.14159;
begin_f_loop(f, thread)
{
F_CENTROID (x,f,thread);
z=x[2]/10;
F_PROFILE(f, thread, nv) = cos(incid)*Vel*Alfa*pow(z,Gama);
}
end_f_loop(f, thread)
}

DEFINE_PROFILE(inlet_e, thread, nv)
{
double x[ND_ND];
face_t f;

begin_f_loop(f, thread)
{
F_CENTROID (x,f,thread);
F_PROFILE(f, thread, nv) = Vel/log(1000.0)*0.4237*Vel/log(1000.0)*0.4237*Vel/log(1000.0)/(0.01+x[2]);
}
end_f_loop(f, thread)
}

DEFINE_PROFILE(inlet_k, thread, nv)
{

face_t f;

begin_f_loop(f, thread)
{
F_PROFILE(f, thread, nv) = Vel/log(1000.0)*0.4237*Vel/log(1000.0)*0.4237/0.3;
}
end_f_loop(f, thread)
}

I resolved the problem. FYI, the txt file in windows and linux is different for return (create a new line)

ref:
http://kb.iu.edu/data/acux.html