UDF for fan model
Dear everyone I'm making the air flow through a fan. The relationship between the pressure difference and velocity is detaP=13912V.I want use UDF to solve the problem. #include"udf.h" DEFINE_PROFILE(pressure,t,i) { real x[ND_ND]; real y; face_t f; begin_f_loop(f,t) { F_CENTROID(x,f,t);
F_PROFILE(f,t,i)=13912*C_V(cell,thread); } end_f_loop(f,t) } But i think the udf has some problems. For example,C_V(cell,thread) has some difference with the V(in the equation),V is stand for meanfacevelocity. Scecond, detaP is pressure difference not Gause pressure.Does the F_PROFILE(f,t,i)=13912*C_V(cell,thread) adapt for detaP=13912V？How to amend the UDF? Hope your reply!! Thank you so much... 
Dear zhaoh,
have you find out the solution for your question?I also concern the F_PROFILE(f,t,i) can add pressure difference or not? Yannian 
UDF for pressure variation
Hii friends
My problem is flow through river channel, I have taken a orbitary region so at exit of my geometry flow exits into river itself. so i need to know how to apply UDf at exit, as pressure must vary with P=row*g*h. my exit cross section is not uniform so what should i do please help. is it possible to apply custom field function ???? in fluent please help ASAP :) 
Dear Nirav,
I think your probelm can be solved by UDF.The formula in your fomular is height whose direction assumed in y direction, so you can write udf in this way(You have to modify some line for your own coordinate): #include "udf.h" DEFINE_PROFILE(Pressionaxiale, thread , position) { real z[ND_ND]; real y; face_t f; begin_f_loop(f, thread) { F_CENTROID(z,f,thread); y=z[1]; row=1000; g=9.8; P0=101325; F_PROFILE(f, thread, position) =(P0+row*g*y); } end_f_loop(f, thread) } 
Thank you Yannian I will try this method

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