Information about Phoenics
 

The default is SI Units.

I am asking this question because i am currently working on an aerodynamic study of NACA 4412 airfoil for my university graduation work and I cant get correct results from the program. Please if you could give some useful tips on how to set the parameters or how to set the grid it will be very crucial for my work because I cant find any information about such applications on Phoenics and I got stuck figuring what to do to get some decent results.

This is an aerofoil Q1 input file that produces a converged solution using the Cartesian cut-cell solver in PH2018. The aerofoil .dat file is on the PHOENICS installation. You can study this case to get some tips on meshing and settings.

Thanks a lot!!! I hope this will solve my problems

Could you please tell me some tricks on how to set the perfect match of domain size-number of cells for an aerodynamic study? My domain size is 7.32x0.992x2.286 and the airfoil has chord 0.6096m and 0.9144m span.