Information about Phoenics

Anastasis · October 11, 2018, 04:06

What is the unit system using Phoenics? (SI or something else)

phoenics_cfd · October 12, 2018, 06:18

The default is SI Units.

Anastasis · October 23, 2018, 13:23

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.

phoenics_cfd · October 23, 2018, 13:54

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.

Anastasis · October 23, 2018, 14:52

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

Anastasis · October 28, 2018, 13:41

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.

October 11, 2018, 04:06	Information about Phoenics	#1
Anastasis New Member Anastasios Dalas Join Date: Oct 2018 Location: Greece Posts: 5 Rep Power: 6	What is the unit system using Phoenics? (SI or something else)

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October 12, 2018, 06:18		#2
phoenics_cfd Member michael malin Join Date: Mar 2009 Location: london Posts: 33 Rep Power: 17	The default is SI Units.

October 23, 2018, 13:23		#3
Anastasis New Member Anastasios Dalas Join Date: Oct 2018 Location: Greece Posts: 5 Rep Power: 6	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.

October 23, 2018, 14:52		#5
Anastasis New Member Anastasios Dalas Join Date: Oct 2018 Location: Greece Posts: 5 Rep Power: 6	Thanks a lot!!! I hope this will solve my problems

October 28, 2018, 13:41		#6
Anastasis New Member Anastasios Dalas Join Date: Oct 2018 Location: Greece Posts: 5 Rep Power: 6	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.