Cp(theta) of 2D laminar circular cylinder flow

Michael_x · May 12, 2015, 15:57

Dear all,

I have a question concerning the Cp(theta) of a 2D cylinder flow at Re=150 and Ma=0.2 (see picture attached).
What I do not understand is: at theta=0 deg Cp should be 1 but in my simulation it is 1.04. Where can these 0.04 come from?
I am doing a compressible calculation (Thermal Energy) with Air Ideal Gas.

Thanks in advance,
Michael

ghorrocks · May 12, 2015, 19:23

4% error is pretty close in most cases. But if you want to be more accurate have a look at the FAQ: http://www.cfd-online.com/Wiki/Ansys..._inaccurate.3F

Michael_x · May 25, 2015, 10:52

Thanks for the answer.

I am using the fourth order backwards Euler scheme in time and the high resolution scheme in space so I am wondering if the error should not be smaller?
The same problem has been calculated with scientif CFD softwares, too, and people used to get errors smaller than 1% (time scheme: runge kutte 4th order accurate, space scheme: central differences 4th order accurate).

Do you guys expect such big errors using CFX (lower formal accuracy in advection scheme)?

Thanks in advance and greetings,
Michael

ghorrocks · May 25, 2015, 21:01

CFX is capable of very high accuracy - you are not limited by the software for how accurate you can go in most cases. The usual limitations of accuracy are the correct choice of physics options, development of a suitable mesh, time and convergence criteria and a computer big enough to run it. So the limitation is the ability of the user to do all these things properly, not the software.

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May 12, 2015, 19:23		#2
ghorrocks Super Moderator Glenn Horrocks Join Date: Mar 2009 Location: Sydney, Australia Posts: 17,854 Rep Power: 144	4% error is pretty close in most cases. But if you want to be more accurate have a look at the FAQ: http://www.cfd-online.com/Wiki/Ansys..._inaccurate.3F

May 25, 2015, 10:52		#3
Michael_x New Member M S Join Date: Nov 2014 Posts: 4 Rep Power: 12	Thanks for the answer. I am using the fourth order backwards Euler scheme in time and the high resolution scheme in space so I am wondering if the error should not be smaller? The same problem has been calculated with scientif CFD softwares, too, and people used to get errors smaller than 1% (time scheme: runge kutte 4th order accurate, space scheme: central differences 4th order accurate). Do you guys expect such big errors using CFX (lower formal accuracy in advection scheme)? Thanks in advance and greetings, Michael

May 25, 2015, 21:01		#4
ghorrocks Super Moderator Glenn Horrocks Join Date: Mar 2009 Location: Sydney, Australia Posts: 17,854 Rep Power: 144	CFX is capable of very high accuracy - you are not limited by the software for how accurate you can go in most cases. The usual limitations of accuracy are the correct choice of physics options, development of a suitable mesh, time and convergence criteria and a computer big enough to run it. So the limitation is the ability of the user to do all these things properly, not the software.