CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > SU2

Unexpected results for 2D cylinder flow

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   March 6, 2019, 18:32
Default Unexpected results for 2D cylinder flow
  #1
New Member
 
D. de Vries
Join Date: Feb 2019
Posts: 3
Rep Power: 7
ddvdc is on a distinguished road
I am trying to learn how to use SU2. As a test, I am trying to solve the 2D, incompressible, inviscid flow around a cylinder using the Euler equations. I have created a simple triangular mesh using Gmsh (see attachment.), and have changed the CFG file from the Inviscid Hydrofoil example on the SU2 website to work with my mesh instead (see attachment). I am then running the case in parallel using the command
Code:
parallel_computation.py -f cylinder.cfg -n 16
. The simulation exits after the convergence criteria are met. The inlet flow conditions are 10 m/s in the positive x-direction, so I expect a symetric flow field and no residual force in the y-direction. However, the flow field is not symmetric and there is a residual force in the negative y-direction. Note also that the velocity of the free-stream is not 10 m/s. I have attached two images depicting a set of streamlines and the pressure coefficient and velocity magnitude respectively. Can anyone tell me what I'm doing wrong here?
Attached Images
File Type: jpg flowFieldAndPressureCoefficient.jpg (54.9 KB, 20 views)
File Type: jpg flowFieldAndVelocityMagnitude.jpg (72.0 KB, 17 views)
Attached Files
File Type: zip cylinder.zip (3.1 KB, 7 views)
ddvdc is offline   Reply With Quote

Old   March 10, 2019, 22:12
Default
  #2
New Member
 
Alex
Join Date: Jul 2018
Posts: 8
Rep Power: 8
AlexF is on a distinguished road
Glancing over the .cfg file you posted, here are a few things that I would change/adjust:

-It looks like you are specifying a CFL of 1e6 on the first iteration, then switching to an adaptive one in the interval [1, 100] for all other iterations (you can monitor this value in the history file).

-You are specifying a convergence criterion of 10 orders of magnitude reduction, but you also have the minimum value of the residual set to -6 (log10). Perhaps your simulation is exiting prematurely; you can try decreasing RESIDUAL_MINVAL to see if the same setup will still converge.

-I would also consider turning off multi-grid until you are achieving appropriate results.

I’m not sure these modifications will solve your problem, but it may help point out other issues.


As for the velocity magnitude not equaling 10 m/s: The values are non-dimensionalized with respect to the initial values by default. You can alter this by using the “INC_NONDIM= ” option. Reference values will be output at the beginning of the simulation, or you can view them in the forces_breakdown.dat file.


Hope this helps,
Alex
AlexF is offline   Reply With Quote

Reply

Tags
cylinder, inviscid flow, test case


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Problem with grid convergence for turbulent flow around cylinder aakie OpenFOAM Running, Solving & CFD 3 November 13, 2018 05:39
Drag force coefficient too high for a flow past a cylinder using komega sst Scabbard OpenFOAM Running, Solving & CFD 37 March 21, 2016 17:16
Flow Simulation : air around an rotating cylinder using Solidworks Flow Simulation Wyrold Main CFD Forum 0 October 22, 2015 09:48
Flow past rotating cylinder: Problem with ForeCoeffs raf1111 OpenFOAM 1 December 16, 2013 10:45
Incorrect Drag and Drag Coefficient for flow over a cylinder ozzythewise Main CFD Forum 8 June 13, 2012 07:24


All times are GMT -4. The time now is 03:01.