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

Help running SST k-omega Stress-Blended Eddy Simulation

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   July 15, 2017, 11:44
Default Help running SST k-omega Stress-Blended Eddy Simulation
  #1
New Member
 
Justin
Join Date: Jan 2015
Posts: 28
Rep Power: 11
DA6righthand is on a distinguished road
I'm in need of advice running a simulation. This is my first experience with LES so I'm new to the solution procedure. My project concerns a rectangular single expansion ramp nozzle which I'm only simulating half of the total domain because it's symmetric about one axis. The nozzle is being ran at a nozzle pressure ratio (ratio of nozzle inlet total pressure to free stream pressure) of 3. Initially this project was intended to be ran only as steady but the need to expand analysis to LES was deemed necessary. Since LES wasn't initially planned, my fluid domain is a bit smaller than I feel is appropriate. I used the same grid as I did for the steady simulation (~30 million elements, ~9 million nodes, good orthogonal quality and skewness). Here's what's been done thus far:

- I began running the Stress-Blended Eddy Simulation (hybrid RANS/LES) from the steady solution result.

- A time step size of \Delta t=0.5\mus was determined from the smallest element size in the jet and velocity of the flow.

- I wanted to run the simulation out to 2 ms (4000 time steps).

After 2182 time steps (1091 microseconds flow time), the below picture was generated to check the solution. It's the schlieren image created in CFD-Post plotted on multiple transparent slice planes using an inverse logarithmic greyscale.

NPR3p0v1_9SBES_1p41275msftSchlieren by Justin Holder, on Flickr

Yes, the simulation is not yet complete as it has not yet fully developed. The full domain is pictured in this plane (above, below, and aft of the jet). As you can see, I'm getting pressure waves reflecting off the left face (a pressure-inlet boundary), the top, bottom and left end (all pressure-outlet boundaries). I attempted to apply non-reflecting boundary conditions to all external boundaries but my solution fails when I do so. My questions are:

1) At what point can I enable non-reflecting conditions?

2) When I do apply non-reflecting conditions, do I need to reduce my time step size? If so, by what amount?

3) Will I even be able to use LES with this domain (i.e., my domain is too small)?

As we speak, the simulation is continuing to run. I'm just not sure of how, if I even can, get a good solution using LES with this domain. Any help is super appreciated!

Thanks,
Justin

Last edited by DA6righthand; July 18, 2017 at 09:29.
DA6righthand is offline   Reply With Quote

Reply

Tags
hybrid, les, non reflecting boundary, rans, sbes


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
Unexpected deltaT decrease in pimpleFoam simulation robyTKD OpenFOAM Running, Solving & CFD 9 June 27, 2014 07:52
Huge file sizes when Running VOF simulation aarratia FLUENT 0 May 8, 2014 13:27
Eddy Viscosity Models and Reynolds Stress Models JuPa CFX 1 August 20, 2013 19:56
Simulation running in background samiam1000 OpenFOAM 1 November 22, 2012 05:24
Detached Eddy Simulation Maged Ismail Main CFD Forum 4 June 10, 2005 09:28


All times are GMT -4. The time now is 00:26.