|February 24, 2016, 08:58||
Problem with initialisation using interpolation
Join Date: Feb 2016
Posts: 3Rep Power: 3
I am trying to simulate supersonic flow on a wedge.During the flow,the wedge angle changes by 0.5 degrees (not due to the flow loads but due to our external input).The nature of flow on the current wedge angle is sensitive to the previous one i.e the path through which this angle came.I am not looking for transient flow but the steady flow after the wedge angle is changed.
To simulate this, I have tried to first solve flow around previous wedge angle,save the data as interpolation file and then initialise this data for the current wedge angle and yeah the mesh changes but I gave same element sizing and mapped face mesh inorder to make sure its not too different from the previous one.
But the initialisation is not working as expected (See the figures attached)
Any help on this is appreciated..Also is there any other way to simulate the physics?
|Thread||Thread Starter||Forum||Replies||Last Post|
|Interpolation with multiple weighing criteria||i_m3_mys3lf||Main CFD Forum||13||May 11, 2015 11:03|
|Help on 2D interpolation in StarCCM+||madhuri||CD-adapco||0||November 3, 2010 15:21|
|Can I solve this problem by Fluent?||Kai_kc||FLUENT||1||October 27, 2010 05:29|
|Surface interpolation schemes and parallelization||jutta||OpenFOAM Running, Solving & CFD||0||February 25, 2010 15:32|
|Interpolation problem!||Severin||FLUENT||1||July 28, 2006 06:10|