|
[Sponsors] |
August 1, 2007, 05:30 |
Initial value File Interpolation
|
#1 |
Guest
Posts: n/a
|
Hi All!
When we specify initial value file and interpolate it onto definition file mesh,what it actually does? Whether it just specifies the values of various dependent variables onto the boundaries or specifies them collectively (avg/min-max values)onto the domains? If i do some changes in geometry and did another mesh for it,and specified previous result file(previous geom without changes) as initial value file and asked to iterpolate onto new mesh,to save computational time,whther it will predict diff results than the one which will start without any initial value file? I think both(with and without initial value file)should give u same results if there is no change in physics,only the computational time differs. pls comment. Thanks and Regards, Pankaj. |
|
August 1, 2007, 08:32 |
Re: Initial value File Interpolation
|
#2 |
Guest
Posts: n/a
|
Dear Pankaj,
1 - IVF into DFM: intersect the meshes and interpolate variable values to the new mesh vertex from element variable values at old mesh element vertices. 2 - Only interpolate mesh vertices values. 3 - As you said, you are using the interpolation as an initial guess. Therefore, the solution should be the same (see below) 4 - For a linear steady state calculation, the solution should be independent of the initial conditions (in any CFD code). For non-linear problems that is not always the case. For transient calculations, the solution is very much dependent of the initial conditions (in any CFD code) Hope this helps, Opaque |
|
August 3, 2007, 05:44 |
Re: Initial value File Interpolation
|
#3 |
Guest
Posts: n/a
|
Thanks Opaque,
" For a linear steady state calculation, the solution should be independent of the initial conditions (in any CFD code)." I was waiting for this confirmation only. Regards, Pankaj. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
problem with Min/max rho | tH3f0rC3 | OpenFOAM | 8 | July 31, 2019 10:48 |
Velocity blows up suddenly after 30,000+ iterations | lordvon | OpenFOAM Running, Solving & CFD | 15 | October 19, 2015 14:52 |
Orifice Plate with a fully developed flow - Problems with convergence | jonmec | OpenFOAM Running, Solving & CFD | 3 | July 28, 2011 06:24 |
Low Mach number Compressible jet flow using LES | ankgupta8um | OpenFOAM Running, Solving & CFD | 7 | January 15, 2011 14:38 |
OpenFOAM on MinGW crosscompiler hosted on Linux | allenzhao | OpenFOAM Installation | 127 | January 30, 2009 20:08 |