|
[Sponsors] |
![]() |
![]() |
#21 | |
New Member
Ersin
Join Date: Sep 2018
Posts: 9
Rep Power: 7 ![]() |
Quote:
Hi tjuAeron, The boundary conditions that I used were nearly same as in the tutorial bentRotorStator because that was my first run with the solver steadyCompressibleMRFFoam and also in foam-extend. The resultant fileds were not true for real rotor 37 ofc. I am not experienced in turbomachinery but at least those are some results ( ![]() I am having a break on this project due to other projects. Ersin |
||
![]() |
![]() |
![]() |
Tags |
nasa 67, openfoam, rhosimplefoam, rotor37 |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
NASA Format | Stone | CFX | 3 | August 11, 2021 02:16 |
Multiphase flow - incorrect velocity on inlet | Mike_Tom | CFX | 6 | September 29, 2016 01:27 |
Ansys CFX problem: unexpected very high temperatures in premix laminar combustion | faizan_habib7 | CFX | 4 | February 1, 2016 17:00 |
Error in Two phase (condensation) modeling | adilsyyed | CFX | 15 | June 24, 2015 19:42 |
Segmentation fault in running alternateSteadyReactingFoam,why? | NewKid | OpenFOAM | 18 | January 20, 2011 16:55 |