|
[Sponsors] |
September 2, 2016, 05:31 |
|
#10 |
New Member
SELANGOR, MALAYSIA
Join Date: May 2016
Posts: 18
Rep Power: 10 |
Yes, the residual convergence.
The closest that I get is as in the figure attached here. I'm reluctant to use the results, even the error compared to experimental is acceptable. Kindly please advice. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Blade Thickness Distribution w/ Blade Distortion | twolfe13 | Main CFD Forum | 1 | May 22, 2014 00:10 |
Compressor Blade Analysis in Ansys CFX | LynchMobster47 | Main CFD Forum | 0 | April 10, 2012 22:43 |
Cells with t below lower limit | Purushothama | Siemens | 2 | May 31, 2010 21:58 |
Blade thickness on propeller wash prediction | Lam | Main CFD Forum | 1 | October 28, 2005 02:36 |
Propeller thrust at diff. advance ratio (CFX 5.7) | Zoltan | CFX | 9 | April 27, 2005 08:23 |