|
[Sponsors] |
November 24, 2011, 01:31 |
naca 23015 mm reference values
|
#1 |
New Member
Shibin Mohamed
Join Date: Nov 2011
Posts: 8
Rep Power: 14 |
I have my NACA 23015 airfoil(flow speed 36m/s) which has a chord length of 100mm, max thickness 15.05mm,...
after scaling the grid to metres...what should be the reference values for area, length and depth... i am unable to obtain correct values for Cl and Cd and am quite inexperienced in using fluent...please help me its very urgent.... viscous model is spalart allmaras boundary conditions are pressure farfield for the whole i later intend to convert the 23015 to a kline fogleman type 2 backward facing step airfoil as a part of my project. Any suggestions? |
|
Tags |
kline fogleman, reference values |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Cl, Cd, Reference Values in 2D? | sniperees | FLUENT | 4 | July 2, 2016 03:09 |
problem with turbulence models after compilation? | lfgmarc | OpenFOAM Programming & Development | 19 | November 20, 2013 00:50 |
Mesh Reference Values problem. | rezki | STAR-CCM+ | 7 | July 19, 2010 05:30 |
Fluent 2D Reference Values | Adam | FLUENT | 1 | January 16, 2009 02:58 |
Why's FLUENT changing the reference values? | siw | FLUENT | 0 | November 6, 2008 13:17 |